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Contents
1.2. SUCTION CHAMBER FUEL SUPPLY MANIFOLD
3. 4 94 NE ul HH I 88
4. 136 1940 5 18 1941 5 12 143424
5. IL I 1
6. 32 1 13 Bendix Stromberg NS 2 7 7 p 397 Rig 388 and p 389 Fig 389 AUTOMATTC CONTROL UNIT
7. Continental KV 69 cf Department of the Army Technical Manual TM9 2910 200 35 Field and depot maintenance manual for pump injector fuel assembly etc Dec 1959 Google Books 70 1991 143 9 22 8PI
8. 133 2 1 H R Ricardo
9. 92 93 2
10. E 96 Et 1935 3 3
11. 1 105 40 122 12 8 i eid dd TT k 7 1 ae 122 Ur 154 23
12. P amp W 1930 11 33 2 23 99748 6
13. 1935 9 1937 6 71 2 1 2 1979 78 79 1838 lt 140 142 143 186 189 232 234 236
14. f
15. E BMW 801 8SU lt H
16. Cr B CrV 84 B
17. 2 2
18. 80 CeH NHs 2 132 NM al 2
19. 146 1
20. ON A 185207 1987 11 16 1940 3 7
21. DCG gt 20g HP h
22. 45 50 a 0 116 cf Judge 7 7 1920 DX8S 216X508mm 4 11 1934 105 106 Ht 1
23. 36 739 DB 601E 41 41 12 15 42 2
24. 40 1953 119 123 44 1 Junkers 2 1 110 2 2009 E Hy 42 B
25. ll 144 143 1956 No 46 1984 76 81 De 144 os wet 2400HP 2800rpm 1486mmHg 1 0atm 57 59 48 12 K H
26. 48 11 93 1 Saurer
27. 43 7 R 2800 F 4U Corsazr F 6F 7e cg P 47 hunderbolt 43 4 1 700 Bell P 63 Kingcobra V 1710
28. P amp W 1 22 1942 21 ADI P amp W Derichment Valve 148
29. 6
30. 1930 122 FA EF Schmidt 1943 119 168 J E Campbell Wasp 9 8 68 PN 3 0 20 Qc
31. I i 0 9 17 12 18 12 a 700km h 191 L NN
32. E 73 74 Qc ul a No 5 1985 9
33. 14 14 50
34. 3 72 7 SE kt 5 ag gt L 5 Re cs 1 NN 1 SS 935 8 4 NRNSSS SS SRIRE2 A FN ll 2 2 or
35. 2 X 32
36. B 17 1 2 2 2 2 Bendix Stromberg 9 2 Pump Control Synchronizing Shaft 2 9 43 44
37. 36 I 17 Fuelcharger 530 24 39 1950 1964 3 33 3 60 v
38. T 4 23 186 148 P amp W
39. R 2800 CB16 100 130 dry 2050HP 2700rpm 1410mmHg 0 9atm 1 1800HP 2600rpm 2600m 2 1600HP 2600rpm 183
40. SS ON NN CH 070W CaEW 3 i 1930
41. ce EE gt 20 ZL 117 199 En 0 342
42. 181 DC 6 DC 7 DC 6 3 4 DC 7 4 3 DC 6 P amp W R 2800 Double Wasp DC 7 R 38350 Turbo Cyclone 4 182 Cyclone18 R 8350 Centaurus 873 173
43. Bendix Stromberg H ji HH 31 H 12 Bendix Stromberg AIR COOP ENGINE FUEL PUMP IO TO 14 PRESSUR AUTOMATIC CONTROL
44. Bristol Stronberg 1
45. 1 40 96 97 1 2 75 0 1941 3 JVol 1 No 10 1955 NM 72 41 100 1250 109 2 1450
46. 1 1 3 E E I
47. 181 193 182 cf Kimble D McCutcheon No Short Days p 6 1 203 x R 3350 2 dry operation 2800HP 2900rpm 2700HP 2900rpm Bendix Stromberg
48. L 82 1984 191 192 36 41 spinner injection slinger injection
49. 200 27 28 45 lt 47 111 BMW 801
50. 11 E 1
51. 177 180 140X140mm 2 162 g 7 0 4 28 40gHP h
52. Miss V 214 23 R Bosch E BMW 801
53. 1 6503 2893 5 WE FS i a i et i a 900F HR ME ERS MG TSE 60 sm fP CS TM Ft FE SE WS CR EF EE RE FE CR Fes RSS NR 7S EE RS 90 RE Fl GEE MR NE 1 i 5 ee RE Me 13 56 XE Je Ep 5 PEPS SG ER AME Be nt ed Wt HR 3
