BERNHARD FRANZ, 42 South, C Street, Virginia, jr. T. Bookseller, Stationer and Dealer in ?IO and FANCY GOODS.fcj LIBRARY OF THE UNIVERSITY OF CALIFORNIA OF Received Accession No. ^L 3..B Class No. - LESSONS AND PRACTICAL NOTES ON STEAM, THE STEAM ENGINE, PROPELLERS, ETC., ETC., FOR fonng (fcnpms, ^tafcrats, aiift BY THE LATE W. H. KING, U. S. N. \ REVISED BY CHIEF ENGINEER J. W. KING, U. S. N. [NINTH EDITION, NEW YOKE D. VAN NOSTRAND, 192 BROADWAY LONDON : TRUBNER & COMPANY. 1864. Entered, according to Act of Congress, in the year I860, BT J. W. KING, In the Clerk's Office of the District Court of the United States for the Southern District of New York. PRINTED KY C. A. ALVOUD, NEW YORK. INSCRIBED TO HON. GUSTAYUS Y. FOX, ASSISTANT SECRETARY OF THE NAVY, IN TOKEN OF THE AID HE HAS EXTENDED TO THE ADVANCEMENT OP NAVAL IRON STEAMSHIP CONSTRUCTION. CONTENTS. INTRODUCTION, PAGE 5. CHAPTER I. STEAM. Steam, 7. Mechanical Effect, 9. Expansion of Steam, 12. Table of Hyperbolic Logarithms, 14. Back Pressure, 16. Gain by Expanded Steam, 18. EXPANSION VALVES. Sickel's, 19. Stevens', 22. Allen & Wells', 23. SLIDE CUT-OFFS. Explanation, 24. Gridiron Valve, 26. Wabash Valve, 29. OTHER KINDS OF VALVES. Double Poppet, 80. Single Poppet, 31. Hornblower's, 32. Box Valve, 33- Equilibrium Slide, 34. Double Slide Valve, 34. Piston Valve, 35. Long D Slide, 36. Short D Slide, 37. Worthington Pump Valve, 38. Pitts- burg Cam, 39. CHAPTER II. THE INDICATOR AND INDICATOR DIAGRAMS. The Indicator, 41. Cylinder Diagrams, 44. Air-pump Diagrams, 56. Power Required to Work the Air-pump, 60. CHAPTER III. THE HYDROMETER. The Hydrometer, 62. Loss by Blowing-off, 64. Gain by the Use of Heaters, 68. Injection Water, 71. Evaporation, 72. Steam and Vacuum Gauges, 75. 4: CONTENTS. CHAPTER IV. CAUSALTIES, ETC. Broken Eccentric, 79. Leaking Yessel, 79. Irregular Feed, 80. Foaming, 81. Hot Condenser, 83. Getting Under Way, 85. Coming into Port, 86. Scaling Boilers, 88. On Coming to Anchor, etc., 89. Management of Fires, 90. Patching Boilers, 93. Sweeping Flues, 95. Ash Pits, 95. Smoke-pipe Stays, 96. Grate Bars, &c., 96. Broken Air-pump, 97. Bro- ken Cylinder-head, 98. Selection of Coal, 98. Safety Valve, 99. CHAPTER V. MISCELLANEOUS. Theory of the Paddle Wheel, 101. Centre of Pressure, 114. Screw Propeller, 116. Altering the Pitch, 132. Parallel Motion, 133. Strength of Mate- rials, 136. Surface Condensers, 141. Cylindrical Boilers, 145. Boiler Explosions, 148. Horse Power, 150. Vibration of Beams, 152. Marine Economy, 154. Limit to Expansion, 155. The Proper Lift for a Valve, 155. Temperature of Condenser, 156. CHAPTER VI. WESTERN RIVER BOAT ENGINE. Western River High-Pressure Engine, 159. Side Elevation, 159. End View, 160. Explanations of Diagrams, 160. Hartuper's Lifter, 165. Stern Wheel Boats, 167. Dimensions and Proportions of the Magnolia, 169. CHAPTER VII. BOILERS, ETC. Water-Tube Boiler, 172. Horizontal Fire Tube, 173. Extracts from Report of Experiments made to Determine the Relative Efficiency of the Two Boiler?, 174. Western River Boilers, 179. Boiler Flues, 184. Riveting, 186. Su- perheated Steam, 189. Draft, 191. APPENDIX. MATERIALS. How to Test Iron, 194. Cast Iron, 195. Malleable Iron, 198. Steel, 202. Te- nacity of Metals, 206. Transverse Strength, 206. Resistance to Torsion, 207. Results of Repeated Heating Bar Iron, 207. Strength of Joints of Boiler Plates, 209, THE ELEMENTS OF MACHINERY. Motion, 211. Application of Power, 212. The Lever, 215. Inclined Plane, 217. Wheel and Axle, 219. Pulley, 219. Screw, 223. Wedge, 224. Centre of Gravity, 225. Centre of Pressure, 225. Gravity, 225. Displacement of Fluids, 227. Table of Pressure, Temperature, and Volume of Steam, 228. BRA OP THB UNIVERSITY INTRODUCTION. a book and then apologizing for having written it, is hardly in accordance with our convic- tions ; but considering, nevertheless, the eminent tal- ent which has preceded us upon the subject we have taken up, a few remarks of explanation may not be out of place. Books heretofore appearing on the steam engine, have been of two classes, or the work itself has been divided into two parts the one for the theorist, the other for the practical man. In the one case long mathematical formulas have been produced, and in the other nothing but simple rules. The prac- tical man, therefore, who has not had the advantage of a mathematical education, has nothing presented to him but the bare rules, which he is compelled wholly to reject, or take entirely upon trust. Besides, these works extend over numerous volumes, the study of which involve much time, labor, and expense, and which usually disheartens the practical man before he has made much progress. Having had many of these difficulties to surmount in our earlier studies of the steam engine, we were led to the course of keeping a Steam Journal, in which we noted, from time to time, as we progressed, whatever we thought important, and was made clear to our mind ; and this course we would also recommend the young student ; for, however well 6 INTRODUCTION. it may be to study books containing other mens 1 thoughts, when we write we are led to the habit of thinking for ourselves, which is of the highest impor- tance ; and, by keeping a journal, we have also the very great advantage of having always at our com- mand, in a condensed form, those things which are the more important, and which can be referred to at any time. Much of the present work has been taken from the Author's Journal, and the remainder has been sup- plied, from time to time, as he found leisure from his hours of business. Our object has not been so much to supply want- ing information, as to direct the student into the habit of thinking and reasoning for himself on those subjects which may be presented for his consideration, and which, in order that he may become eminent in his profession, he must thoroughly understand. It is not sufficient to assert that Newton said this, or somebody else said that. The reasons why they said it, and the fundamental principles upon which they based their conclusions, are necessary to be understood, in order to have a clear understanding of the subject; and if we have succeeded in making any thing more clear, or in rendering any service to that class of persons who are eagerly seeking for information, but who re- quire some assistance to direct them in the proper channel, our only object in launching this, our little bark, on the troubled sea of authorship, is fully accom- plished, conscious all the while, however, of the many imperfections it contains. LESSONS AND PRACTICAL NOTES. CHAPTER I. STEAM. STEAM is a thin, elastic, invisible fluid, generated by the application of heat to any liquid, usually water. That, however, which is generated while the water is in a state of ebullition, is alone generally termed steam, while that which is formed while the surface of the water is quiescent, is denominated vapor a dis- tinction, to our mind, without much difference. The mean pressure of the atmosphere at the sur- face of the ocean is equal to 14.7 pounds per square inch, or is equivalent in pressure to a column of mer- cury 29.9212 inches in height. Under this pressure, fresh water boils at a temperature of 212 Fahrenheit. The 212 is, however, not the total number of de- grees in the steam, but simply that which is indicated by the thermometer, and which is termed sensible heat ; for we all know that to raise water from the freezing to the boiling point requires a certain time, and a certain amount of fuel; and we know further, that when the water commences to boil, it does not all evaporate at once, but that the evaporation goes on 8 STEAM. gradually, and the time, and hence the fuel required to evaporate it, is much greater than that required to raise it from the freezing to the boiling point. This extra heat must have gone off somewhere, and must be in the steam, but as it is not indicated by the ther- mometer, it is termed latent heat. When the steam is reconverted into water, the latent heat becomes again sensible, which is evidenced by the large amount of water required to condense a small amount in the shape of steam. The precise ratio the one bears to the other shows the latent, compared with the sensible heat. The subject of latent heat has been one of unusual interest, ever since the invention of the steam engine, and numerous theories have been advanced, and nu- merous experiments made some of them not very carefully in order to determine the exact law it fol- lowed ; but none, up to Regnault's time, seem to have settled the subject satisfactorily. Some maintained that the latent heat of steam was a constant quantity, some that the sum of sensible and latent heat was a constant quantity, and that quantity was 1202 Fahr- enheit. This was the most popular theory, and was the one generally adopted by engineers. Others, again, maintained that neither the sensible, latent, nor sum of the sensible and latent heats, were a constant quantity, but that they all varied. The exact ratio, however, in which they varied was not established until Regnault undertook his able series of experi- ments at the instigation of the French Government. These are the latest and most reliable experiments, and we subjoin, therefore, a table compiled from his labors, which we earnestly recommend to the attention of the reader. MECHANICAL EFFECT. 9 REGNAULT'S EXPERIMENTS. Degrees of heat contained in saturated steam, in Fahrenheit degrees of heat and English inches. I -.s~ * -5 .a~ | *.l Corresponding elastic tj'is g' *S 1 ^ J Corresponding elastic C" _ o-' l-ifl force Ji|| ll-l force ill! || || In In Atmo- :?ll! Mil In In Atmo- 5j| |%* Inches. spheres. 11 ? $*i Inches. spheres. II b Fah. 32 0.1811 0.006 1123.70 248 58.7116 1.962 1189.58 50 0.361-6 0.012 1129.10 266 79.9321 2.671 1194.98 68 0.6846 0.023 1134.68 284 106.9930 3.576 1200.56 86 1.2421 0.042 1140.16 302 140.9930 4.712 1205.96 104 2.1618 0.072 1145.66 320 183.1342 6.120 1211.54 122 3.6212 0.121 1151.06 338 234.7105 7.844 1216.94 140 5.8578 0.196 1156.64 356 297.1013 9.929 1222.52 158 9.1767 0.306 1162.04 374 371.7590 12.425 1227.92 176 13.9621 0.466 1167.62 392 460.1943 15.380 1233.50 194 20.6869 0.691 1173.02 410 560.9673 18.848 1238.90 212 29.9212 1.000 1178.60 428 684.6584 22.882 1244.48 230 42.3374 1.415 1184.00 446 823.8723 27.535 1249.88 FIG. 1. FIG. 2. MECHANICAL EFFECT. We will now take into consideration the mechani- cal effect of steam, and a common-place demonstration will serve our purpose. Suppose a cylinder, A, Fig. 1, to be one square inch in area of cross section, and fitted with a steam tight piston, at- tached by means of a flexible cord to the weight $, which is of sufficient size to balance the weight of the piston, and all the parts to work without friction. Now suppose a quan- tity of water, equal to one o O cubic inch, to be placed in the bottom of this cylinder, 10 MECHANICAL EFFECT. and a fire to be lighted under it. The temperature of the water will gradually rise until it attains 212, when it will commence to boil, and the piston will soon begin 7 and continue to rise if the cylinder be long enough until it obtains a height of 1700 inches from the base. This 1700 is the volume of steam at atmospheric pressure, the water being 1, from which it is generated. If, now, we suppose to be added to the weight, $, another weight equal to the pressure of the atmosphere or a fraction less, so that motion may en- sue and the steam under the piston to be condensed, the piston will return to the bottom of the cylinder by the pressure of the atmosphere, through a space of 1700 inches, and will have raised the extra weight of 14.7 Ibs. appended to $, up that distance. Hence this cubic inch of water, by its evaporation, produced a mechanical effect of raising 14.7 pounds through a space of 1700 inches = (14.7 X 1700) 24,990 pounds through one inch. Let us now take another cylinder, B, Fig. 2, similar in every respect to A, excepting that the piston has a weight laid upon it equal to the pressure of the atmo- sphere, viz., 14.7 pounds, and suppose a fire to be lighted under this cylinder. The water, as in the other case, will be heated up to the boiling point, which, in this case, will be 250, corresponding to the pressure of two atmospheres when it will commence to evaporate, and the piston will rise until it obtains a height of 900 inches from the base, this being the volume of steam under the pressure of two atmo- spheres, water being 1. If, now, we suppose this pis- ton to be fixed where it is, the weight removed from the top of it and applied to c, then the steam condensed and the piston unfixed, it will return to the bottom of MECHANICAL EFFECT. 11 the cylinder, raising the weight applied to c, up a dis- tance of 900 inches. Now, then, since the weight of 14.71bs. was first raised 900 inches on the top of the piston, and afterwards raised the same distance by be- ing attached to ^ fr >> br K w w w w W 1.05 .049 3.05 1.115 5.05 1.619 7.05 1.953 9.05 2.203 1.1 .095 3.1 1.131 51 1.629 7.1 1.960 9.1 2.208 1.15 .140 3.15 1.147 5.15 1.639 7.15 1.967 9.15 2.214 1.2 .182 3.2 1.163 5.2 1.649 7.2 1.974 9.2 2.219 1.25 .223 3.25 1.179 5.25 1.658 7.25 1.981 9.25 2.225 1.3 .262 3.3 1.194 6.3 1.668 7.3 1.988 9.3 2.230 1.35 .300 3.35 1.209 5.35 1.677 1 7.35 1.995 9.35 2.235 1.4 .336 3.4 1.224 5.4 1.686 7.4 2.001 9.4 2.241 1.45 .372 3.45 1.238 5.45 1.696 7.45 2.008 9.45 2.246 1.5 .405 3.5 1.253 5.5 1.705 7.5 2.015 9.5 2.251 1.55 .438 3.55 1.267 5.55 1.714 7.55 2.022 9.55 2.257 1.6 .470 3.6 1.281 6.6 1.723 7.6 2.028 9.6 2.262 1.65 .500 3.65 1.295 5.65 1.732 7.65 2.035 9.65 2.267 1.7 .531 3.7 1.308 5.7 1.740 7.7 2.041 9.7 2.272 1.75 .560 3.75 1.322 5.75 1.749 7.75 2.048 9.75 2.277 1.8 .588 3.8 1.335 5.8 1.758 7.8 2.054 9.8 2.282 1.85 .615 3.85 1.348 5.85 1.766 7.85 2.061 9.85 2.287 1.9 .642 3.9 1.361 5.9 1.775 7.9 2.067 9.9 2.293 1.95 .668 3.95 1.374 5.95 1.783 7.95 2.073 9.95 2.298 2. .693 4. 