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112:. Like the other D-series engines, the cylinders had a bore of 125 mm (4.9 in) and a stroke of 120 mm (4.7 in). Power for different models was in the 100 kW-190 kW (140 hp-260 hp) range.
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119 kW (160 hp) at 2,520 rpm (take-off), 97 kW (130 hp) at 2,360 rpm (Max cruise)
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was a four-cylinder, inverted inline aircraft engine. It was first built shortly before
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Two valves per cylinder with sodium cooled exhaust valves
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194 kW (260 hp) 4D-34 with aerobatic oil system
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449:. London: Sampson Low, Marston & Company, Ltd.
458:. Wellingborough: Patrick Stephens. p. 107.
239:Four-cylinder air-cooled inverted inline engine
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49:Wings Over the Rockies Air and Space Museum
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108:, but did not enter full production until
80:Société des Avions et Moteurs Henry Potez
58:4-cyl. inverted air-cooled piston engine
330:with one pressure and two scavenge pumps
226:Jane's All The World's Aircraft 1953-54.
447:Jane's All The World's Aircraft 1961–62
438:Jane's All The World's Aircraft 1953-54
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27:1930s French piston aircraft engine
456:World Encyclopedia of Aero Engines
376:0.83 kW/kg (0.51 hp/lb) (take-off)
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445:Bridgman, Leonard, ed. (1961).
436:Bridgman, Leonard, ed. (1953).
212:S.N.C.A.C. NC-840 Chardonneret
1:
604:1930s aircraft piston engines
218:Specifications (Potez 4-D 01)
182:Morane-Saulnier MS.700 Petrel
47:A Potez 4D on display at the
535:Horizontally opposed engines
367:245 gram/hp/hour (take-off)
620:
363:Specific fuel consumption
160:194 kW (260 hp)
154:119 kW (160 hp)
148:179 kW (240 hp)
142:164 kW (220 hp)
136:179 kW (240 hp)
130:119 kW (160 hp)
124:127 kW (170 hp)
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404:List of aircraft engines
392:de Havilland Gipsy Major
231:General characteristics
599:Potez aircraft engines
454:Gunston, Bill (1986).
315:One Zenith carburettor
177:Morane-Saulnier MS.570
422:Bridgman 1953, p.328.
372:Power-to-weight ratio
272:1,207.5 mm (47.5 in)
386:Comparable engines
284:668.5 mm (26.3 in)
192:Nord 1202 Norécrin
88:Major applications
586:
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440:. London: Jane's.
354:Compression ratio
321:80 octane minimum
293:143 kg (314.6 lb)
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16:(Redirected from
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278:510 mm (20.1 in)
266:5.85 L (352 in³)
257:120 mm (4.72 in)
248:125 mm (4.92 in)
187:Max Holste MH.52
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398:Related lists
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497:aero engines
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313:Fuel system:
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262:Displacement
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171:Applications
106:World War II
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341:Performance
325:Oil system:
18:Potez 4D-31
593:Categories
430:References
336:air-cooled
319:Fuel type:
305:Valvetrain
298:Components
289:Dry weight
223:Data from
207:SIPA S.70
202:Nord 3400
197:Nord 3202
93:Nord 3202
33:Potez 4D
381:See also
328:Dry sump
116:Variants
102:Potez 4D
282:Height:
270:Length:
276:Width:
253:Stroke
69:France
494:Potez
410:Notes
237:Type:
163:4D-36
157:4D-34
151:4D-33
145:4D-32
139:4D-31
133:4D-30
127:4D-01
121:4D-00
55:Type
244:Bore
110:1949
100:The
568:9Ab
563:6Ba
526:12D
358:7:1
595::
578:9E
573:9B
558:3B
542:4E
521:8D
516:6D
511:4D
486:e
479:t
472:v
374::
365::
356::
307::
291::
264::
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246::
20:)
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