54. 1936 8 11 550 48 49 2 3ooo 700o
55. E EF 25 E 35 E 4 1984 DNS
56. Shilling s orifice 23 1944 9 B 1 E RR
57. lt ed F E 26 EE 1 201 Ns TOTO E 4
58. 1 77 800 116 i TEE 7 HE EE HH 1 Ei NE i EB i HE EE Ie29 I79p 900 0e 2900 78 800 117 E FrHHTHFTT 1 1 Fm HH ETE HH FTTH EE EE HH HH ee 11 HH HH s HH 1 EE HHHHHHH H HH SRG GETSss31 TTF HH 3 1 EE
59. Qc 149 28 150 No 43 1983 11 18 188 87 350mm
60. DB 601A 16 DB 601A DB 601A 4 NE 2 4 2 1
61. 87 92 91 132 H H 73 74 511 512 517 133 lt 139
62. b No 6 1936 3 14 12 14 93 80
63. 328 194 165 0 166
64. 1 99 28 13 146 39 BMW 801 42 E 2
65. 198 ADI 2003 225 364 450 F6F 412 F4U 1D 364 210
66. E 3 E 1 CsH4Br 6 h h 30 ATDC 30kg cm
67. P amp W P amp W 8 D 1949 N A C A Aiecraft Engine Research Laboratoryy
68. I 2 E S Ineclion labe E 8 Taylor and G L Williams Further Investigation of Fuel Injection in an Engine Having Spark Ignition 4 E Transactions Vol 28 1932 Fig 3 4 and 6 cf S D Heron Development of Aviation Fuels in R Schleifer and S D Heron Development erg Engines and Fuels pp 585 587 1956 9 1940 1955 1976
69. 1 Me109R Mez09 755 138km h FAI 2 B 29 130 4 700km h
70. 1934 9 Armstrong Whitworth 27s X31zin 73 0x8g8 9mm N A C A 2 C ER o 8 16 1 000rpm CFR g 3 15 5 0
71. 26 Ei I 9 Ex Cell O ES gt RNN est Ca HP 144 173 P M Heldt High Speed Diesel Engines N Y 1940 p 165 Hig 4 Heldt 26 148 146 27 27 Continental
72. 1934 er V 12 gt No K 24 P amp W 9 SN Eclipse Aviation Corp Bendix W1710 1980
73. 111 112 163 40 331 164 1 RE 9
74. 100 8 H 3 ee 192 158 lt
75. MEGVOM 1 NE 2CN 180 cf La comande 6lectromagnetique des soupapes dinjection Les Arles No 888 1938 il 1938 No 905 1938 Ee Hi LRMAJNo 481 2005 8 cf La Commande Electrique des Injecteurs Pomps es Ailes 4 3 1939 202 3 6
76. Junkers Ju87A Heinkel He 111 Fokke Wulf Ta 152 68000 1 18 Junkers Report No F SU 1105 ND Aug 1946 Headquarters Air Material Command Wright Field Dayton Ohio p 7 Fig 4 1 19 Junkers 40 FOLLER FOLLOMWER A UNGER CON TROL PINICON V BACK LASH RACK 2 2 2 2 FUEL MULLERSLEEVE TL I PIN 2 MLECTION ALANIFO A BARREL AAA NV 2 LUNGER AN NE DELIVERY Nk CHECK LALVES AIN CONTROL RACKN FE EZ NETEFING TAANSMATTING MOTION EAOM AUTOMATIC
77. DB 601A E oe iv E Ys 1941 1942 1943 1944 1945 3 10 2 257 2 579 3 782 6 437 20 957 40 1 349 3 343 2 323 50 3 527 1 180 60 1 525 2 128 5 183 7 430 833 12 178 5 408 3 149 107 1944 FY 108 50 59 2
78. 4 0 19 2 1 dual carburettor 92021 g 5 0
79. Oil seal 2 Tv 1939 4 Motoren Werke A G BMW BMW 801 2R14 61 000 2000 BMW 801 48 14 Deckel V 0 BMW 48 102 103 2000 801
80. 102 1940 7 30 1941 7 21 144654 445 446 147353 108 100 No 18 1978 114 116
81. 1 8 0 52 atm rpm 30 1 000 300 0 lt 300 30 2 000 50 300 350 100 1 000 50 350 400 30 1 000 100 0 100 100 1 000 50 100 150 30 100 108 4
82. 1 113 kr k 1 2 I 74 2 78 1 75 2 114 5 LIM 72 4