1.386 6. 1-792 8. 2.079 10 2.303 2.05 .718 4.05 1.399 6.05 1.800 8.05 2.086 15. 2.708 2.1 .742 4.1 1.411 6.1 1.808 8.1 2.092 20. 2.996 2.15 .765 4.15 1.423 6.15 1.816 8.15 2.098 25. 3.219 2.2 .788 4.2 1.435 6.2 1.824 8.2 2.104 30. 3.401 2.25 .811 4.25 1.447 6.25 1.833 8-25 2.110 35. 3.555 2.3 .833 4.3 1.459 6.3 1.841 8.3 2.116 40. 3.689 2.35 .854 4.35 1.470 6.35 1.848 8.35 2122 45. 3.807 2.4 .875 4.4 1.482 6.4 1.856 8.4 2.128 50. 3.912 2.45 .893 4.45 1.493 6.45 1.864 8.45 2.134 55. 4.007 2.5 .916 4.5 1.504 6.5 1.872 8.5 2.140 60. 4.094 2.55 .936 4.55 1.515 6.55 1.879 8.55 2.146 65. 4.174 2.6 .956 4.6 1.526 1 6.6 1.887 8.6 2.152 70. 4.248 2.65 .975 4.65 1.537 6.65 1.895 8.65 2.158 75. 4.317 2.7 .993 4.7 1.548 P.7 1.902 87 2.163 80. 4.382 2.75 1.012 4.75 1.558 675 1.910 8.75 2.169 85 4.443 2.8 1.032 4.8 1.569 6.8 1.917 8.8 2.175 90. 4.500 2.85 1.047 4.85 1.579 6.85 1.924 8.85 2.180 95. 4.554 2.9 1.065 4.9 1.589 6.9 1.931 8.9 2.186 100. 4.605 2.95 1.082 4.95 1.599 6.95 1.939 8.95 2.192 1000. 6.908 3. 1.099 5. 1.609 7. 1.946 9. 2.197 10000. 9.210 C c f D EXPANSION OF STEAM. 15 The hyperbolic logarithm of any number can be found by multiplying the common logarithm by 2,30258509. From the nature of hyperbolic logarithms they are thus very useful in working steam expansively. Let the Line A, B, Fig. 5, represent Fl0 - 5 - the pressure of steam which we will as- sume to be unity at the time the cut-off valve closes ; C, D, half the length of A, a B, and the line A, C, a hyperbolic curve, .69 -f- from the table gives the mean length A of all the ordinates, 1, 2, 3, 4, &c., which before we had to arrive at by approxima- tion. If the cut-off valve, instead of closing at half stroke, had closed at some other point, say, when the piston had traveled only one-fourth its distance, C, D, would be one-fourth of a, b, and the curve A, C, would have extended from a to , attached to the center d. Should there be too much water in the dash-pot, the valve will not seat quickly, but " hang," as it is technically termed. At a there is a cock for the pur- pose of supplying it with water. Attached to the dash-pot, there is usually another cock or valve for the purpose of letting out any superfluous water. In- sufficient water is evidenced by the slamming of the valve. This cut-off was formerly made without the wiper F, there being used instead a sliding cam, shaped something like this <\ . As the valve rose up, the clutch struck the bevel on this cam, which forced the clutch out of its position, and allowed the valve to fall. With this arrangement, however, it will be seen that the valve must trip while it is rising, and as it is at its highest position when the piston is about half stroke, it cannot be possible to cut off by this mode longer than half stroke ; but with the arrangement of the wiper, it will be seen, inasmuch as it vibrates back and forth, that the valve can be just as well tripped on its descent as when rising, and this is the reason why it was sub- stituted for the cam. " Stevens."' 1 The next cut-off that we shall take 22 EXPANSION VALVES. FIG. 2. O into consideration is Stevens's, a diagram of which is shown in figure 2. A A are the steam toes ; B B, the steam-lifting toes ; D, rock-shaft arms ; C C, the valves ; #, pin in rock-shaft arm for eccentric hook. The manner in which this is made an adjustable cut-off, is by raising or lowering the toes A A, thereby giving them more or less lost mo- tion. In the position in which they are shown in the diagram, it will be seen that they will have to travel a considerable distance before touching the toes B, B, and as the piston is in motion during this time; and the steam valve closed, the steam will be acting expan- sively. If the end of the toes A A be dropped lower down, the steam will be cut off shorter ; if raised higher up, longer. By dropping the toes down, however, we diminish the lift of the valve, and also alter the lead. To retain the one, we raise the pin a in the rock-shaft arm, and the other we turn the eccentric a little ahead. To alter the point of cut-off, therefore, while the engine is in motion, so as to cut off shorter, we have first to drop the toes A A, then raise the pin a, and set the ec- centric ahead. To cut off longer, reverse the operation. The number of things required to be altered in changing the point of cutting-off is a very great objec- tion to this arrangement. In practice it has seldom been accomplished without stopping the engine. EXPANSION VALVES. 23 Allen and Wells. This cut-off is represented by sketch, figure 3. A, A, are the exhaust toes ; B B, steam toes; C C lifting toes ; D D, the valves ; E E', FIG. 8. palls fitted to the end of the toes B, B' ; F, rock-shaft arm, which is operated from the eccentric in the usual 24 SLIDE CUT-OFFS. way ; G G, a cross arm secured to the end of the rock- shaft arm ; a a, rollers on the end of the cross-arm G 7 G' ; H H, two arms fitted loosely on the rock-shaft. These arms receive their motion from any part of the engine having motion nearly coincident with that of the piston ; b ', rollers on these arms. This cut-off operates thus : The rock-shaft is put in motion by the eccentric. The pall E resting upon the roller #, is raised, and with it the toe B, and lifter toe C ; but after the pall E is raised up so as to clear the roller , the pall E slides in on top of , which, having a down- ward motion, lowers the valve, while the rock-shaft arm continues to rise. The rollers b b\ being attached to the arms H H, which having motion nearly coinci- dent with that of the piston, start to go down at nearly the same time the rock-shaft arm starts to rise. Now then by turning around the right and left-hand screw c c, the rollers b b', will be set further apart, or closer together, and will therefore alter the time they will clear the end of the pall E, and hence the point of cut- ting off. To follow farther separate the rollers b b', to cut off shorter, screw them closer together. In altering the point of cutting off we have nothing to do but to turn around the screw c c. This cut-off is like " SickePs," momentarily adjust- able, but it cannot, however, be made to cut off quite so short as " SickePs." SLIDE CUT-OFFS. In the use of the ordinary three-ported slide-valve, or other slide-valves combining both the steam and exhaust, the expansive principle can be carried only to a very small extent, owing to the derangement of SLIDE CUT-OFFS. 25 the exhaust passages. Suppose, for instance, that suffi- cient lap be given to the steam side of the valve to cause the steam to be shut off at half-stroke, and sup- pose the same amount of lap be given also to the ex- haust side, it is manifest, that when the steam is shut off, the exhaust will be shut off also, and the pent up steam, therefore, having no escape, and increasing in pressure as the piston approaches the end of the stroke, will act as a serious retarding force. This arrange- ment, therefore, cannot operate. Now, then, suppose that we put lap on the steam side, as before, but none on the exhaust, in which event another difficulty equally great presents itself. It is this : Supposing the valve, Fig. 4, to have neither lap nor lead, when the end a arrives at a!, steam will just begin to be admitted into the cylinder, but the point FIG. 4. Z>, at the same time, will have arrived at the point ', and steam just begin also to exhaust ; now, then, let half an inch be added to each end of the valve at a and 5, when the valve begins to open to steam in this case, a, instead of being at a', will be half an inch past it ; and, as there has been no lap added to the exhaust side, 1} w^ill be half an inch past ', so that the exhaust 26 SLIDE CUT-OFFS. must have opened considerably before- the piston ar- rived at the end of the stroke ; hence, in this case, we exhaust too soon. All we can do, therefore, in practice, is to strike a mean between these evils ; that is to say, when we add lap to the steam side, add lap also to the exhaust side, but not so much so that we open the exhaust before the piston arrives at the end, and close it again before it reaches the other end. The shortest this kind of valve can be made to cut-off to advantage in practice, is considered about - from commencement of stroke ; but even this we consider most too short for beneficial working of large engines. Owing to these confined limits, the beneficial re- sults obtainable from the expansive principle by this arrangement is very small, which has led to the adop- tion of an independent slide cut-off valve, situated on a separate face, back of the steam valve, as shown in FIG. 5. Fig. 5, in which a' is the steam, and b b the cut-off valve. The valve a having only sufficient lap to cover the ports a' a' fairly, when it is in the middle of the stroke, operates as in other cases, but the lap on b b can be made to any required extent, so that SLIDE CUT-OFFS. 27 during a large part of the stroke the ports V 1J are closed, preventing further access of steam to the cylinder, notwithstanding the steam valve itself is open. The valve b b is operated by an independent eccentric, through the valve stem E. In the position shown in the figure the steam is cut off about half stroke: d' shows another opening covered with the valve d, having a stem c sliding loosely through the valve b b ; the other end gf the stem passing through the chest, has a handle attached to it for the purpose of moving the valve 6?, in order to open the port d\ when the engine is stopped. This is necessary, for the reason that the engine may stop when the valve b b is in such a position as to prevent the steam from enter- ing to the steam valve a, and the engine could not,, therefore, be started. In the figure, the cut-off valve has but two ports for the admission of steam, but any number of ports can be made the more numerous, the less stroke will be required to get the necessary opening. This is what is termed the gridiron valve, from the resemblance it bears to that very useful in- strument. After this valve is once made, the point of cutting off usually remains fixed, but it can, however, be varied FIG. 6. within narrow limits by altering the stroke of the valve. Thus, in Fig. 6, supposing the end of the valve stem to be raised from a to #, the valve, instead of 28 SLIDE CUT-OFFS. being closed, as shown, will be open the distance b e, and will therefore have that much additional to travel before the steam is cut off; hence, by increasing the travel of the valve we increase the point of cutting off, and conversely, supposing the pin a had been lowered in the rock-shaft arm the distance a e, equal to a 5, the ports, instead of being closed, as shown, would be closed the distance b c; the steam, therefore, would be cut off sooner. But by altering the point of cutting off we also alter the lead of the valve ; for, taking the case in which we increased the travel of the valve, we see that when it would have been closed with the original lead, it lacked the distance b c. If its travel had been reduced, it would have lacked that much of being open. To obviate this, whenever the travel of the valve is altered, the eccentric should also be altered, so as to retain the original lead. If the travel of the valve be made too great, the valve d will pass entirely over the port d', and gradu- ally close d, unless they be set some distance apart. If the travel be made too small, the steam will be shut off, and the motion of the eccentric being reversed long before the piston arrives at the end of the stroke, steam will be admitted to it again before the steam valve closes. From the above facts, and the figure before us, we draw the following general conclusions in reference to this kind of slide cut-off valves : That, with a given amount of lap, the cutting off point can be varied from the longest point of cutting off allowable by said lap, to a certain point within the stroke, by reducing the stroke of the valve and alter- ing the eccentric so as to retain the original lead. If the stroke be reduced beyond this, steam will be shut SLIDE CUT-OFFS. 29 off and given to the piston again before it arrives at the end of the stroke. In practice, this variation will not amount to more than from about J- to | of the stroke. In altering the stroke of the valve, the slot through which the pin a moves should be an arc of a circle, struck with a radius equal to the length of the link d a, and with d as a centre. With equal leads, the ^cutting off point cannot be effected equally on both ends of the cylinder with a slide valve, owing to the connecting rod acting out of parallelism, or, in other words, owing to the crank not being at 90 when the piston is half way. The shorter the connecting rod, the greater the discrepancy. FIG. 6|. CONNECTS TO CONDENSER Fig. 6J, is an arrangement of cut-off valve as con- structed by Messrs. Merrick & Son, of Philadelphia, in 1855, for the U. S. Steam Frigate " Wabash." In consequence of the satisfactory manner in which it worked on board that vessel ; its simplicity, and easy adjustment for cutting off at any portion of the 30 OTHER KIND OF VALVES. stroke likely to be required, it lias been applied to nearly all the U. S. Screw ships recently constructed, as also to a number of other engines. C is the steam valve ; D D are the cut-off valves, attached to the valve stem E by right and left hand screws working in nuts let into the valves ; F F, rings in the steam chest cover, fitting close down on the back of the main steam valve, enclosing the space G, which is connected to the con- denser by the pipe H, for the purpose of balancing the valve. This cut-off can be worked by a separate eccentric, or from any part of the engine having a motion coin- cident with that of the piston. To alter the point of cutting-off, a wheel is on the end of the valve stem E, which, if turned in one direc- tion, will draw the valves closer together, and the openings will not be closed so soon, consequently the steam will follow the piston farther, i. e. cut off longer. To cut off shorter, the operation is reversed. OTHER KIND OF VALVES. Having explained the principles of the leading cut- offs, we will now take a glance at some of the most prominent steam and exhaust valves now in use; bur, inasmuch as the student is supposed to understand the leading features of most of these, we will not devote much time to this part of our study. Figure 7 is a diagram of a double poppet valve, in which the rectangular space, a b c d is the open- ing to the cylinder ; A B, the steam valves, and C D, the exhaust valves. The object of this arrangement is to make the valve a balance valve. Thus the steam acting on the top of A and bottom of B, if they were OTHER KIND OF VALVES. 