Knowledge (XXG)

Klimov M-120

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bomber in November 1940. It was submitted for its State acceptance trials in August 1941, but the main connecting rod and the supercharger both broke down and the tests were not completed. The project was cancelled in 1942.
131:. It began development in 1938 and manufacture of five prototypes began in late 1939. The first prototype was completed on 30 October 1939 and began bench tests the next year. Two M-120TKs were flown in a prototype 368: 566: 336: 571: 361: 354: 288: 191: 31: 388: 545: 535: 446: 441: 436: 215: 411: 396: 332: 268: 107:
prototype 18-cylinder liquid-cooled inline aircraft engine designed during the early years of
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1,800 hp (1,342 kW). Version with a long shaft to the remote reduction gear.
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1600 hp, weight of 950 kg (2,094 lb), fitted with turbo-supercharger.
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1,600 hp (1,193 kW), weight of 850–895 kg (1,874–1,973 lb).
502: 224: 128: 498: 346: 484: 456: 377: 53: 350: 111:. Testing did not go well and it was cancelled in 1942. 497: 483: 455: 387: 127:in an inverted 'Y' configuration, driving a common 362: 8: 166:A 1940 project to combine the two variants. 119:The M-120 was developed by arranging three 369: 355: 347: 331:. Marlborough, Wiltshire: Crowood Press. 190:liquid-cooled, 18-cylinder, three-block 30:Liquid-cooled, 18-cylinder, three-block 305: 18: 7: 16:1940s Soviet piston aircraft engine 14: 220:54 L (3,295 cu in) 245:single stage, two-speed geared 1: 567:1940s aircraft piston engines 327:Kotelnikov, Vladimir (2005). 264:1,600 hp (1,193 kW) 329:Russian Piston Aero Engines 229:950 kg (2,090 lb) 588: 211:170 mm (6.7 in) 202:148 mm (5.8 in) 21: 289:List of aircraft engines 171:Specifications (M-120TK) 572:Klimov aircraft engines 182:General characteristics 312:Kotelnikov, pp. 145–46 178:Kotelnikov, p. 146 554: 553: 269:Compression ratio 97: 96: 579: 381:aircraft engines 371: 364: 357: 348: 342: 313: 310: 88: 78: 40: 19: 587: 586: 582: 581: 580: 578: 577: 576: 557: 556: 555: 550: 493: 479: 451: 383: 375: 345: 339: 326: 322: 317: 316: 311: 307: 302: 297: 280: 258: 249:Cooling system: 236: 184: 173: 142: 125:cylinder blocks 117: 86: 76: 39:National origin 38: 17: 12: 11: 5: 585: 583: 575: 574: 569: 559: 558: 552: 551: 549: 548: 543: 538: 533: 528: 523: 518: 513: 507: 505: 495: 494: 489: 487: 481: 480: 478: 477: 472: 467: 461: 459: 453: 452: 450: 449: 444: 439: 434: 429: 424: 419: 414: 409: 404: 399: 393: 391: 389:Piston engines 385: 384: 376: 374: 373: 366: 359: 351: 344: 343: 337: 323: 321: 318: 315: 314: 304: 303: 301: 298: 296: 293: 292: 291: 279: 276: 275: 274: 265: 257: 254: 253: 252: 246: 235: 232: 231: 230: 221: 212: 203: 194: 183: 180: 172: 169: 168: 167: 164: 161: 158: 155: 152: 149: 146: 141: 138: 116: 113: 95: 94: 89: 87:Developed from 83: 82: 79: 73: 72: 69: 65: 64: 61: 57: 56: 51: 47: 46: 41: 35: 34: 28: 24: 23: 15: 13: 10: 9: 6: 4: 3: 2: 584: 573: 570: 568: 565: 564: 562: 547: 544: 542: 539: 537: 534: 532: 529: 527: 524: 522: 519: 517: 514: 512: 509: 508: 506: 504: 500: 496: 492: 488: 486: 482: 476: 473: 471: 468: 466: 463: 462: 460: 458: 454: 448: 445: 443: 440: 438: 435: 433: 430: 428: 425: 423: 420: 418: 415: 413: 410: 408: 405: 403: 400: 398: 395: 394: 392: 390: 386: 382: 379: 372: 367: 365: 360: 358: 353: 352: 349: 340: 338:1-86126-702-9 334: 330: 325: 324: 319: 309: 306: 299: 294: 290: 287: 286: 285: 284: 283:Related lists 277: 272: 270: 266: 263: 262:Power output: 260: 259: 255: 250: 247: 244: 242: 238: 237: 233: 228: 226: 222: 219: 217: 213: 210: 208: 204: 201: 199: 195: 193: 192:inline engine 189: 186: 185: 181: 179: 177: 170: 165: 162: 159: 156: 153: 150: 147: 144: 143: 139: 137: 134: 133:Ilyushin DB-4 130: 126: 122: 114: 112: 110: 106: 102: 93: 90: 85: 84: 80: 75: 74: 70: 67: 66: 62: 59: 58: 55: 52: 50:Manufacturer 49: 48: 45: 42: 37: 36: 33: 32:inline engine 29: 26: 25: 20: 416: 328: 320:Bibliography 308: 282: 281: 267: 261: 248: 241:Supercharger 239: 223: 216:Displacement 214: 205: 196: 187: 175: 174: 121:Klimov M-103 118: 109:World War II 101:Klimov M-120 100: 98: 92:Klimov M-103 77:Number built 44:Soviet Union 503:turboshafts 256:Performance 115:Development 561:Categories 499:Turboprops 295:References 234:Components 225:Dry weight 163:M-120UV-TK 129:crankshaft 60:First run 485:Turbofans 457:Turbojets 176:Data from 68:Produced 278:See also 140:Variants 71:1939–40 546:VK-3000 541:VK-2500 536:VK-1500 526:TV7-117 521:TV3-117 516:TV2-117 511:GTD-350 157:M-120UV 151:M-120TK 531:VK-800 475:RD-500 447:VK-150 442:VK-110 437:VK-109 432:VK-108 427:VK-107 422:VK-106 378:Klimov 335:  251:liquid 207:Stroke 105:Soviet 103:was a 54:Klimov 22:M-120 491:RD-33 465:RD-45 417:M-120 412:M-110 407:M-105 402:M-103 397:M-100 300:Notes 273:6.6:1 188:Type: 145:M-120 63:1940 27:Type 501:and 470:VK-3 333:ISBN 198:Bore 99:The 81:5? 563:: 123:A 370:e 363:t 356:v 341:. 271:: 243:: 227:: 218:: 209:: 200::

Index

inline engine
Soviet Union
Klimov
Klimov M-103
Soviet
World War II
Klimov M-103
cylinder blocks
crankshaft
Ilyushin DB-4
inline engine
Bore
Stroke
Displacement
Dry weight
Supercharger
Compression ratio
List of aircraft engines
ISBN
1-86126-702-9
v
t
e
Klimov
aircraft engines
Piston engines
M-100
M-103
M-105
M-110

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