83. 83 EN 83 42 2 1971 1971 202 lt 203 107 1770
84. 5 6 C44 2 4 9 4 0 0 1 0 2 BTDC 20 BTDC 112 II 0 3 S1 84 0 4
85. zep R 2800 3 800 4800m cf P A Wilkinson Aircratt Engines of the World 1957 p 252 1978 573 145 cf Ricardo bid pp 314 315 2 NH4NO
86. 30 EE Prescott 93 1936 41 41 30 Ice Inhibitor
87. 1 2 LT HHT OR PR PP U LL 7A
88. 451 452 146 1975 283 184 E E
89. Vol 1 No 10 1955 Vol 2 No 9 10 1956 EE o 57 cf H R Ricardo Les sans soupape a injection d essence Les Ailes No 81 1938 1938 s 3 2 77e High Speed Internal Combustion Engine 4th ed London and Glasgow 1935 pp 34 92 96 124 125 191 193 296 297 303 311 320 355 359 360 363 369 372 376 380 384 387 58 cf Bill Gunston Fedden 68 the lite of Sir Roy Fedden Derby 1998 pp 142 143 55 BBDC 60 ATDC 180 i H 160mmHg 1 750rpm
90. P 47 199 1991 115 116 Rolls Royce pic 1992 181 185 Gunston amp 3 106 107 1942 Whittle 297 298
91. 27 872 14 V 12 168 260 261 266 66 69 77 84 89 90 110 111 70 75 52 20 4km h 38km h
92. 53 Wilkinson Aircraftt Engines of the World 1957 p 292 106 107 5 3 488 489 4 1 3 Gunston 204 205 206 De aerator 54 Wilkinson 7 108 109 5 2 55 1982 212 213 7 A S Float and Pendulum Type R amp D
93. Derichment Valve ADI Water Enrichment Vavle ADI 2 E
94. 1910 1945 105 106 ui 211 0 DC 6A 6B R 2800 CB17 1 ALTITUDE CALIBRATION HORSE POwER AND MANIFOLD PRESSURE AT STANDARD ATMOS a _PHERIC CONDMONS wm AUTO RICH MIXTURE STRENGTHS UNLESS OTHERWSE NOTED Ne a ES TE PR ER MS OR YO TE 3 UE ER OR PE RO CR FE I EE PE Et WE REE OE WE PE RE TRY tal EE 1 ie EMAXIMUM CONTINUOUS MANIFOLD PRESSURE fa a 2 5OIN HG AT CRITICAL ALTITUDE 1 5 Wi A do ST ea EE EE a EN
95. 1 5 a 14 F 107 T 5828 4 1944 3 45
96. a NN 14 15 EE H Little D E Danielson Description of German Fuel Injection Systems Rescinds Summary Report No F SU 1105 ND Aug 1946 Headquarters Air Material Command Wright Field Dayton Ohio 16 5 No 327 1982 DB 601 No 828 359 82 85 25 No 112 151C64 67 36
97. 1 830 Bosch ATMOSPRERIC PRESSYURE DECR EASE CHARGE PLUNGER CONTROL RACK ATMOSPHERIC PRESSURE NANO ConrTROL SPAING LOADED le RICn POSITmore CAPSULE TEMP INCREASE i TEMP CoNTROL Rop BoosT PRESSURE ditto p 35 Fig 27 46 DB 601A A 26 1 12 1 5 51 3 6
98. 155 1 107 40 66 C No 2 66 DB 601A 1937 20 50 5
99. 1923 Louis Renault h e g 100Hz 4 12 000rpm 0 1 hs 1 R 3850 20 1
100. 650 480270 6 2 as 1 47 650 2 73 1
101. 2 2 7 3 5 3 2 3 7
102. 74 1944 4 76 ml am 2
103. 1999 185 M G Chandler RT
104. 75 60 1 h F FE 5 1 48 1935 4 4 EE 4 40 1 000 NT F gt gt
105. 214 154 4 Nb NN 20 214 0 10 2 II 45 1 67 I EEH 6 7 40 2 808
106. 21 1 450 2 600 1 850HP 80 800 2 500 1 680HP 2 100m 150 2 300 2 800 400 2 600 1 800 2 500 1 2 2 500 150 2 100 0 2 200 150
107. 78 88 1kg 0 25kg I 57 850rpm 1 HHR HH Ei HE HH 3 ms N EHHEHt o liRi nv 3
108. 109 14 10m s 2 650rpm 13 75m s 2 750rpm 3 1 12 400mmHg 2