31 of equal size, an equilibrium would be established, but the valve B is made just small enough to slip through FIG. 8. the upper seat, so that the difference in area serves to keep the valves fairly in their seats.* On the exhaust side the reverse is the case. The steam acts under C, and on top of D, the lower valve D is usually made the larger. In order to get D into its place, the upper seat is either made removable by being secured in its place by tap-bolts, or a hand-hole is cut in the side of the steam-chest, or, in some cases, it is passed in through the cylinder nozzle. Figure 8 is a diagram of the single poppet valve, in which A is the steam valve, and B, the exhaust. With these kinds of valves we see that we require considerable power to operate them by hand, as we have the full pressure of steam on the back of A, and also the exhaust on B; but when the engine is hooked on the pressure is in part balanced. On the steam valve this is occasioned at the time the valve is opened, by the exhaust valve *In some cases, the areas of the valvea are equal] and they are seated by their own weight. 8 32 OTHEK KIND OF VALVES. being closed before the piston arrives at the end of tho stroke, producing the pressure called cushion. And on the exhaust valve the pressure is reduced (at the time the valve is opened) by expansion. In some cases this pressure is but little above that in the con- denser. It is therefore obvious that these valves can be made to work with but little power from the engine. They also have the advantage of being easily made tight and occupying but little room. The disadvantage of working by hand, however, led to the adoption of the double poppet valve, the single poppet being the earlier invention. The double poppet valve is the one now almost universally used in American low-pressure river, or marine paddle-wheel engines. Figure 9 is a representation of what is termed " Hornblower's " valve, in which a a b b are the valve FIG. 9. seats ; A A, the valve ; B, one of a number of cross- bars secured to the top of the valve, to which the OTHER KIND OF VALVES. 33 valve stem is attached. From the figure it will be seen that the only surface the steam has to act upon to keep the valve in its seat, is the upper edge, c c, of the valve ; it is therefore an equilibrium valve. Figure 10 is what is termed a box valve; a a are the parts communicating with the cylinder; 5, FIG. 10. steam-pipe ; C the steam line. Divide A E into any number of equal parts, and erect the perpendiculars A B, 1 1', 2 2', an d so on. So that by placing this instrument in a small quantity of water, drawn from the boilers at intervals, it will show the exact density, by which we know how to regulate the bio wing-off. In the boilers of sea-going vessels the water is usually carried from 1 % to 2 per hydrometer, i. o /> o A o f\ position, $ ^O0.4OU 26.225 294.655 294 655 - = 1 3.394 per cent, of the power applied to 22 the wheel lost by slip. At the angle of 55 the paddle is .445 part im- mersed, but, being so near, we have taken it at a half for simplicity, and for like reason have considered the paddle at 50 entirely immersed. It will be seen from the above, that the paddle, from the time it enters the water until after it passes THEOEY OF THE PADDLE WHEEL. 113 45, is traveling horizontally at a less rate than the vessel, and the same effect ensues as it rises out of the water ; there must, therefore, be a loss from drag or negative slip. Let us see what this amounts to. Cosines. .73775 - .57358 At 55 = - -g = 8.208 per cent. " 50 = .73775 - .64279 = 9.496 " " " 45 = .73775 - .70711 = 3.064 " " 20.768 2 Doubled for entering and leaving, 41.536 41.536 22 = 1.933 per cent. We have, then, for a total loss in this wheel, slip (13.394 per cent.) + drag (1.933 per cent.) = 15.327 per cent, of the power applied to it. The total loss in the radial wheel having been shown to be 38.982 per cent, (and in the feathering wheel 15.327 per cent.), we have 23.655 per cent, in favor of the feathering wheel. But of the whole power applied to the engines, about 20 per cent, is ex- pended in overcoming friction of ditto, friction of load on working journals, working air and feed pumps with their loads, &c. Consequently, only 80 per cent, reaches the wheels, and 23.655 per cent, of 80 per cent, equals 18.924 percent, of the total power applied to the engines in favor of the feathering wheel. To stand off against this, we have the friction of the eccentrics, &c. (an amount that, perhaps, can only be estimated) extra weight and wear and tear of the wheels. It will be seen also from the above, that the differ- ence between the velocity of the feathering wheel and 114 CENTRE OF PRESSURE. the vessel being 26.235 per cent, of the speed of the wheel, and the difference between the velocity of the radial wheel and the vessel being 18 per cent, of its speed, it follows that, making the same number of revolutions, the speeds of the vessels will be as 73.775 to 82, or as 1.00 to 1.11 ; consequently, the speed of the feathering wheel will have to exceed the speed of the radial wheel 11 per cent, to give the vessel the same velocity, but this speed of the wheel is as shown consequent upon there being less resistance to the pad- dles attained by an expenditure of 18.924 per cent, less power. Centre of Pressure. The centre of pressure of a rectangular plane im- mersed in a fluid, the upper extremity of which is even with the surface of the fluid, is ^ from the bottom ; but, inasmuch as the pressure is as the depth, when its upper extremity is below the surface of the fluid, this law no longer holds good. To ascertain the centre of pressure in such case, " Jamieson on Fluids " gives the following practical rule deduced from elaborate math- ematical calculations : " Divide the difference ot the cubes of the extremi- ties of the given plane below the surface of the fluid, by the difference of their squares, and two-thirds of the quotient will give the distance of the centre of pressure below the surface, from which subtract the depth of the upper extremity, and the remainder will show the point in the centre line of the plane in which the centre of pressure is situated." This rule can be applied directly to the feathering wheel, by taking the mean immersion of the paddles CENTRE OF PRESSURE. 115 as they move through the water, and assuming figure 3 to be of the same diameter from outside to outside of paddles, as figure 2, viz: 26 feet, we find the mean immersion of the lower edges of the paddles, after their upper extremity gets below the surface, to be (29.23 -f- 37.84 -f 45.59 -f 62.44 -f 58.32 -f- 63.09 -f 67.02 -f- 69.78 -f 71.44) 19 2 + 72 = 55.87 inches, and upper edge 35.87 inches. The mean centre of pressure of the paddles in these /55.S7 3 35.87 3 \ positions is ( 55t87 2_ 3 5 87 - 2 )|- = 46.59 35.87 = 10.72 inches from top, or 9.28 inches from bottom, and the mean centre of pressure from the time the paddle enters until it leaves the water, 9.28xl9+(6.62+3.25)2 ,, , ^-=8.52 inches from the bottom. Zo In the radial wheel, however, as the outer ex- tremity of the paddle moves more rapidly than the inner extremity, and as the resistance is as the square of the velocity, the centre of pressure must be consid- erably nearer the outer extremity on this account. One-third from the bottom, in this case, is, therefore, probably, not much out of the truth ; but as a portion of the paddle only part of the time is immersed, we take the mean of the third of that portion and a third of the whole breadth of the paddle during the time it is entirely immersed. T , -- - Inus : v ~r-)V~ ~ 6.37 inches from 2ci the bottom, showing the centre of pressure under these circumstances to be (8.52 6.37 = ) 2.15 inches nearer the lower edge of the paddle in the radial than it is in the feathering wheel. THS r.-r-i-r^. 116 THE SCREW PEOPELLEE. Practical Remarks on the Foregoing. From what has been shown, it would appear that the use of the feathering wheel over the radial wheel, from the great saving it effects, would lead to its uni- versal adoption ; but, unfortunately, the practical diffi- culties are such that its use is confined within very narrow limits. The increased weight of the wheel, occasioned by the eccentrics, levers, arms, , we ascertain the pitch thus : As cosine b : whole circumference of propeller : : sine b : to whole pitch. The pitch can also be determined by construction, without any calculation whatever. Thus, supposing the line a b represents the whole circumference of the propeller, we draw the line B b at the angle to a b as- certained from measurement, and erect the perpendic- ular a B, which will give the pitch required. In a true screw, it matters not whether we take the angle at the periphery or any other part of the blade ; for, though the angle will be different, increas- ing as we approach the centre, the pitch will be the same, it only being necessary to know the circumfer- ence at the point where we measure the angle. Should the blade not be a true screw, but an ex- panding pitch, we have to take the angle at two or more points, by drawing tangents to the curve, and take the mean, for the mean angle of the blade. Thus, in figure 5, the mean of the angles B b A and c G A will give the mean angle of the blade. Some propellers are made to expand from hub to periphery, instead of from anterior to posterior portion of the blade. To ascertain the pitch of such a propeller, take the mean of the angles at several points in the blade, and proceed as above. In order to ascertain the pitch of any propeller, it is always proper to take the angles at THE SCREW PROPELLEtt. 121 two or more points in the blade, from which we learn whether it expands from hub to periphery, whether it be true screw, or no screw at all. . The fraction of the pitch, as we have explained it above, is the fraction of the pitch of one blade, but as screw propellers usually have two, three, four, six, &c., blades, constituting fractions of a double-threaded, treble-threaded, four-threaded, six-threaded, s. x 2 length of stroke in ft. x No. of revols. per min. Pitch of propeller in feet x number of revolutions per minute. Theoretical thrust in Ibs. The difference between this and the actual thrust, shows the amount lost in friction of engines, propeller, and load, overcoming resistance to edge of propeller blades, working pumps, etc. The loss from slip is independent of this. THE SCREW PEOPELLER. 125 Strain upon a Screw Propeller-blade. We can best illustrate this by an example. Given, circumference of centre of pressure of a 3 bladed propeller, 30.9 feet ; distance from hub to cen- tre pressure 41 inches; pitch 22. 5 feet; thrust 12700 pounds : required, the strain upon each blade at the hub. SOLUTION. Let F G H be the development of the he- lix on a plane, draw B D at right angles to F H, and A E at right angles to G H. Trigonometri cally, we ascertain the angles at A and D to be each = 37 9', and at C and B to be each = 52 5', and the lengths of the lines A E, B D, to be relatively as 1.000 to 1.237. Now, inasmuch as the whole thrust can be supposed to be concentrated in the centre of pressure of the blade, and as the 12700 Ibs. is in a line with the axis, it follows that, if the line A E represents the direction and amount of this thrust, the line B D, at right angles to the pro- peller blade at the centre of pressure, according to the resolution of forces, will represent the resultant of the pressures on the blade, or the total pressure tending to break it. But inasmuch as there are three blades, the pressure will be divided equally among them all ; therefore, each has to sustain but a third of this pres- sure; hence 12700 x 1.237 (proportion B D bears to A E) KOQfl O OO 3 Ibs. pressure on each blade at the centre of pressure. 126 THE SCEEW PROPELLER. The pressure at the hub on each blade equals 5236 Ibs. X 41 ins. = 214676 Ibs. acting with the leverage of one inch. EXAMPLE 2D. Suppose, in example 1, the breadth of the blades at the hub to be 32 inches, and the pro- peller to be made of composition, capable of sustaining a pressure per square inch of cross-section of 520 Ibs., acting through the leverage of 1 inch ; required, the mean thickness of the blade at the hub ? SOLUTION. The strength of beams is directly as their breadths and the squares of their depths, and in- versely as their lengths. In the example before us, the propeller resolves itself into a simple beam ; we have, then, - = 12.9 inches = square of the 32 X 520 thickness, and v/12.9 = 3.59 inches in thickness. Helicoidal Area. As has already been shown, the development of the helix on a plane is the hypothe- nuse of a right-angled triangle, having the pitch of the screw for the height; and the circumference, corre- sponding to the radii of the helix, for the base. Now, as the propeller can be supposed to have an infinite number of helices, each one becoming longer and longer as we approach the periphery, which alter the lengths at the same time, of the hypothenuse and base of the triangle, we will suppose the propeller to be divided into a number of concentric rings, taking the centre line of each, for the helix or hypothenuse of the trian- gle ; the circumference corresponding to radii of said helix for the base, and the pitch for the height, from which we have all the elements required for the cal- culation. THE SCEEW PROPELLER. 