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Lorraine 12Rcr Radium

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Six engines were ordered, but it is unclear how many were completed, as the examples supplied to Bernard and Nieuport-Delage were merely empty shells for use as mock-ups. Bench testing commenced in March 1931, two months after the intended delivery to the airframe manufacturers, progressing slowly,
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The 12 Rcr was an inverted V-12 liquid-cooled engine with supercharger and reduction gearbox. Designed to deliver 2,000–2,200 hp (1,500–1,600 kW) at 4,000 rpm, the 12 Rcr had a high specific power from a displacement of only 28.7 L (1,750 cu in) and weight of 510 kg
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leading to the first delivery of a complete engine to Dewoitine in July 1931. The second engine was tested at the Lorraine plant up to 3,000 rpm, but this highlighted concerns over the airworthiness of the engine, which was rejected for flight use. Once
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by winning the competition three times consecutively. Despite this desire, success for French aircraft was not forthcoming. To help address shortcomings, the
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had permanently secured the Schneider Trophy, further development of the Schneider racers and their specialised engines was abandoned.
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Rateau mechanical two-stage supercharger with a hydromechanical drive running at 7:1 crankshaft speed.
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From the first Schneider Trophy race in 1913, France had a deep desire to fulfil the requirements of
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was an inverted liquid-cooled 60Âş V-12 piston engine, designed specifically for use by
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DOCAVIA 25 : les Moteurs Ă  pistons aeronautiques français (1900/1960) Tome II
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3 complete engines with other part-completed engines used as maock-ups
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The 12Rcr was intended to power the following racing seaplanes:
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les Moteurs à pistons aeronautiques français (1900/1960)
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1,500–1,600 kW (2,000–2,200 hp) at 4,000 rpm
446: 385: 112:service technique et industriel de l'aĂ©ronautique 30:V-12 inverted water-cooled racing piston engine 360: 8: 87:Coupe d'Aviation Maritime Jacques Schneider 367: 353: 345: 301:L'aviation - Grande EncyclopĂ©die IllustrĂ©e 308:Bodemer, Alfred; Laugier, Robert (1987). 270:Bodemer, Alfred; Laugier, Robert (1987). 178:V-12 inverted liquid-cooled piston engine 262: 252:0.3487 kg/kW (0.5733 lb/hp)} 18: 7: 338:Jane's all the World's Aircraft 1931 205:28.7 L (1,750 cu in) 16:1930s French aircraft piston engine 84:racing seaplanes competing in the 14: 94:) air races in the early 1930s. 214:510 kg (1,120 lb) dry 486:Lorraine-Dietrich aero-engines 319:Les avions Bernard: DOCAVIA 31 1: 515:Inverted V12 aircraft engines 505:1930s aircraft piston engines 321:(in French). Éd. Larivière. 531: 510:Lorraine aircraft engines 482: 299:Novara, A.A. V.V (1985). 196:145 mm (5.7 in) 187:145 mm (5.7 in) 21: 386:V- and W- piston engines 336:Grey, C.G., ed. (1931). 170:General characteristics 154:Nieuport-Delage NiD.651 90:(commonly known as the 160:Specifications (12Rcr) 98:Design and development 447:Radial piston engines 78:Lorraine 12Rcr Radium 317:Liron, Jean (1990). 122:Operational history 492: 491: 376:Lorraine-Dietrich 104:Jacques Schneider 74: 73: 51:Lorraine-Dietrich 522: 369: 362: 355: 346: 341: 332: 313: 304: 286: 285: 267: 149:Dewoitine HD.412 92:Schneider Trophy 67: 37: 19: 530: 529: 525: 524: 523: 521: 520: 519: 495: 494: 493: 488: 478: 442: 381: 373: 335: 329: 316: 307: 298: 295: 293:Further reading 290: 289: 282: 269: 268: 264: 259: 237: 221: 172: 162: 144:Bernard H.V.220 137: 124: 100: 65: 36:National origin 35: 17: 12: 11: 5: 528: 526: 518: 517: 512: 507: 497: 496: 490: 489: 483: 480: 479: 477: 476: 471: 466: 461: 456: 450: 448: 444: 443: 441: 440: 435: 430: 425: 420: 415: 410: 405: 400: 395: 389: 387: 383: 382: 374: 372: 371: 364: 357: 349: 343: 342: 333: 327: 314: 305: 294: 291: 288: 287: 281:978-2862482279 280: 261: 260: 258: 255: 254: 253: 248:Specific power 244: 236: 233: 232: 231: 220: 217: 216: 215: 206: 197: 188: 179: 171: 168: 161: 158: 157: 156: 151: 146: 136: 133: 123: 120: 99: 96: 72: 71: 68: 62: 61: 58: 54: 53: 48: 44: 43: 38: 32: 31: 28: 24: 23: 15: 13: 10: 9: 6: 4: 3: 2: 527: 516: 513: 511: 508: 506: 503: 502: 500: 487: 481: 475: 472: 470: 467: 465: 462: 460: 457: 455: 452: 451: 449: 445: 439: 436: 434: 431: 429: 426: 424: 421: 419: 416: 414: 411: 409: 406: 404: 401: 399: 396: 394: 391: 390: 388: 384: 380: 377: 370: 365: 363: 358: 356: 351: 350: 347: 339: 334: 330: 328:2-84890-065-2 324: 320: 315: 311: 306: 302: 297: 296: 292: 283: 277: 273: 266: 263: 256: 251: 249: 245: 242: 241:Power output: 239: 238: 234: 229: 227: 223: 222: 218: 213: 211: 207: 204: 202: 198: 195: 193: 189: 186: 184: 180: 177: 174: 173: 169: 167: 166: 159: 155: 152: 150: 147: 145: 142: 141: 140: 134: 132: 130: 129:Great Britain 121: 119: 115: 113: 109: 105: 97: 95: 93: 89: 88: 83: 79: 69: 64: 63: 59: 56: 55: 52: 49: 47:Manufacturer 46: 45: 42: 39: 34: 33: 29: 26: 25: 22:12Rcr Radium 20: 428:12Rcr Radium 427: 379:aero engines 337: 318: 309: 300: 271: 265: 246: 240: 226:Supercharger 224: 208: 201:Displacement 199: 190: 181: 175: 164: 163: 138: 135:Applications 125: 116: 111: 101: 91: 85: 77: 75: 66:Number built 408:12F Courlis 403:12E Courlis 235:Performance 60:March 1931 499:Categories 484:See also: 474:18F Sirius 433:12R Sterna 423:12H PĂ©trel 257:References 219:Components 210:Dry weight 57:First run 438:18G Orion 418:12Q Eider 165:Data from 464:9N Algol 459:7M Mizar 325:  278:  192:Stroke 82:French 41:France 176:Type: 108:STIAĂ© 27:Type 413:AM-6 323:ISBN 276:ISBN 183:Bore 76:The 469:14A 398:12D 501:: 454:5P 393:8B 110:( 368:e 361:t 354:v 331:. 284:. 250:: 228:: 212:: 203:: 194:: 185::

Index

France
Lorraine-Dietrich
French
Coupe d'Aviation Maritime Jacques Schneider
Jacques Schneider
STIAĂ©
Great Britain
Bernard H.V.220
Dewoitine HD.412
Nieuport-Delage NiD.651
Bore
Stroke
Displacement
Dry weight
Supercharger
Specific power
ISBN
978-2862482279
ISBN
2-84890-065-2
v
t
e
Lorraine-Dietrich
aero engines
8B
12D
12E Courlis
12F Courlis
AM-6

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