109. ml Ice Detector De leing Unit 1 ALCOHOL TANK ICE PETECTOR 1CE FORMATION OBSTRUCTS SMALL ORIFICE FIRST BALANCINC ORIFICE IDENTICAL IN SIZE WITH DETECTOR ORIFICE DETECTOR DIAPrRACM AIR BLEEDS Normally the detechor orifice is clear pressures Normally the akohol valve is held closed by on both sides of detector diaphragm are equal Spring When detector valve is opened and detechor valve is closed Suction acts on alkcohol diaphragm and When ice obstructs small orifice pressure allows alcohol valve lo open then alcohol rises in the chamber above detector diaphragm is ntroduced with the fuel ice dispersed and delecior valve opens pressure balance resFored and alcohol Yalve closed normal condition DIAGRAMMATIC_ARRANGEMENT OF AUTOMATIC DE CING_UNIT FOR CARBURETTORS 169 Andrew Swan Aero Engines eszgg and Practice Handbook
110. Pe 8 9 5ata Qc 58 68 Schmidt 1915 37 7 3 40 100 87 42 122 N A C C N A C A 1938 Armstrong Siddeley Jaguar
111. CHsCOCH C eHsNH2 HH 20 H 7 1 93 5 En H 3 101 83 0 3 1 3 Fl 3 780HP 2 600rpm 450mmHg 2 500rpm 300mmHg 70 10 2 750rpm G GH 87
112. Vickers NN 1942 2 4 E gt RT 1 83 42 2 89 512 513 125 1 I 84 42 2 126 9g 23 3 20 4
113. 5 7 6 11 2 21
114. SS et 0 E 8 1 G L Williams Cooperative Fuel Research Committee 1 3174X412 in 82 6x114 3mm 20 20 C FR C Society of Automotive UNA A JI RY 1921
115. The Technical History of Mitsubishi Aero Engines From Renault to Kinsei Family Engines Part Il Evolution of Gasoline Injection and Water Alcohol Injection in Aero engines and Mitsubishi Heavy Industries Discussion Paper No 78 2013 6 27 Shigeki SAKAGAMI FT SC9 TS h HE Ni 6 1
116. 40 93 12 2 200r
117. H DB 601 E 200 F
118. I 10 Continental Heldt Ex Cell O ei Ex Cell O I 11 Rx Cell O 27 cf P M Heldt High Speed 7ese Engines N Y 1940 pp 165 166 28 ML Pumping and ak distribehing phinger 1 L C Lichty Internal Combustion Engines 6th ed N Y et al 1951 p 239 Fig 158 from G M Lange Fuel Injection versus Carburetion for Personal Ai
119. I H 1939 FH eS
120. 4 1940 SU 8SU 3 E ez777
121. Bendix Stronberg 8 I 16 R 2800 CB17 Bendix Stromberg PR 58E BALANCE DIAPHRAGM es gt VALVE IHPELLER SLINGER RING 3 Vol 1 No 10 1955 10 833 13 34 33
122. 2 EE 2 Et J a 141 513 142 y 182 62 1944 16 1941 5
123. h 201 202 65 202 e gt 15 18 17 64 66 180 200 20 2008 216
124. E P amp W 1938 Bendix Stromberg 3 28 E Bendix Stromberg 0 7 lt 0 98kg cm2 0 35kg cm2 2
125. 49 I 29 Daimler Benz DB 601A TwO OM DRAIN HOLES COMMON PASSAGE LEADING TO CAM SHAFT BEARINGS FED BY AuXIUARY GEAR PUMP DRIVEN SUPPORTED BY CASTINGC Os E OL GROOVE IN PLUNGE R COMMUNICATING WITH GROOVE 1 CONTROL RACK PASSAGE lt ALLOWS OIL TO RETURN NA Re NS N COMMON PASSACE LE ADING 0 ENGNE OL TO GROOVES 2 FORMED IN PLUNGER AND E lt BARREL ASSASE FRON PLUNGER TO PETRO UU F NN Sie 1 2 2 FORMED NBARREL NN NN AY CONNECTION TO ENGINE kr kN OIL SYSTEM SN DELIVERY 77o p 37 Fig 29 50 1 2 8