127 To make this the more clear, take the triangle B A C ; the lines B 1, B 2, B 3, B C, represent the helices having the corresponding circumferences of A 1, A 2, A3, and A C. Now, then, if these helices be the lengths of the rings, or elements for one entire convolution of the thread, all we have to do is to mul- tiply it by the breadth of the element, which will give the area for one convolution ; but as only a fraction of a convolution is used in practice, we multiply by this fraction, whatever it may be, and the product gives the area for the part used. This mode of calcu- lation is, of course, only an approximation ; but when- ever the blade is divided into a considerable number of elements, say 6 inches in breadth each, the result obtains sufficiently near the truth for all practical pur- poses. The following is a calculation on the screw of the U. S. Steam Frigate "Wabash," and which agrees, within a very small fraction, of the area as projected upon a plane : 128 THE SCEEW PKOPELLEK. Diameter of screw, IT feet 4 inches ; diameter of hub, 2 feet 4 inches. "c fti |S . J3 ,C "^ 6 4 1 .|1 9 **d *0 a! 01 ^ Pitch. Radii of 1 5g* Lengtl Elements Convolul the Th: Fraction Pitch i ^-M^ bOffl ^ J Breadths meni O A B C D E F G H 2.B x 3.1416 V A 9 ' 1 O 2 D xE FxG ft. ft. ft. ft. ft. ft. sqr. feet. 23 1.5 9.42 24.89 V 7.11 .5 3.555 u 2. 12.56 26.20 1 7.48 u 3.74 u 2.5 15.70 27.85 1 7.96 3.98 u 3. 18.84 29.73 1 8.49 4.245 (I 3.5 21.99 31.82 1 9.09 4.545 ' 4. 25.13 34.07 ' 9.73 4.865 u 4.5 28.27 36.44 4 10.41 5.205 u 5. 31.41 38.93 1 11.12 5.56 5.5 34.55 41.50 1 11.86 5.93 u 6. 37.69 44.15 "/51 12.12 6.06 it 6.5 40.84 46.87 U 12.86 6.43 u 7. 43.98 49.63 3 /n 13.54 6.77 u 7.5 47.12 52.43 4 / 15 13.78 6.89 ii 8. 50.27 55.27 J /4 13.82 6.91 ti 8.5 53.40 58.14 Vs 11.63 5.815 * Helicoidal area of one side of both blades = 80.5 square feet. Practical Remarks on the Screw Propeller. In the application of power to the propulsion of the hulls of vessels through water, a portion of the effect is lost by the instrument through which it is transmitted. In the common radial wheel this loss of effect is compounded of two losses, slip, plus oblique action ; in the feathering wheel, slip, plus drag, and in the screw propeller, slip, plus friction of the propeller blades on the water. That instrument, therefore, which, possessing no more practical disadvantages than other * For the calculations of the friction of a screw surface on the water, see Isherwood's calculation on the " San Jacinto," (Journal of the Franklin Insti- tute, Third Series, Vol. XXL, p. 349,) or on the " Arrogant," (Appleton's Me- chanics' Magazine, Vol. I., p. 156,) from which the form for the above table is taken. THE SCREW PEOPELLEE. 129 instruments, and which has the sum of its losses the least, must be the most economical propelling instru- ment. The feathering wheel, from what we have seen, would present itself very conspicuously to our eye as being the best instrument within our knowledge ; but, unfortunately, the practical difficulties are such as to preclude its universal adoption. The loss from ob- lique action in the common radial wheel, particularly where the diameter is comparatively small and the dip of the paddles considerable, amounts to an important percentage of the total power of the engines; and since this loss in the screw propeller does not exist, but is replaced by one of much smaller magnitude, viz., friction of the blades, it follows, that were the slip of the two instruments alike, the screw propeller would be the more economical. In practice, however, with the screw propeller, when contending against head winds, or other increased resistance, the slip is increased to a very serious extent. In fact, in some cases it has occurred, when the engines were going ahead at nearly full speed, the vessel stood nearly still. On the other hand, however, when the sails are set to a fair wind, the slip of the propeller is materially reduced, while the thrust remains unaltered. The increased slip when contending with head winds is also experienced with paddle wheels, but they are not affected to the same extent as the propeller, the increasing or decreas- ing the resistance with the latter instrument, not making a vast difference in the revolutions of the en- gines (as is the case with the paddle wheel) so long as the pressure on the piston remains unaltered. In the application of the screw propeller, it is well to sink it as low as possible in the water, in order that the hydrostatic pressure above may be sufficient to 130 THE SCREW PEOPELLEE. cause the water to flow in solid, even to the centre of the propeller, which, therefore, having the proper resisting medium, is less liable to excessive slip. This will also prevent the centrifugal action the throwing of the water off radially from the centre which exists to a small extent in some very aggravated cases. Increasing the helicoidal surface of the screw be- yond what is barely sufficient to transmit the power given to it, has no other effect than to occasion an increased loss by friction, by the increased surface in- terposed. The friction of solids on fluids, unlike solids on solids, depending upon the extent of rubbing sur- face as one of the elements. The object, therefore, to be sought after in practice, is to make the sum of the loss by slip, plus friction, as little as possible, and this sum, manifestly, must depend, to a considerable extent, on the amount of helicoidal surface ; but, nevertheless, there appears to be no general rules yet devised, from theory or practice, which can be used as a reliable guide ; different engineers making considerable differ- ence in the areas of propellers applied to the propulsion of the same sized and modeled steamers. Negative Slip. It would certainly appear a very strange anomaly, were one on boarcj a vessel, which he should discover from the indications of the log was mov- ing actually faster through the water than the screw, there being no other propelling instrument ; yet such has been apparently the case, and there are, perhaps, to this day, persons though we hope they are very few who think that a screw propeller may drive a vessel faster than it is moving itself. There have been cases, it is true, where the log has shown that the ves- sel was apparently moving faster than the screw, which THE SCEEW PEOPELLEE. 131 alone was the propelling instrument, but that such a thing could be true is absolutely absurd, and hence attention was turned to discovering the anomaly. It is accounted for in two ways. When a body having a blunt stern is drawn through water at a high velocity, the water, not being able to flow in from the sides of the body sufficiently rapid to fill the vacuity occasioned by its passage, flows in from all other directions, and a column of water, therefore, necessarily, follows in the wake of such a body. This is the case with screw propeller vessels having blunt runs, and, by consequence, the propeller, instead of acting upon water at rest, acts upon water in motion, having the same direction as the vessel. Now, then, supposing a propeller, acting upon water at rest, to have a slip of 10 per cent., if a column of water follow the ship with the velocity of 11 per cent, of the speed of the propeller, which still retains its ten per cent, slip, the log, as it takes no cognizance of the velocity of this water, would show a negative slip of 1 per cent., i. e., it would show the vessel to be actually moving 1 per cent, faster than the propeller, when in reality the latter would be moving 10 per cent, the faster. To produce such a result as this, of course, possesses no mechanical or other advantage ; for power must have been originally taken from the engines to pro- duce the current, which cannot be returned to its full extent. It is, therefore, a very important element in the design of a screw vessel to make the run very sharp the lines fine in order that the water may flow in solid at once, to fill the vacuity occasioned by the vessel's progress, or the propeller's revolutions. The other theory in regard to negative slip is this : All known bodies yield to pressure, it being only 132 ALTEEING THE PITCH. necessary in order to cause the amount of yield to be measurable to make the pressure sufficiently great. It is hence conceived, that when a screw propeller is in motion, the pressure of the water on the blades causes them to spring, thereby increasing the pitch; conse- quently, in calculating its speed through the water, if we use the true pitch, instead of the pitch assumed, while it is in motioa, the velocity given to it will be too small, and may be less than the velocity of the vessel. We would, however, remark, that negative slip in a screw propeller, unassisted by sails, is more imaginary than real, and could only exist under very aggravated circumstances, for a screw propeller usually has about 20 per cent, slip, at least, and to reduce this to nothing, even under the conditions set forth above, would be rather a perversion of circumstances. Altering the Pitch. Propellers are sometimes constructed in such a manner that the pitch can be altered, from time to time, by altering the angle of the blades, which are made adjustable in a large spherical hub. Thus, if it be desired to increase the pitch, increase the angles by turning round the blades ; or if it be desired to de- crease the pitch, reverse the operation. Such an ar- rangement, however, in practice, must be confined within very narrow limits, for, inasmuch as the surface of a screw propeller blade, being that of a helicoid, every point in the blade must have a different angle, which increases as the hub is approached, and if the propeller be constructed so that all the angles be adapted to one particular pitch, it is not very likely PARALLEL MOTION. 133 that they will, after being distorted, be adapted to any other pitch ; that is to say, if the propeller be a true screw, for instance, and have a certain angle at the periphery, if we move the blade so as to increase the angle at that point 10, the angle at every other point in the blade will also be increased 10, which should not be the case, but should be correspondingly less as the hub is approached; thus, by this arrangement, we give a greater pitch at the hub than there is at the periphery ; and if the operation be reversed, and we decrease the angle at the periphery, the angle at the hub, and every other point in the blade, is decreased to precisely the same extent, thus giving less pitch at the hub than there is at the periphery, or any other point in the blade. We therefore arrive at this con- clusion : That having three conditions presented to us, viz., true screw, expanding screw, from periphery to hub, and expanding from hub to periphery the latter two not in regular ratio it is more than probable that one or the other of these must be found practically to be the superior, and whichever it may be, and that one adopted, the advantage to be derived from alter- ing it, after it is once adopted, does not appear very plain, the arguments to the contrary notwithstanding. Parallel Motion. Parallel motion is a combination of bars and rods, having for its object the guiding of the piston-rod of a steam-engine in a constant straight line, or as near a straight line as can be practically attained. It is ap- plicable, in different forms, to any type of engine, but 134 PARALLEL MOTION. its adaptation to the side-lever engine is the more general. We have constructed figure 10 with the view of FIG. 10. illustrating its application to this type of engine, and to clear it, if possible, of the mystery that usually hangs over it in the shape of formulas. A B is half the length of the side lever, vibrating on the centre B ; A C, the side rod attached to the cross-head at C ; Gr F, the parallel motion side rod ; D F, the parallel bar, and E F, the radius bar vibrating on the centre E. The object to be attained is to make the point C travel vertically in a straight line, or as near so as pos- sible ; and from the construction of the figure, it will be seen that, when the point Gr moves to the right the point F moves to the left, and vice versa ; hence it is manifest, that there must be some point H, in the rod F Gr, which will describe very nearly a straight line, and if the lengths G B and E F were equal, that point would be in the centre of F Gr ; but, since they are of unequal lengths, H must be in such a position that EFxFH^BGxGH. PAEALLEL MOTION. 