257:
26:
626:
619:
612:
700:
597:
583:
569:
420:
705:
275:
635:
312:
307:
285:
280:
181:
90:
679:
265:
504:
47:
324:
34:
145:
60:
460:
290:
161:
44:
374:
270:
492:
256:
593:
579:
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451:
125:
184:, but the turbocharging experiments were abandoned after the turbine failed on 4 May 1918.
638:
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70:
50:
295:
177:
153:
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223:
213:
173:
137:
399:
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197:
129:
133:
25:
206:
1917 - Main production variant, 150 horsepower (112 kW). 3,608 built.
176:
experimental version of the RAF 4, the RAF 4d, was developed using a
222:
1917 - 240 horsepower (180 kW), strengthened cylinders and enlarged
674:
659:
654:
649:
480:
255:
141:
112:
232:
1915 - 150 horsepower (112 kW), pusher version with fan-cooling.
608:
180:
exhaust-driven turbocharger. The engine was test-flown in a
564:. Cambridge, England. Patrick Stephens Limited, 1989.
323:
A preserved RAF 4a engine is on public display at the
592:. Marlborough, Wiltshire: Airlife Publishing, 2003.
620:
212:1916 - 180 horsepower (134 kW), experimental
148:but produced by the two British companies of
8:
438:163 hp (122 kW) at 1,800 rpm (takeoff power)
627:
613:
605:
352:12-cylinder, upright, 60-degree Vee engine
590:British Piston Engines and their Aircraft
404:EOI (side-valve inlet, exhaust overhead)
521:
410:Twin Claudel-Hobson Mk.1A carburettors
15:
7:
562:World Encyclopaedia of Aero Engines
238:170 horsepower (127 kW), increased
14:
260:The Royal Aircraft Factory R.E.8
24:
33:Preserved RAF 4a engine at the
140:. Based on the eight–cylinder
1:
701:1910s aircraft piston engines
276:Royal Aircraft Factory B.E.12
196:1914 - Prototype engine, 140
313:Royal Aircraft Factory F.E.4
308:Royal Aircraft Factory F.E.2
286:Royal Aircraft Factory R.E.8
281:Royal Aircraft Factory R.E.7
164:version of the same engine.
91:Royal Aircraft Factory R.E.8
722:
576:The Royal Aircraft Factory
645:
266:Armstrong Whitworth F.K.8
32:
23:
18:
578:. London: Putnam, 1990.
505:List of aircraft engines
425:0.5:1, Left-hand tractor
447:0.2 hp/cu in (9.2 kW/L)
344:General characteristics
331:Specifications (RAF 4a)
325:Science Museum (London)
216:installation. 16 built.
144:it was designed by the
35:Science Museum (London)
636:Royal Aircraft Factory
528:Gunston, 1989, p. 156.
465:0.24 hp/lb (0.4 kW/kg)
261:
146:Royal Aircraft Factory
61:Royal Aircraft Factory
546:Lumsden 2003, p. 224.
461:Power-to-weight ratio
379:806.15 cu in (13.2 L)
259:
132:engine developed for
706:V12 aircraft engines
291:Siddeley-Deasy R.T.1
475:Related development
271:Bristol F.2 Fighter
493:Rolls-Royce Falcon
487:Comparable engines
319:Engines on display
262:
86:Major applications
688:
687:
537:Hare 1990, p. 265
452:Compression ratio
242:version of RAF 5.
118:
117:
713:
629:
622:
615:
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547:
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538:
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529:
526:
370:5.51 in (140 mm)
361:3.94 in (100 mm)
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588:Lumsden, Alec.
560:Gunston, Bill.
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541:
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513:
472:
432:
414:Cooling system:
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388:680 lb (308 kg)
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321:
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574:Hare, Paul R.
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443:Specific power
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421:Reduction gear
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296:Vickers F.B.14
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154:Siddeley-Deasy
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108:Developed from
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80:December 1914
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598:1-85310-294-6
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584:0-85177-843-7
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570:1-85260-163-9
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499:Related lists
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436:Power output:
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124:is a British
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71:A.J. Rowledge
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57:Manufacturer
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639:aero engines
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554:Bibliography
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408:Fuel system:
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382:
375:Displacement
373:
364:
355:
349:
338:
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334:
322:
247:Applications
214:supercharger
174:turbocharged
171:
168:Turbocharger
157:
121:
119:
98:Number built
430:Performance
138:World War I
136:use during
51:aero engine
695:Categories
511:References
416:Air-cooled
400:Valvetrain
393:Components
384:Dry weight
198:horsepower
126:air-cooled
102:>3,600
77:First run
336:Data from
200:(104 kW).
67:Designer
470:See also
188:Variants
134:aircraft
339:Lumsden
150:Daimler
596:
582:
568:
366:Stroke
235:RAF 5b
224:valves
219:RAF 4e
209:RAF 4d
203:RAF 4a
178:Rateau
162:pusher
160:was a
156:. The
48:inline
45:Piston
19:RAF 4
680:RAF 8
675:RAF 7
670:RAF 5
665:RAF 4
660:RAF 3
655:RAF 2
650:RAF 1
516:Notes
481:RAF 1
456:4.3:1
350:Type:
302:RAF 5
252:RAF 4
229:RAF 5
193:RAF 4
182:R.E.8
158:RAF 5
142:RAF 1
122:RAF 4
113:RAF 1
41:Type
594:ISBN
580:ISBN
566:ISBN
357:Bore
240:bore
152:and
120:The
130:V12
697::
327:.
172:A
128:,
628:e
621:t
614:v
600:.
463::
454::
445::
423::
402::
386::
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359::
226:.
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