126. 30 5th ed 2006 pp 17 18 58 Messerschmitt Bo6lkow Blohm MBB 68 Hy E 66 14 C41 BMW 801A es 53
127. EO OE 2 2 2 NMM 199 3g BHP H 1H U6 130C 2 Sir Dugald 5 17 8 Bureau of 6 962 8 7
128. 170 23 P amp W 123 P amp W AD1 124 125 II 2 R 2800 123 100 62 P
129. 65 1942 No 12 39 3 EB 1950 1940 100 109 79 1989 6 Q147 12 14 15 130 16
130. DB 601A 2 097 58 22925 2 2 3
131. Heinkel Messerschmitt Bf 109 DB603 1e2 x 1s0 72 000 45 4 2 IS 123 124 I Nr 1956 452 454 45 cf Mercedes DB600 der erste Deutsch 1000PS Flugmotor 47 Heft17 1937 DB600 1000 2 2 Le Daimler Benz D B 600 es4 es No 910 1938 48 DB 601 60 V Bosch A 26 11 PZ 12MH 100711
132. 194 195 40 NR RS NN 1944 11 B 29 F 4U P51 6F P amp W R 2800
133. 2 180 So
134. 2 gt 9 2 9 18 and 19 Clark Jumo 211A 2 H 1941 13 DD NN T
135. 15mm I 54 650rpm i EE EE EE EE HH HH 1 4 ue 86 7 850rpm ii I 55 850rpm FH 1 1 HH rt EE EE Et 0 HH IH tH EEE BET ae E te 87 2
136. f 1930 C EK Taylor Marvel Carburetor Co 37 Cye ope Eclipse Aviation Corp 1929 Bendix Stromberg Motor Devices Com 1929 Aviation Corp Bendix Stromberg
137. 3 185 t Es SEM LU 2 zK 1 1 0 5 160mmHg 0 4 lt 0 5lg cm2 28
138. 2 Double Wasp 146 0x152 4 Twin Wasp 89 7x139 7 2
139. 29 Bendix Stromberg Vol 2 No 2 1956 30 222 0 ERG 0 1997 420 421 MM 33
140. Eb4 12 P M 544 Wilkinson Ford V 12 Aircraft Rngine Aviation June 1941 VH12 5 8 1941 8 13 cf C M Green H C Thompson and P C Roots Planning Munitions for War 1955 United States Army in World War II pp 298 301 Allan Nevince and FE E Hill Ford Decline and Rebirth ILI OG N Y 1963 pp 193 194 204 1988 194 833 E 11
141. 126 cf Kimble D McCutcheon No Short Days The Struggle to Develop the R 2800 Double Wasp Crankshatt Society AEHS HP 173 p 6 1 Aircraft Rngine History piston engines 12 0 H 2 F
142. 22 27 23 2 187 Mu Hm ADI P amp amp W Derichment Valve 149 23
143. 130 134 178 77ez777 61 2 2 cf C F Taylor Aircraft Propulsion Smithonian Institution 1971 p 68 Higure 64 from Flight Vol 42 p 656 Dec 17 1942 179 HH Power Jet Ltd 1955 Frank Whittle 2 1
144. 1941 E 40 22 27 23 Hy 103 2 000rpm 575
145. 1 91 42 2 H 1 92 42 2 12157jE 35206 5 FET Mt 26 H 138 i a
146. JDistributor Block 8 E 251 7
147. lt E gt de 9 SS
148. 112 I 161 1955 1 158 LIL 11 58 166 173 193 140 RN Ng 62 162 62 DB 601 20
149. 1993 1 1998 131 92
150. 4 1 lt DB 601A 62 E F XX 1941 1940 Battle of Britain DB 601 MerZzn 1
151. IM 6 10 20 12 1 21 2 171 171 197 R 2800
152. 56 PETROL GALLERY 1 4 10 4 H 2 0 2 1 E
153. Qr 1 44 BMW 801 65 EIN NN LTTE TL i 3 gt PP Dt i Deckel 2 NN A SNS NN NN A YE 2 Bosch ditto p 75 Fig 59 part p 72 Fig 56 Arsenal 1941 zzzo 41 zzz o 213
154. d 1936 6 No 23 1987 8 1 1935 12 36 E4 600 k Hy
155. B HHH 1 101 23 98 114 2005 68 99 0 25 0 35kg cm2 1 8kg 10 1 6kg cm2 MAN