135 Now, then, having secured the point H, draw the line B C through H, which will determine C, the cen- tre of the cross-head ; and the triangles B H G, B C A, being similar, and joined together in such manner that, no matter how much the angles of the one may alter, the angles of the other must alter to precisely the same extent ; and hence, these triangles always remain- ing similar, it follows that if the apex (H) of the one moves in a straight line, the apex (C) of the other must move in a straight line also. It matters not where the points D F G may be situated, so long as D does not coincide with C, and the figure A D F G is a parallelogram ; nor does it matter about the respective lengths of the sides of the parallelogram, so long asEFxFH=:BGxGH. In practice, it happens sometimes that the parallel motion gets out of adjustment, the piston rod perhaps rubbing hard on one side of the stuffing-box at the top of the stroke, and hard on the opposite side on the bottom of the stroke ; or it may rub hard on the stuff- ing-box at one end of the stroke, and be quite free at the other. Such a result can be brought about in three ways only : either the sides of the parallelogram A D F G have got out of parallelism, the radius bar E F, of incorrect length from the wear of the brasses, , furnace doors ; prepared by the direct combination of iron and carbon. The process is to take the best bars and plates of wrought iron and expose them in a converting furnace, for seven or eight days, to a me- dium temperature, in contact with powdered .charcoal, so as to totally exclude the air. The bars, on being taken out, exhibit in the fracture a uniform crystalline appearance. The degree of carbonization is varied according to the purpose for which the steel is in- tended. CAST STEEL. 203 Shear Steel is generally made from blistered steel refined by piling into fagots, which are brought to a welding heat in a reverberatory furnace, hammered and rolled again into bars ; this operation is repeated several times to produce the finest kind of shear steel. The name is derived from the fact that this variety of steel was used in England for shears. Cast Steel. For this important invention we are indebted to Benjamin Huntsman, of the village of Hands worth, near Sheffield, England, who, about the year 1740, perfected his invention, from which the civilized world has derived such vast and varied ad- vantages. It is made by breaking blistered steel or cutting bar iron into small pieces, and melting it in combination with a small quantity of charcoal (when it is made from iron, manganese is mixed with it) in close air-tight crucibles, from which it is poured into iron moulds ; the ingot is then reduced to a bar by hammering or rolling, as described under the head of malleable iron. Cast steel is the finest kind of steel. It is known by a very fine, even, and close grain, and a silvery and homogeneous fracture ; it is very brittle, and acquires extreme hardness, but is difficult to weld without the use of a flux. The other kinds of steel have a similar appearance to cast steel, but the grain is coarser and less homogeneous; they are softer, less brittle, and weld more readily. Properties of Steel. The best steel possesses the fol- lowing characteristics : Heated to redness and plunged into cold water, it becomes hard enough to scratch glass and to resist the best files ; the hardness is uni- form throughout the piece ; after being tempered it is 204 CAST STEEL. not easily broken; it welds readily; it does not crack or split ; it bears a very high heat, and preserves the capability of hardening after repeated working ; the grain \sfine, even, and homogeneous, and it receives a brilliant polish. Hardening and Tempering. On these operations the quality of manufactured steel in a great measure depends. Hardening is effected by heating the steel to cherry red and plunging it into a liquid, generally cold water; the degree of hardness depends on the heat and rapidity of cooling. Tempering. Steel in its hardest state being too brittle for most purposes, the requisite strength and elasticity are obtained by tempering, which is per- formed by heating the hardened steel to a certain degree and cooling it quickly. The requisite heat is usually ascertained by the color which the surface of the steel assumes a straw color is common for cold chisels and machinists' tools. Case Hardening. This operation consists in con- verting the surface of wrought iron into steel, by heat- ing the iron to a cherry red, in a close vessel, in contact with carbonaceous materials, and then plunging it into cold water. Bones, leather, hoofs, and horns of animals are used for this purpose, after having been burnt or roasted, and pulverized. Soot is also frequently used. To Test the Quality of Boiler Iron. Bend it cold at sharp angles, and double the pieces together ; heat it cherry red, and perform the same operation, and punch holes very near the edges of the sheets. If it stands these tests without cracking, it is neutral iron, and of the best quality. CAST STEEL. 205 To Test the Quality of Bar Iron. Cut a notch on one side with a cold chisel, then bend the bar over the edge of an anvil at sharp angles. If the fracture exhibits long silky fibres, of a leaden gray color, co- hering together, and twisting or pulling apart before breaking, it denotes tough, soft iron, easy to work and hard to break. In general, a short, blackish fibre in- dicates iron badly refined. A very fine close grain denotes a hard steely iron, which is apt to be cold short, but working easily when heated, and making a good weld. Numerous cracks on the edges of the bar generally indicate a hot short iron, which cracks or breaks when punched or worked at a red heat, and will not weld. Blisters, flaws, and cinder holes are caused by imperfect welding at a low heat, or by iron not being properly worked, and do not always indicate inferior quality. To Test Iron when Hot. Draw a piece out, bend and twist it, split it and turn back the two parts, to see if the split extends up ; finally, weld it, and observe if cracks or flaws weld easily. Good iron is frequently injured by being unskilfully worked: defects caused by this may be in part remedied. If, for example, it has been injured by cold hammering, moderate anneal- ing heat will restore it. Steel. To test steel, break a few bars, taken at random, make tools of them, and try them in the severest manner. For further information on the subject of materials, we refer the reader to an excellent work called u Use- ful Metals and their Alloys," by Messrs. Clay, Aitken, Vospicket, and Fairbairn. 206 TENACITY OF MATERIALS. Tenacity of Materials. Cast Steel 134,000 Ibs. Swedish 72,000 ^ Experiments by Frank- Salisbury, Conn 66,000 I lin Institute/on bars Bar-iron Bellelonte, Pa 68,500 f whose cross section English 56,000 I was about one-fifth Pittsfield, Mass 57,000 | of a square inch. Pig metal 15,000 n Good common castings 20,000 Experiments of Maj. W. Specks ,0,,, gun *I j HJOJ ? _, Cast Steel 128,000 on pieces whose cross B _ g n m eta, | 000 5*J *- T ' Copper, cast, (Lake Superior) 24,138 Brass 18,000 S Wrought .. 34,000 C PP er |cast..r. 19,'000 Tin, cast 4,800 Zinc 3,500 Platinum 56,000 Silver , 40,000 Gold 30,000 Lead 1,800 WOODS. Ash 15,800 Mahogany 11,500 Oak 11,600 White Pine 11,800 Walnut 7,700 In general, the tenacity of metals is increased by hammering and wiredrawing. The strength of Pitts- field bar iron, given in the above table, is the mean of four trials, with cylinders 1 inch long and 0.9 inch di- ameter. They were extended in length, before frac- ture, to 1.4 in., and they were reduced in diameter to 0.6 in. in the middle. A bar of wrought iron is extended about one-hun- dredth part of its length for every ton of strain on a square inch. Transverse Strength. S the weight in pounds required to break a beam 1 in. square and 1 in. long, fixed at one end and loaded at the other ; b the breadth, d the depth, and I the RESISTANCE TO TORSION. 207 length, in inches, of any other beam of the same mate- rial, and "W the weight which will cause it to break, neglecting the weight of the beam itself. 1. If the beam is supported at one end, and loaded at the other : 2. If the beam is supported at one end, and the load distributed over its whole length : 3. If the beam is supported at both ends, aiid loaded in the middle : 4. If the beam is supported at both ends, and loaded uniformly over its whole length : bd* W = SS -j- 5. If the beam is supported at both ends, and loaded at the distance m from one end : W = S 7-j -- r m (i m) Resistance to Torsion. S the weight in pounds required to break, by twisting, a solid cylinder, 1 inch diameter ; the weight acting at the distance of 1 inch from the axis of the cylinder ; d, the diameter in inches of any other cylin- der of the same material ; r, the distance from its axis to the point where the breaking weight W is applied ; then: Results of Repeated Heating Bar Iron. In a series of experiments, with regard to the im- provements and deterioration which result from oft- repeated heating and laminating of bar iron, made by William Clay, Esq., of the Mersey steel and iron works, Liverpool, he says that, taking a quantity of ordinary 14 208 RESULTS OF REPEATED HEATING BAR IROX. fibrous puddled iron, and reserving samples marked No. 1, we piled a portion five high, heated and rolled the remainder into bars marked No. 2, again reserving two samples from the centres of these bars, the remain- der were piled as before, and so continued until a por- tion of the iron had undergone twelve workings. 41 The following table shows the tensile strain which each number bore : Nov Pounds. 1. Puddled bar 43,904 2. Re-heated 52,864 3. 59,585 4. 59,585 5. 57,344 6. 61,824 7. 59,585 8. 57,344 9. 57,344 10. : 54,104 11. 51,968 12. 43,904 " It will thus be seen that the quality of the iron increased up to No. 6, (the slight difference of No. 5 may, perhaps, be attributed to the sample being slightly defective) ; and that from No. 6 the descent was in a similar ratio to the previous increase." TENSILE STRENGTH OF IRON AND STEEL BARS PER SQUARE INCH. Description of Iron and Steel. Tensile Strength. Authority. 62 644 English Rolled Iron 56 532 American Board of 56,103 Ordnance American Hammered ... ... 53 913 Krupp's Cast Steel, average of 3 samples... Cast Steel highest 111,707 142 2 k > -) Min. of War, Berlin. Mallett *' mean 88 657 do u u 134,256 150,000 Shear Steel 124 400 Blister " 133,152 Mersey Steel and Iron Co. Puddled steel, highest 173 817 Dito another sample . 160 832 Average of three samples tested at the Liv- erpool Corporation testing machine 112,000 STRENGTH OF JOINTS OF BOILER PLATES. 209 On the strength of the joints of single and double riveted boiler plates, by William Fairbairn, Esq., F. R. S. On comparing the strength, of plates with their riveted joints, it will be necessary to examine the sec- tional areas taken in a line through the rivet-holes with the section of the plates themselves. It is perfectly obvious, that in perforating a line of holes along the edge of a plate, we must reduce its strength : it is also clear that the plate so perforated will be to the plate itself, nearly as the areas of their respective sections, with a small deduction for the irregularities of the pressure of the rivets upon the plate ; or, in other words, the joint will be reduced in strength somewhat more than in the ratio of its section through that line to the solid section of the plate. It is evident that the rivets cannot add to the strength of the plates, their ob- ject being to keep the two surfaces of the lap in contact. When this great deterioration of strength at the joint is taken into account, it cannot but be of the greatest importance that in structures subjected to such violent strains as boilers and ships, the strongest method of riveting should be adopted. To ascertain this, a long series of experiments yy- ^ were undertaken by Mr. Fairbairn, - some of the results of which will be of interest here. The joint or- dinarily employed in ship building is the lap joint, shown in Figs. 1 and 2. The plates to be united are made to overlap, and the rivets are passed through them, no cov- ering-plates being required, except at the ends of the plate, where they butt against each 210 STRENGTH OF JOINTS OF BOILER PLATES. other. It is also a common practice to countersink the rivet-heads on the exterior of the vessel, that the hull may present a smooth surface for her passage through the water. This system of riveting is only used when smooth surfaces are required ; under other circum- stances, their introduction would not be desirable, as they do not add to the strength of the joint, but, to a certain extent, reduce it. There are two kinds of lap- joints, those said to be single-riveted (Fig. 1), and those which are doable-riveted (Fig. 2). At first, the former were almost universally employed, but the greater strength of the latter has since led to their general adoption in the larger descriptions of vessels. The rea- son of the superiority is evident. A riveted joint gives way either by shearing off the rivets in the middle of their length, or by tearing through one of the plates in the line of the rivets. In a perfect joint, the rivets should be on the point of shearing just as the plates were about to tear ; but in practice, the rivets are usually made slightly too strong. Hence, it is an estab- lished rule, to employ a certain number of rivets per lineal foot. If these are placed in a single row, the rivet-holes so nearly approach each other, that the strength of the plates is much reduced ; but if they are arranged in two lines, a greater number may be used, and yet more space left between the holes, and greater strength and stiffness imparted to the plates at the joint. The experiments of Mr. Fairbairn and others have established the following relative strengths as the value of plates with their riveted joints : Taking the strength of the plate at 100 The strength of the double-riveted joint would then be 70 And the strength of the single-riveted joint 50 MOTION. 