156. E x 89 H 158 169 560km h 1 57 1999 169 27 032
157. Cyclone 37 3 E 41 5 1937 40 TWA CC
158. 140 4 gt 95 139
159. 29 DAMPING FLUID 80 Bendix Stromberg Bendix Stromberg
160. 41 DB 601 100 1984 4 9 81 82 9 84 6 2
161. 94 6 98 13 Q 2 Q 90 E 8 1 20 19 0 1 Q6 22 El 5 6 0 10 H 77 23 6 31 10 80 0 Q1
162. 2 2 2 193 NE BE P amp W 2 79 RR 3 4 5
163. General Electric B 11 gt Bendix Stromberg GC RR 2 B 29 10 1 es 1200 RR Merizin
164. R 3350 ASH 90 18 Bendix Stromberg 49 Goliath 1951 3 54 FE Borgward 700 900cc 2 2 1961 55 1952 Benz 44ezceges 300SL 54
165. United American Bosch Corp 1985 6 1 23 YAN a E J ER Campbell 1934 24 a 1835 E
166. 3 lt 4kg cm2 HH 192
167. 1 104 wp 3 1 2 2 7A 1943 FE 11 153 1 3 1 2
168. 106 wobble plate cam plate 5 91ein 14 29mm B 135psi 9 48kg cm2 VS No 87 1982 11
169. E i lt Oversized engine high compression engine 164 E 1 54 12
170. N20 145
171. R 3350 Centaurus 973 R 3350 205 2 P amp W H 1938 11 1940 3
172. 75 8 4 0 3 4 2 1943 3 20 100 NE NG 115 B CC 1943 12 109 4
173. 8 5 5 0 4 3 1 500rpm I 1 C E 2 NR 2 2 SNS 1212 RAAAAL ARRY d NN LA RR NN A A 2 2 i CF Taylor E S Taylor and G L Williams Fuel Injection with Spark Ignition in an Otto Cycle Engine 4 E Transactions Vol 26 1931 Fig 2 and 5 Development of Aircraft Engines in R Schleifer and S D Heron Development of Aircraft Engines and Fuels N Y 1950 pp 529 544 14 Bosch
174. B 70 80C 91 f 2 91
175. 6 89 14 1 850rpm 2 2 I 58 850rpm eth Huttt et 90
176. I 29 39 R 3350 P amp W Cye oze R 1820
177. 104 104 i 156 c 62 11 23 4 18 42 43 3 100 62 112 I 33 62 1500HP 2600rpm 500mmHg 1350HP 2000m 1250HP 5800m 2600rpm 105 62
178. E 1944 1 H 2
179. 201 i F H 1967 Bill Gunston 996 1997 1 ADI 1 ADI 1908
180. 1 28 Daimler Benz DB 601A Bosch 4 WO DO WDDD ditto p 39 Fig 31 DHS Nn dr i D B 600 4 4 1939 K Brode Mercedes Benz Flugmotor DB601 Luttwissen Bd 8 Nr 4 1941 DB601 9 5 1941 R W Young Mercedes Benz DB 601A Aircraft ngine Design Features and Performance Characteristics 9 4 Jounal Vol 49 3 1941 DB 601A 10 5 1942 A 26 1998 10 13 3 DB 601A
181. 1944 1 97 100 145A 14 2 a EN aa ON i as a 56 32 34 33 1943 NN 97 43 4 1971 203 147 E 11 PPC
182. 2 P amp W 41 P amp W 42 9 P amp W 20 30 40 10 amp HP h 6
183. D R Pye 155 205 45 ABDC E 84 4 5 R raco s F 58 8
184. Ns 2
185. 152 7A 4 1 E 1 3
186. 28 Bendix Stromberg KR 215 H 1 m f
187. H 7 5 lt 11 0 9 5 8 1 5 2u 13 5mm 9 0mm 11 0 12mm 20 lt 80
188. 2 139 86 928 32 Standard Oil Co 100 Stanavo Aviation Gasohine A S T M 4 25 100
189. 1 000rpm atm rpm mm3 30 1 000 300 0 300 442 30 2 000 50 300 350 455 30 1 000 350 442 100 1 000 50 350 400 426 30 1 000 400 443 30 1 000 100 0 100 320 100 1 000 50 100 150 302 30 1 000 150 320 1 I771 109 7 SS 6
190. 1 0kgycm2 23 1 6kg 148 o Cr C 1 0 1 1 Mn 0 25 Si 0 20 Cr 1 5 CrV C 1 38 1 45 Mn 0 55 0 60 Si 0 25 Cr 1 6 V 0 189 0 4 0 5mm
191. 196 197 B 29 R 3350 P amp W Bendix Stromberg ADI 43 40
192. 2 2 150 100 2 000rpm 50 50 50
193. 2 E 11 23 et 190 tp ka LL 3 11 23 147 R 2800
194. ls R Ci H
195. 30 BTDC 0 3 0 1kg cmz 240mmHg 50 30 10 ATDC 10 ATDC 100 120mmHg E E 0 5 0 3 60mmHg 0mmHg 60mmHg 1 600 1 800 2 000 2 200rpm 1 000m 2 000m 0mmHg 1 600
196. 10 5 13 5mm 5 7 5 E 42 2 1942 B
197. 30 E 1 ui 6 0 11 70 24 10 37 2 7 33
198. Bendix Stromberg 99 14 1971 215
199. B 1 10 E 5 5 2012 jJ TBA MTBE 206 215 163 I 1 9 1
200. B 29 R 8350 R 3350 Turbo Cyclone Douglas DC 7 Lockheed 1049 Super Cozz7e
201. E SS Merlin Griftton RR v Bendix Stromberg 7 1 45 Rolls Royce E R 6 R R 2 1969 225 ES J E Bishop Battle of Britain 1966 1972 116 117 1949 1 This window commemorates the pilots of the Royal Air Force who in the Battle of Britain turned the work of our hands into the salvation of our country
202. 1 39 BMW 801 De aerator 60 FLOAT AMD PENDULUM TYP OE AEARATOR AnR TO TATNK FUEL TO ENGINE DE AERATED FUE TECTION PUMP DE AERATOR ditto p 60 Fig 48 Float and Pendulum Type De aerator Bosch 9 I 40 BMW 801 Float and Pendulum Type De aerator 49 Bosch 130560 1939 6 15 133101 1939 11 8 1986 6 22 137489 1940 7 19 1986 7 17
203. 1938 9 9 6485 1940 7 2 1941 9 24 145709 gt H 1940 5 23 BMW 2 147350 1940
204. 1910 1945 190 1990 430 2 F I 20mm 2 2 7 200m 26 33 f RR 2 2 6 155 4 l 156 1 m B 29
205. 2 64 100 12 Q1 A a 18 B LL LD 30 24 33 12 1 32 3 4 SS e ee e e l esses SSS SS eeeel HSeese SEE 9 9 9 SSS IN 9242
206. 1939 N A C A Comper 35 hb Eclipse Compur Bosch
207. 3 1 62 N 8 KR 7 vV I 62 40 1 81 D P No 62 2010 8
208. 212 4 Department of the Air Force AF MANUAL 51 9 Aircratt Performance Engineering for reciprocating engines 1954 p 128 213 E 6 1 m
209. 5 1942 E 2 43 12 907 72 85 C38 amp 21
210. SU E 72 E H Sir Oliver EE Simmonds 1946 Simmonds Aerocessories Inc SU Simmonds 600 SU Fuel Injection Systems 6 0 7 7kg cm2
211. 1944 3 50 90 0 15 0 2 a
212. 5 1956 9 6 1957 361 373 0 1970 202 204 220 232 C Campbell 1971 187 196 C Campbell 1972 268 279 280 39 cf Junkers Hochleistungsflugmotor Jumo 211 1200PS ohne Vergaser mit Benzineinspritzung Flugsport Bd 30 Nr 21 1938 211 3 12 1938 The Junkers Petrol Injection Engine Flight Vol 37 No 1621 7 4 Heldt 3 1200HP 1940 91 58 94 97
213. 6 K 170 C41 8 E E H 1 H
214. 121573 1935 11 30 l fF 19837 9 1 tt A 8314 315 145707 1941 9 24 HH F 1987 9 1 1940 3 7 35 150443 1 O 150759 472 473 595 596 606 607 98
215. I 97 42 2 14 BB 101 96 DB 601 O 1943 F 4 144 14 14 18 42 2 18
216. f 800 No 20 1937 2 2 3 5 800 14 140mm 150mm 32 342 7 0 20 BTDC 65 ABDC 75 BBDC 30 ATDC 25 BTDC 2 000m 84 SOAP Spectrometric Oil Analysis Program 1940
217. 3 13 0 8 87 100 12 5 550mmHg 13 6 4 3 3 100 1940
218. 801D 1700HP 1440HP 18700ff 30000ft 9144m 63 Graz Pischinger DB 601E 81