211 THE ELEMENTS OF MACHINEKY. IN consequence of having found many young en- gineers unacquainted with the principles of mechani- cal powers, we have thought best to devote a short space to the subject, prefacing it with the description of motion, and application of power, by David A. Wells, A. M. Motion. Motion is the act of changing place. It is absolute or relative. Absolute motion is a change of position in space, considered without reference to any other body. Relative motion is motion considered in rela- tion to some other body, which is either in motion or at rest. When a body commences to move from a state of rest, there must be some force to cause its motion, and this force is generally termed u Power." On the contrary, a force acting to retard a moving body, de- stroy its motion, or drive it in a contrary direction, is termed " Resistance." The chief causes which tend to retard or destroy the motion of a body are gravi- tation, friction, and resistance of the air. The speed, or rate, at which a body moves, is termed velocity. The momentum of a body is its quantity of motion, and this expresses the force with which one body in motion would strike against another. This momentum, or force, which a moving body exerts, is estimated by multiplying its weight by its velocity. Thus a body weighing 20 Ibs., and moving with a velocity of 200 feet per second, will have a momentum of 20 x 200 = 4000. 212 APPLICATION OF POWER. Action and Reaction. When a body communicates motion to another body, it loses as much of its own momentum, or force, as it gives to the other body. The term Action is applied to designate the power which a body in mo- tion has to impart motion, or force, to another body ; and the term Reaction to express the power which the body acted upon has of depriving the acting body of its force or motion. There is no motion, or action without a corresponding and opposite action of equal amount ; or, in other words, action and reaction are always equal and opposed to each other. Application of Power. The principal agents from whence we obtain power for practical purposes, are men and animals, water, wind, steam, and gunpowder. When work is performed by any agent, there is always a certain weight moved over a certain space, or resistance overcome ; the amount of work per- formed, therefore, will depend on the weight, or re- sistance that is moved, and the space over which it is moved. For comparing different quantities of work done by any force, it is necessary to have some stand- ard ; and this standard is the power, or labor, ex- pended in raising a pound weight one foot high, in opposition to gravity. A machine is an instrument, or apparatus, adapted to receive, distribute, and apply motion derived from some external force in such a way as to produce a desired result ; but it cannot, under any conditions, create power, or increase the quantity of power or force applied to it. Perpetual motion, or the con- struction of machines which shall produce power sufficient to keep themselves in motion continually, is, APPLICATION OF POWER. 213 therefore, an impossibility, since no combination of ma- chinery can create, or increase, the quantity of power applied, or even preserve it without diminution. The great general advantage that we obtain from machinery is, that it enables us to exchange time and space for power. Thus, if a man could raise to a cer- tain height 200 pounds in one minute, with the utmost exertion of his strength, no arrangement of machinery could enable* him unaided to raise 2000 pounds in the same time. If he desired to elevate this weight, he would be obliged to divide it into ten equal parts, and raise each part separately, consuming ten times the time required for lifting 200 pounds. The application of machinery would enable him to raise the whole mass at once, but would not decrease the time occupied in doing it, which would still be ten minutes. The power will overcome the resistance of the weight, and motion will take place in a machine, when the product arising from the power multiplied by the space through which it moves in a vertical direction, is greater than the product arising from the weight multiplied by the space through which it moves in a vertical direction. Thus if a small power acts against a great resistance, the motion of the lat- ter will be just as much slower than that of the power, as the resistance or weight is greater than the power, or if one pound be required to overcome the resistance of two pounds, the one pound must move over two feet in the same time that the resistance, two pounds, requires to move over one. All machines, no matter how complex and intri- cate their construction, may be reduced to one or more of six simple machines, or elements, which we call the 214 THE LEVEE. Mechanical Powers. The simple machines, six in number, are usually denominated the lever, inclined plane, wheel and axle, pulley, screw, and wedge. The wheel and axle is, however, a revolving lever, the screw a revolving inclined plane, and the wedge a double inclined plane, thus reducing them to three in number, viz. : lever, inclined plane, and pulley. All these machines act on the same fundamental principle of virtual velocities ; accordingly, the weight multiplied into the space it moves through is equal to the power multiplied into the space it moves through. This is the general law which determines the equi- librium of all machines ; and keeping this principle in mind, there will be no difficulty in solving any of the propositions appertaining to the simple machines. In all machines, a portion of the eifect is lost in overcoming the friction of the working parts ; but, in making calculations upon them, it is made first as though no friction existed, a deduction being after- wards made. And so also we have to assume a per- fection in the machine itself which does not exist; that is to say, the inclined plane, screw, wedge, &c., to be a perfectly smooth hard inflexible substance, and the rope of the pulley, and wheel and axle, to be perfectly flexible and non-elastic, conditions, for which allowance has to be made after the calculation is completed. Lever. Of the lever there are three orders, as shown respectively by the figures 1, 2, 3. THE LEVEE. 215 J. X Tig". 2 3 o- . 3 W = weight, P = power, F = fulcrum. EXAMPLE 1. Given the Weight W = 1000 Ibs., required the power P, the lengths of the arms re- spectively as marked in the figures ? A^s. 1. P X 3 = 1000 X 1 3P = 1000 P = 333^ Ibs. Am 2. P x 4 = 1000 X 1 4P = 1000 P = 250 Ibs. . 3. P X 1 = 1000 X 4 P = 4000 Ibs. EXAMPLE 2. Given a compound lever with lengths < 2 ) and weight as marked in fig. 4, required the power P. 216 THE LEVER. p x 16 = 1000 X 4 Up = 4000 p = 250 Ibs. = weight required at p, supposing there to be but one lever therefore P x 10 = 250 X 2 10P = 500 P = 50 Ibs. Or, 1000 x4x2 = PxlOxl6 8000 160P P = 50 EXAMPLE 3. Given, as per figure 5, a safety valve 100 sqr. ins. area 20 Ibs. per sq. in. pressure 2000 Ibs. total pressure. 100 sq. ins. area, subject to a pressure per square inch above the atmosphere of 20 Ibs., lengths of the long and short arms of the lever as shown in the figure, required the weight W to balance the pressure on the valve ? W x 25 = 100 X 20 X 5 25W = 10000 W = 400 Ibs. - EXAMPLE 4. Suppose, in example 3, the valve and stem should weigh 20 Ibs., and the lever, which is uniform throughout its length, weigh 2 5 Ibs., what would be the weight W, in that case, to balance the same pressure of steam ? The valve and stem being 5 inches from the ful- crum, act with a leverage of 5 inches, but the lever being uniform, its action is the same as though the INCLINED PLANE. 217 whole weight was concentrated at x (the centre of gravity) half way of its length. Wherefore W X 25 + 20 X 5 + 25 x 12.5 = 100 X 20 X 5 25W + 100 + 312.5 = 10000 25 W = 10000 -412.5 W = 383.5 Ibs. the re- quired weight. Practically, the pressure a safety valve lever ex- erts on the valve can be-ascertained by fixing it in its place, and attaching a spring balance to the pin hole immediately over the valve. If the valve and weight be also attached, the balance will indicate the total pressure which tends to keep the valve in its seat, which pressure being divided by the number of square inches in the valve, will give the pressure per square inch at which steam will commence to blow off. Inclined Plane. Ex. 1. Weight W 500 Ibs., length, and height of the plane, as per figure 6, 20 and 9 ins. respectively, required the pow- er P? Considering the weight W to be started at the base of the plane and rolled up to the top, it will travel vertically the height of the plane, (9 inches), while the power, P, will descend a distance equal to the length of the plane (20 ins.), therefore, according to the principle of virtual velocities, P x 20 = 500 X 9 TF" H o 20P =i 4500 P = 225 Ibs. Ex. 2. Length and height of the plane as per fig. 7, weight 500 pounds, required the 218 INCLINED PLANE. power P applied in a line with the base of the plane ? In this case, when the weight will have risen from the base to the top of the plane, 9 ins., the distance descended by P will manifestly not be equal to the length but to the base. Wherefore P X 3* = 500 X 9 17.86P = 4500 P = 251.96 - Ibs. In order to establish Equilibrium between the weight and power, this calculation is also applicable when the power is applied in the di- rection of the base as shown in dots, figure 7. If the power be applied at an angle with the plane, as C A, figure 8, in order to ascertain the proportion of weight to the power, to establish equilibrium, we proceed thus : Draw CD, the vertical of the centre of gravity of the weight, of any convenient length ; CE, at right angles to BE, and DE parallel to AC. CD can represent the length of the plane, and DE the height. Where- fore Weight x DE = Power x CD Power = Weight x DE CD ~ Geometrically, the angles BC and CDE, from the construction of the figure, can be demonstrated to be equal, and also ECD, and BEG ; from which, knowing the lengths of two legs of the triangle BEG, WHEEL AND AXLE. 219 and the angle G, to be a right angle, the lengths of the lines CD ED can be determined. Wheel and Axle. In the wheel and axle, when the power is applied tangentially to the wheel, W X radius of axle = P x radius of wheel W x diameter of axle = P x diameter of wheel W x circumference of axle = P x circum. of wheel. When the power is v not applied ^ \ tangentially to the wheel, but in the [\ C^\ direction shown in fig. 9, the length W J of the line ab at right angles to the ^V^_-Xl, power will give the leverage of the \ power, hence *\ W x radius of axle = P x ab. . 9. J "5" o Pulley. If a cord be pulled at one end the ten- sion throughout its whole length must be alike. Taking figure 10, and supposing the power to be 1, the tension throughout the entire length of the cord will be 1, but as there are two parts of the cord supporting the lower block, the weight must be 2. The pressure on the fulcrum or support must be always equal to the weight, plus the power. If there be more than one support, the sum of the pressures on them will be equal to the sum of the weight and power. Or, in figure 10, according to the principle of virtual velocities, the weight is double the power, because the power must descend 2 feet for every foot ascent of the weight. TF} 220 THE PULLEY. J- 2 2 2 2 ~T7 The numbers above the top blocks in all the ex- amples of pulleys here shown represent the pressure on the supports. In fig. 11, the power and weight are as 1 to 8, because the power supports 4 weights, each one double its size. In fig. 12 the tension on the 1st cord is 1 ; on the 2d 2 ; 3d 4 ; 4th 8 ; 5th 16 ; and as there are 2 parts of the cord hav. ing a tension of 16, the weight to establish equi- librium, must be 32. In fig. 13 the weight to the power is as 3 to 1, there being 3 parts of the cord having a tension of 1 supporting the weight. THE PULLEY. 221 In fig. 14 the power to the weight is as 1 to 12, the power being multiplied four times by the application of the second set of pul- leys, or luff-tackles, as they are technically termed. In fig. 15 the power is to the weight as 1 to 12, the tension throughout the first cord being 1 ; the sec- ond cord 2 ; third 5, and as there are two parts of the cord hav- ing a tension of 5, and one part of the cord having a tension of 2, supporting the weight, if all the cords be supposed parallel, the weight must be the sum of these, or 12. In fig. 16 the power to the weight is as 1 to 4. In figure 1Y, where the power is applied at an angle, we ascer- tain the proportion of the weight and power thus: Draw AD, of any convenient length^ and from the point A draw AB parallel to rig-, 222 THE PULLEY. Cc and AC parallel to B5. The power and weight will be re- spectively as the lengths of the lines DC or DB and AD. Tig. 16 From which it ^ill be seen that the greater the angle CDB the longer will be the line DC or DB, and hence the greater the power. So that the weight of the line itself will be sufficient to prevent any powei whatever from drawing it mathematically straight. QUESTION. In figure 18, two blocks of granite, joined together as shown, are laid upon a horizontal plane ; required their relative sizes in order that they may commence at the same time to move, and con- tinue to move with equal velocity ? A^s. 2 to 1, because the larger block is supported by two parts of the cord, and has in consequence, double the force exerted upon it of the smaller block. THE SCREW. 223 Screw. In the screw, like all other simple ma- chines the power x space moved through = weight X space moved through. Ex. Length of lever 20 ins., pitch of screw inch, weight 500 Ibs., re. quired the power P at the end of the lever ? ANS. Px 20x2x3.1416 = 500 X T 125.664P = 250 P = 1.989 Ibs. The screw is simply a revolving inclined plane, the power being applied parallel to the base of the plane, which is repre- sented by the circumfer- ence described by P, and the height of the plane by the pitch of the screw. Fig. 20 is a compound screw. The upper screw AA is fitted to the thread in the nut B which re- mains fixed. The cylin- der AA being hollow has another screw C, of a finer thread, fitting into it The nut D is fixed, al- lowing C to slide up and down within it, without 224 THE WEDGE. turning. By this arrangement it will be seen, that when the screw A A is turned once round, the distance ascended by the weight will not be equal to the pitch of A A, but the difference between the pitch of A A andC. EXAMPLE. Pitch of AA ^ inch, of C T 7 T inch, weight 16000 Ibs., required the power P, applied 20 inches from the centre ? P x 20 X 2 X 3.1416 = 16000 X T V - T V 125.634P = 1000 P = 7.957 Ibs. In order to multiply the power the same number of times with a single screw, the pitch would have to be T ! T inch, which would render the thread too weak to withstand a heavy pressure. Wedge. Let WW, fig. 21, be two weights of 1000 Ibs. each, rest- ing upon a horizontal rig- 21 pl ane ? ^quired the power to be applied at P, to the wedge, having the dimensions shown in the figure to o to separate them ? P X 20 = 1000 X 2 20P = 2000 P = 100 Ibs. Because, when the power P has descended to the point A, the weights have been separated 2 inches while the power has travelled 20 inches, the length of the wedge. GKAVITY. 225 Cenfre of Gravity. The centre of gravity of a cone from the vertex equals f- the axis. In a paraboloid, the distance from vertex equals -J the axis. In a parabolic space, equals f the axis from the vertex. In a triangle, equals f the axis from the vertex. Centre of Pressure. The centre of pressure of a parallelogram, when the upper surface is level with the water, = ^ from the bottom ; of a right-angled triangle with the base down = | from the bottom, measured on the perpendicular line B C ; with the base up = ^ B C. See Hanris Mechanics. Semi-parabolic plane. FOKMULA : m = centre of pressure, o m =. -f- of a c, m n = -fV of a d. Gravity. The spaces described by a body acted upon freely by gravity are as the squares of the times ; i. e., a body falling 2 seconds, will describe 4 times the distance of 226 GRAVITY. a body falling one second. Hence, in order to ascer- tain the distance fallen by a body, it is only necessary to multiply the square of the number of seconds by the distance fallen in the first second ; the product will be the total distance fallen. All bodies fall with the same velocity in vacuo, namely, 16.08 feet in the first second, having a velocity of 32.166 feet at the end of the second. Where the atmosphere is interposed, the velocity will be some- what less, say for heavy bodies, such as the metals, 16 feet for the first second. EXAMPLE. Which will strike with the greater effect, a weight of 200 Ibs., falling through 144 ft., or 100 Ibs. falling through 256 feet ? The velocity of a body at the end of a fall is equal to the number of seconds it is falling, multiplied into (32 feet) the velocity at the end of the first second, and the momentum of a body is equal to the weight multiplied into the velocity. We have, then, first to find the velocity, and afterwards the momentum. v/16 : 1 : : ^144 : 3 seconds time of falling of 200 Ib. ^16 : 1 : : v/256 : 4 " " " 100 Ib. 32 x 3 = 96 ft. per second velocity at end of fall of 200 Ib. weight. 32 X 4 = 128 ft. per second velocity at end of fall of 100 Ib. weight. 96x200=19200= momentum of the 200 Ib. weight, 128x100=12800= momentum of the 100 Ib. weight. 6400= difference, which is 33| per cent, of the larger number. DISPLACEMENT OF FLUIDS. 227 Centre of Gravity of Several Bodies taken together. Suppose there be several weights placed as follows in the same plane, required the centre of gravity of them all taken together ? Cylinder. Air-pump. Shaft. Boilers. Tons. Tons. Tons. Tons. 5 2 10 30 < 8ft. X 10ft x 20ft. > a to Assume a point (&), at any distance (say 2 feet) from either of the extreme weights, and multiply each weight separately by its distance from this point ; the sum of these products, divided by the sum of the weights, will be the distance of the centre of gravity from the assumed point. Thus : 80 X 2 = 60 10 X 22 = 220 2 X 32 = 64 5 x 40 = 200 47 ) 544 (11.57 ft. = centre of gravity from the point #, or 9.57 feet from the boilers towards the shaft. Displacement of Fluids. Solid bodies immersed in fluids will displace an amount of the fluid equal to their own weight. If the specific gravity of the body be greater than that of the fluid, it will sink ; otherwise it will float. EXAMPLE. Eequired the distance a cube of cherry, one foot high, will sink in fresh water? The specific gravities of fresh water and cherry are relatively as 1.00 to .606 ; the cherry will therefore sink ,606 feet. 228 FORCE, TEMPER ATTIRE, AND VOLUME OF STEAM. Table of the Elastic Force, Temperature, and Volume of Steam, from a Temperature of 80 to 387.3, and from a Pressure of one to 410 Inches ol Elastic force in Tempera- ture. Volume. Elastic force in Tempera- ture. Volume. inches of mercury. pounds per sq. inch. inches of mercury. >ounds per sq. inch. 1 .49 80 41031 53.04 26 243.3 10<)7 1.17 .573 85 35393 55.08 27 245.5 973 1.36 .666 90 30425 57.12 28 247.6 941 1.58 .774 95 26686 59.16 29 249.6 911 1.86 .911 100 22873 61.2 30 251.6 883 2.04 103 20958 63.24 31 253.6 857 2.18 .068 105 19693 65.28 32 255.5 833 2.53 .24 110 16667 67.32 33 257.3 810 2.92 .431 115 14942 69.36 34 259.1 788 3.33 .632 120 13215 71.4 35 260.9 767 3.79 .857 125 11723 73.44 36 262.6 748 4.34 2.129 130 10328 75.48 37 264.3 729 5 2.45 135 9036 77.52 38 265.9 712 5.74 2.813 140 7938 79.56 39 267.5 695 6.53 3.1 145 7040 81.6 40 269.1 679 7.42 3.636 150 6243 83.64 41 270.6 664 8.4 4.116 155 5559 85.68 42 272.1 649 9.46 4.635 160 4976 87.72' 43 273.6 635 10.68 5.23 165 4443 89.76 44 276 622 12.13 5.94 170 3943 91.8 45 276.4 610 13.62 6.67 175 3838 93.84 46 277.8 598 15.15 7.42 180 3208 ' 95.88 47 279.2 586 17 8.33 185 2879 97.92 48 280.5 573 19 9.31 190 2595 99.96 49 281.9 564 21.22 10.4 195 2342 102 50 283.2 554 23.64 11.58 200 2118 104.04 51 284.4 544 26.13 12.7 205 1932 106.08 52 285.7 534 28.84 14.13 210 1763 108.12 53 286.9 525 29.41 14.41 211 1730 110.16 54 288.1 516 30 14.7 212 1700 112.02 55 289.3 508 30.6 15 212.8 1669 114.24 56 290.5 500 31.62 15.5 214.5 1618 116.28 57 291.7 492 32.64 16 216.3 1573 i 118.32 58 292.9 484 33.66 16.5 218 1530 120.36 59 294.2 477 34.68 17 219.6 1488 122.4 60 295.6 470 35.7 17.5 221.2 1440 124.44 61 296.9 463 36.72 18 222.7 1411 126.48 62 298.1 456 37.74 18.5 224.2 1377 128.52 63 299.2 449 38.76 19 225.6 1343 130.56 64 300.3 443 39.78 19.5 227.1 1312 132.62 65 301.3 437 40.80 20 228.5 1281 134.64 66 302.4 431 41.82 20.5 229.9 1253 136.68 67 303.4 425 42.84 21 231.2 1225 138.72 68 304.4 419 43.86 21.5 232.5 1199 140.76 69 305.4 414 44.88 22 233.8 1174 142.8 70 306.4 408 45.90 22.5 235.1 1150 144.84 71 307.4 403 46.92 23 236.3 1127 146.88 72 308.4 398 46.94 23.5 237.5 1105 148.92 73 309.3 393 48.96 24 238.7 1084 150.96 74 310.3 388 49.98 24.5 239.9 1064 153.02 75 311.2 383 51. 25 241 1044 J 155.06 76 312.2 379 FORCE, TEMPERATURE, AND VOLUME OF STEAM. 220 Elastic force in Tempera- Elastic force in Tempera- inches of pounds per ture. V OlUID6. inches of pounds per ture. Volume. mercury. sq. inch. mercury. sq. in. 157.1 77 313.1 374 254.99 125 349.1 240 159.14 78 314 370 265.19 130 352.1 233 161.18 79 314.9 366 275.39 135 355 224 163.22 80 315.8 362 285.59 140 357.9 218 165.26 81 316.7 358 295.79 145 360.6 210 167.3 82 317.6 354 306 150 363.4 205 169.34 83 318.4 350 316.19 155 366 198 171.38 84 319.3 346 326.39 160 368.7 193 173.42 85 320.1 342 336.59 165 371.1 187 183.62 90 324.3 325 346.79 170 373.6 183 193.82 95 328.2 iSlO 357 175 376 178 203.99 100 332 295 367.2 180 378.4 174 214.19 105 335.8 282 377.1 185 380.6 169 224.39 110 339.2 271 387.6 190 382.9 166 234.59 115 342.7 259 397.8 195 384.1 161 244.79 120 345.8 251 408 200 387.3 158 PUBLICATIONS, FROM THE PRESS OF D. YAN HOSTBAND, 192 BROADWAY, (UP STAIRS,) NEW YORK. A large Stock of English, French, and American Military Worlcs, constantly on hand. Copies of any of these Books sent free by mail on receipt of the Catalogue price. D. Van Nbstrand's Publications. Hand- Book of Artillery, For the Service of the United States Army and Militia. New and revised edition. By Maj. JOSEPH HOBEKTS, U. S. A. 1 vol. 18mo, cloth, New arid enlarged edition. $1 00. " A complete catechism of gun practice, covering the whole ground of this branch of military science, and adapted to militia and volunteer drill, as -well as to the regular army. It has the merit of precise detail, even to the technical names of all parts of a gun, and how the smallest operations connected with its u&e can be best performed. It has evidently been prepared with great care, and with strict scientific acciiracy. By the recommendation of a committee appointed by the commanding officer of the Artillery School at Fort Monroe, Ya., it has been substituted for ' Burns' Questions and Answers,' an English \vo;k which has heretofore been the text-book of instruction in this country." Ntw Yoi-k Century. New Infantry Tactics, For the Instruction, Exercise, and Manoeuvres of the Soldier, a Com- pany, Line of Skirmishers, Battalion, Brigade, or Corps d'Armee. By Brig. -Gen. SILAS CASEV, U. S. A. 3 vols. 24mo. Halt roan, lithographed plates. $2.50. VOL. I. School of the Soldier ; School of the Company ; In- struction for Skirmishers. VOL. II. School of the Battalion. VOL. III. Evolutions of a Brigade ; Evolutions of a Corps d'Armee. The manuscript of this new system of Infantry Tactics was carefully ex- amined by General MCLEI,LAN, and met with his unqualified approval, which be has since manifested by authorizing General CASEY to adopt it for his entire division. The author has retained much that is valuable contained in the sys- tems of SCOTT and HAKDEE, but has made many important changes and addi- tions which experience and the exigencies of the service require. General CASEY'S reputation as an accomplished soldier and skilful tactician is a guar- antee that the work he has undertaken has been thoroughly performed. "These volumes are based on the French ordonnances of 1831 and 1845 for the manoeuvres of heavy infantry and chatweurs d pied ; both of these systems have been in use in our service for some years, the former having been trans- lated by Gen. Scott, and the latter by Col. Hardee. After the introduction of the latter drill in our service, in connection with Gen. Scott's Tactics, there arose the necessity of a uniform system for the manoeuvres of all the infantry arm of the service. These volumes are the result of the author's endeavor to communicate the instruction, now used and adopted in the army, to achieve this result." Boston Journal. " Based on the best precedents, adopted to the novel requirements of the art of war, and very full in its instructions, Casey's Tactics will be received as the most useful and most comprehensive work of its kind in our language. From the drill and discipline of the individual soldier, or through all the various combinations, to the manoeuvres of a brigade and the evolutions of a Corps D'Armee, the student is advanced by a clear method and steady progress. Nu- merous cuts, plans, and diagrams illustrate positions and movements, and de- monstrate to the eye the exact working out of the individual position, brigading, order of battle, &c., &c. The work is a model of publishing success, being in three neat jwcket volumes." Jfew Yorker. r~ D. Van Nostrand 's Publications. Gunnery Instructions. Simplified for the Volunteer Officers of the U. S. Navy, with hints to Executive and other Officers. By Lieut.-Commander EDWARD BARRETT, U. S. N., Instructor in Gunnery, Navy Yard, Brook- lyn. Third edition, revised and enlarged. 1 vol. 12mo, cloth. $1 25. "It is a thorough work, treating plainly on its subject, and contains also some valuable hints to executive officers. No officer in the volunteer navy should be without a copy." Boston Evening Traveller. "This work contains detailed and specific instructions on all points connected with the use and management of guils of every kind in the naval service. It has full illustrations, and many of these of the most elementary character, especially designed for the use of volunteers in the navy. The duties of executive officers and of the division officers are so clearly set forth, that ' he who runs may read 1 and understand. The manual exercise is explicit, and rendered simple by dia- grams. Forms of watch and quarter bills are given; and at the close there is a table of ranges according to the kind and calibre of gun, the weight of the ball, and the charge of powder. A valuable little hand-book." Philadelphia In- quirer. "I have looked through Lieut. Barrett's book, and think it will be very valu- able to the volunteer officers who are now in the naval service. "C. K. P. RODGERS, Commanding U. S. Steam Frigate Wabash." The " C. S. A." and the Battle of Bull Run. (A Letter to an English Friend.) By J. G. BARNARD, Major of Engi- neers, U. S. A., Brigadier-General, and Chief Engineer, Army of the Potomac. With five maps. 1 vol. 8vo, cloth. $1 50. " This book was begun by the author as a letter to a friend in England, but as he proceeded and his MSS. increased in magnitude, he changed his original plan, and the book is the result General Burnard gives by far the best, most compre- hensible and complete account of the Battle of Bull Run we have seen. It is il- lustrated by some beautifully drawn maps, prepared for the War Department by the topographical engineers. He demonstrates to a certainty that but for the causeless panic the day might not have been lost. The author writes with vigor and earnestness, and has contributed one of the most valuable records yet pub- lished of the history of the war." Boston Commercial Bulletin. Models of Fortifications. Vauban's First System One Front and two Bastions ; Scale, 20 yards to an inch. The Modern System One Front ; Scale 20 yards to an inch. Field- Works The Square Redoubt; Scale. 5 yards to an inch. Mr. Kimber's three volumes, viz. Vauban's First System, The Modern System, and Field- Works, will accompany the Models. Price for the Set of Three, with books, $60. _J />. Van Nostrand^s Publications. Rifles and Rifle Practice. An Elementary Treatise on the Theory of Rifle Firing ; explain- ing the causes of Inaccuracy of Fire and the manner of cor- recting it ; with descriptions of the Infantry Rifles of Europe and the United States, their Balls and Cartridges. By Capt. C. M. WILCOX, U. S. A. New edition, with engravings and cuts. Green cloth. $1.75. "Although eminently a scientific work, special care seems to have been taken to avoid the use of technical terms, and to make the whole subject readily comprehensible to the practical enquirer. It was designed chiefly for tho uso of Volunteers and Militia; but the War Department has evinced its ap- proval of its merits by ordering from the publisher one thousand copies, for the " use of the United States Army." Louisville Journal. 'The book will be found intensely interesting to all who are watching the changes in the art of war arising from the. introduction of the new rifled arms. We recommend to our readers to buy the book." Military Gazette. " A most valuable treatise.' 1 New York Herald. " This book is quite original in its character. That character is complete- ness. It renders a study of most of the works on the rifle that have been published quite unnecessary. We cordially recommend the book. 1 " United Service Gazette, London. 'The work being in all its parts derived from the best sources, is of tho highest authority, and will be accepted as the standard on the subject of which it treats.'' New Yorker. Army Officer's Pocket Companion. Principally designed for Staff Officers in the Field. Partly trans- lated from the French of M. DE ROCVRE, Lieutenant-Colonel of the French Staff Corps, with Additions from Standard Amer- ican, French, and English Authorities. By WM. P. CRAIGHILL, First Lieutenant U. S. Corps of Engineers, Assist. Prof, of Engineering at the U. S. Military Academy, West Point. 1 vol. 18mo. Full roan. $1.50. " I have carefully examined Capt. CRAIGHTLL'S Pocket Companion. I find it one of the very best works of the kind I have ever seen. Any Army or Volunteer officer who will make himself acquainted with the contents of this little book, will seldom be ignorant of his duiies in camp or field. 1 ' H. W HALLECK, Major-General U. S. A. " I have, carefully examined the ' Manual for Staff Officers in the Field. 1 It is a most invaluable work, admirable in arrangement, perspicuously written, abounding in most useful matters, and such a book as should be the constant pocket companion of every army officer, Regular and Volunteer" G. W. CULLUM, Brigadier-General U. S. A. Chief of General Halleck's Staff, Ch r ef Engineer Department Mississippi "This little volume contains a large amount of indispensable information relating to officers 1 duties in the siege, camp, and field, and will prove to them a most valuable pocket companion. It is illustrated with plans and drawings." Boston Com. Bulletin. D. Van Nostran&s Publications. Nautical Routine and Stowage, With Short Rules in Navigation. By JOHN McLEOD MURPHY, and WM. N. JEPFERS, Jr., U. S. N. 1 vol. 8vo, cloth. $2 50. Union Foundations. A Study of American Nationality, as a Fact of Science. By Major . E. B. HUNT, Corps of Engineers, U. S. A. 1 vol. 8vo, paper. 30 cents. Standing Orders of the Seventh Reg- iment, National Guard. For the Regulation and Government of the Regiment in the Field or in Quarters. By A. DURYEE, Colonel. New edition. Flexible cloth. 40 cents. "This, which is a new edition of a popular work, cannot fail to be eagerly Bought after, ns presenting clearly and succinctly the principles of organization and discipline of a most favorite corps. An appropriate index facilitates refer- ence to the matter of the volume." New Yorker. The Automaton Regiment; Or, Infantry Soldiers' Practical Instructor. For all Regimental More- ments in the Field. By G. DOUGLAS BREWERTON, U. S. A. Neatly put up in boxes, price $1 ; when sent by mail, $1 40. The "Automaton Regiment" is a simple combination of blocks and counters, so arranged and designated by a carefully considered contrast of colors, that it supplies the student with a perfect miniature regiment, in which the position in the battalion of each company, and of every officer and man in each division, com* pany, platoon, and section is clearly indicated. It supplies the studious soldier with the means whereby he can consult his "tactics, and at the same time join practice to theory by manoeuvring a mimic regiment. The Automaton Company; Or, Infantry Soldiers' Practical Instructor. For all Company Move- ments in the Field. By G. DOUGLAS BREWERTON, U. S. A. Price in boxes, $1 25 ; when sent by mail, $1 95. The Automaton Battery; Or, Artillerists' Practical Instructor. For all Mounted Artillery Ma- noeuvres in the Field. By G. DOUGLAS BREWERTON, U. S. A. Price in boxes, $1 ; when sent by mail, $1 40. D. Van Nostrand's Publications. Siege of Bomarfimd (1854). Journals of Operations of the Artillery and Engineers. Published by permission of the Minister of War. Illustrated by imps and plans. Translated from the French by an Army Officer. 1 vol. 12mo, cloth. 75 cents. "To military men this little volume is of special interest. It contains a translation by an officer of the United States Army, of the journal of operations by the artillery and engineers at the siege of Bomarsund in 1854, published by permission of the French Minister of War in the Journal de Artite* special?* et del Etat Major. The account of the same successful attack, given by Sir Howard Douglas in the new edition of his work on Gunnery, is appended -and the narrative is illustrated by elaborate maps and plans." Jfetc York Paper. Lefsons and Pradical Notes on Steam, The Steam-Engine, Propellers, &c., &c., for Young Marine Engi- neers, Students, and others. By the late W. R. KING, U. S N. Revised by Chief-Engineer J. W KING, U. S. Navy. Fifth edition, enlarged. 8vo, cloth. $2.00 "This is the second edition of a valuable work of the late W E KINO U. S. N. It contains lessons and practical notes on Steam and the Steam- Engine, 1 ropellers, &c. It is calculated to be of great use to young marine en- gineers, students, and others. The text is illustrated and explained by numerous diagrams and representations of machinery. This new edition has been revised an .I enlarged by Chief Engineer J. W. KING. U. S. N., brother to the deceased author ofthe work." Barton Daily Advertiser. "This is one ofthe best, because eminently plain and practical, treatises on the Steam-Engine ever published."/ hiladelphia Press. "Its re-publication at this time, when so many young men are entering the service as naval engineers, is most opportune. Each of them ought to have a copy." Philadelphia Evening Bulletin. Manual of Internal Rules and Reg- ulations for Men-of-War. By Commodore U. P. LEVY, U. S. N., late Flag-officer command- ing U. S. Naval Force in the Mediterranean, &c. Flexible bine cloth. Second edition, revised and enlarged. 50 cents. "Among the professional publications for wh r ch we are indebted to the war, we willingly give a prominent place to this useful little Manual of Rules and Regulations to be observed on board of ships of war. Its authorship is a suffi- cient guarantee for its accuracy and practical value ; and as a guide to young officers in providing for the discipline, police, and sanitary government of the vessels under their command, we know of nothing superior." N. Y. Herald. "Should be in the hinds of every Nival o^cer. of whatever grade, and will not come amiss to any intelligent mariner.' 1 Boston Traveller. "A work which will pro-e of i'rent utilitv. in both the Naval service and the mercantile marine." Baltimore American. D. Van Nostranfrs Publications. A Treatife on Ordnance and Naval Gunnery. Compiled and arranged as a Text-Book for the U. S. Naval Acad- emy, by Lieutenant EDWARD SIMPSON, U. S. N. Second edi- tion, revised and enlarged. 1 vol. Svo, plates and cuts, half morocco. $5. "As the compiler has charge of the instruction In Naval Gunnery at the Naval Academy, his work, in the compilation of which he has consulted a large number of eminent authorities, is probably well suited for the purpose designed by it n-unely, the circulation of information which many officers, owing to constant service afloat, may not have been able to collect. In simple and plain language it gives instruction as to cannon, gun carriages, gun powder, projectiles, fuzes, locks, and primers; the theory of "pointing guns, rifles, the practice of gunnery, and a great variety of other sim lar matters, interesting to fighting men on sea and land." Washington Daily Globe. " A vast amount of information is conveyed in a readable and familiar form. The illustrations are excellent, and many of them unique, being colored or bronz"d so as (o represent various military arms, &c., with more than photo- graphic literaluess." Washington Star. "It is scarcely necessary for us to say that a work prepared by a writer so practically conversant with all the subjects of which he treats, and who has ouch a reputation for scientific ability, cannot fail to take at once a high place among the text-books of our naval service. It has been approved by the Secretary of the Navy, and will henceforth be one of the standard authorities on all matters connected with Naval Gunnery." New York Herald. "The book itself is admirably arranged, characterized by great simplicity and clearness, and certainly at this time will be a most valuable one to officers of the Navy/' Boston Commercial Bulletin. "Originally designed as a text-book, it is now enlarged, and so far modified in its plan as to make it an invaluable hand-book for the naval officer. It is comprehensive preserving the cream of many of the best books on ordnance and naval gunnery .and is printed and illustrated in the most admirable man- ner." New York World. Elementary Instruction in Naval Ordnance and Gunnery. By JAMES H. WARD, Commander U. S. Navy, Author of " Naval Tactics," and "Steam for the Million." New edition, revised and enlarged. Svo. Cloth, $2. " It conveys an amount of information in the same space to be found no- where else, and given with a clearness which renders it useful as well to tho general as the professional inquirer."^. Y. Evening Post. " This volume is a standard treatise upon the subject to which it is devoted. It abounds in valuable information upon all the points bearing upon Naval Gunnery." Jf. Y. Commercial Advertiser. "The work is an exceedingly valuable one, and is opportunely issued." Boston Journal. D. Van Nbstrand's Publications. Sword-Play. THE MILITIAMAN'S MANUAL AND SWORD-PLAY WITHOUT A MASTER. Rapier and Broad-Sword Exercises copiously Explained and Illustrated ; Small- Arm Light Infantry Drill of the United States Army ; Infantry Manual of Percussion Mus- kets ; Company Drill of the United States Cavalry. By Major M. W. BERRIMAN, engaged for the last thirty years in the prac- tical instruction of Military Students. Second edition. 1 vol. 12mo, red cloth. $1. "Captain Berriman has had thirty years' experience in teaching military students, and his work is written in a simple, clear, and soldierly style. It is illustrated with twelve plates, and is one of the cheapest and most complete works of the kind published in this country." Jfew York World. " This work will be found very valuable to all persons seeking military in- struction; but it recommends itself most especially to officers, and those who have to use the sword or sabre. We believe it is the only work on the. use of the sword published in this country." New York Tablet. " It is a work of obvious merit and value." Boston Traveller. Military Law and Courts Martial, By Capt. S. V. BENET, U. S. Ordnance, Asst. Prof, of Ethics in the United States Military Academy. 1 vol. 8vo. Law sheep, ,f 3.BP. The Artillerift's Manual: Compiled from various Sources, and adapted to the Service of the United States. Profusely illustrated with woodcuts anil engrav- ings on stone. Second edition, revised and corrected, with valuable additions, By Capt. JOHN GIBBON, U. S. Army. 1 vol. 8vo, half roan, $5 ; This book is now considered the standard authority for that particular branch of the Service in the United States Army. The War Department, at Washing- ton, has exhibited its thorough appreciation of the merits of this volume, the want of which has been hitherto much felt in the service, by subscribing for 700 copies. "It is with great pleasure that we welcome the appearance of a new work on this subject, entitled 'The Artillerist's Manual, 1 by Capt. John Gibbon, a highly scientific and meritorious officer of artillery in our regular service. The work, an octavo volume of 500 pages, in larse, clear type, appears to be well adapted to supply just what has been heretofore needed to fill the gap between the simple Manual and the more abstruse demonstrations of the science of gun- uery. The whole work is profusely illustrated with woodcuts and engravings on stone, tending to give a more complete and exact idea of the various matters described in the text. The book may well be considered as a valuable and im- portant addition to the military science of the country," New York Herald. UNIVEESITY OF CALIFORNIA LIBRARY, BERKELEY THIS BOOK IS DUE ON THE LAST DATE STAMPED BELOW Books not returned on time are subject to a fine of 50c per volume after the third day overdue, increasing to $1.00 per volume after the sixth day. Books not in demand may be renewed if application is made before expiration of loan period. JAN 33 1943 JUN261962 REC'D LI OCT SEP 1 REC.C1R.SEP 4*78 20m-ll,'20 ~^WM : :