219. Lucas Industries eggszs 1932 E2 1 1934 70 BTDC 7 0 5 85 56
220. J Connors 2 400HP R 2800 128 3 400HP 129 3 400HP 3 800HP P 47 R 2800 P amp W 3 200HP R 2800 Mc cs VI 2 P amp W gt
221. lt EE o 8 FE 0 3 j ts
222. 43 12 3 100 62 28 39 2 17 Vickerc MAN 28 11 23
223. 137 148720 1941 1 28 1942 2 27 NNN OE CE GN 186 315 316 T2r Ti 1000 Ts 500 Ti 600 T2 100C 273
224. 2 15 sg 19 n2 FT GQ8 21 L 20 7 Q9 0 F Ge 3 8 2 29 30 35 1
225. 47 2 6 i 44 1 27 2 f i i Daimler Benz DB 601A Bosch 1935 Daimler Bentz AG zzzo 211 DB 600Qnv 12V 150x160 DB 601A
226. 199 Bendix Stromberg ADI R 8350 P amp W R 2800 oz2 e Wasp DC 6A 6B R 2800 CB17 1 We 2500HP 2800rpm 3800ft Dry gt 2200HP 2800rpm 4400ft 1900HP 2600rpm 7000ft 1660HP 2400rpm 12200ft
227. 160 12 151 16 999 28 541 46 526 12 360 72 39 1950 305 7 J B Cohem 0 IT 1943 10 12 108
228. 2 2 5 Centrifugal De aerator 0 28kg cm2 HH I 38 BMW 801 2 De aerator 59 ditto p 64 Hig 50 F1oat and Pendulum Type De aerator
229. R 3350 14 250km 1950 E 9 29 lt 10 18 032km A 26 45 184 cf P H Wilkinson Aircraft Engines of the World 1957 pp 256 257 Schlaifer i Ricardo P amp W
230. 1 dopes cf W J Stern Aircraft Rngines Chap XVI of J N HH O E 81 88 1 E 78 76 41 5 5 40
231. 35 Engines of the World 795Z Washington D C 1957 p 256 P H Wilkinson Aircratt 133 sczss7o7 Paper No 60 814 HH 121 2010 7 8 b 100 slinger 36
232. I 2 92 20 BTDC 65 ABDC 75 BBDC 30 ATDC 50 85 BTDC 70 ABDC 60 BBDC 45 ATDC 80 1 507 60mmHg 1 900rpm 2 ATDC 180mmHg gt gt pX
233. R 3350 R 3350 7urbo Cye ope 170g HP h yclone 18 195g HP h TurboCyclone oz e Wasp 10
234. FE 2 87 1935 37 85 f 80 ATDC 0 50 100mmHg 1 800 1 400rpm 50 1 600rpm
235. 1 6 08 910 1945 98 99 175 178 90 91 167 100 A i CC 195 gt II 65 a 451
236. B sl 1947 Centaurus 373 2R18 146x178mm 10 C A V 9BB 120X780D 9 xX2 C A V MA J E 60 cf V F Bingham Major Piston Aero Engines of World War 77 Bath 1998 pp 55 57 59 61 62 65 61 cf 7 ZZ and Gunston Fedden p 284 Wilkinson 47c7g Engines of the World 7 5Z p 267 Hercules 216 2R14 146 x 165mm dry 1800HP 2800rpm Hobson R A E B1 BH17 2 2 ezcz es 759 dry 2040HP 2800rpm Zenith R A
237. P amp W ji 20 3 3 0 11 2 off 23 a 20 20 8
238. 1 10 1949 67 MN 1 56 4 i H R Ricardo 5W 30 CAV Bosch CAV 26
239. 102 23 2 20 BTDC E 80kg cm2 50kg cm2 103 7A 1 103 i 5 3
240. 10 15 5 18 dual carburettor 50 2 1923 tt g 5 0 E
241. 180 A 1908 RI Antoinette
242. 1 EE 2 H 1953 4 lt LEE 1976 CO 4 E H 1944 7he Aeroplane Production Yeaz7 oo 48de 21 1 COs 10 2 N23 398 399 pp 425 429
243. Bendix Stromberg P amp W ADI 100 ADI 22 12 99 22 22 97 28 P amp W
244. 74 3 1956 1 71 5 i 1930 E 72 DB 601
245. 0 amp O Ten SR SME RE RS TE OE EE OS ER A EE NE EEN De CE EEE SE EE EE es Re SR DN a A IGE FEE FE RE OE ad MR Sa 7 A WEE EE EE F et Bee ERE ER a RE OE 9 MOR Wa i Stns pet Ss SE SE EE gt eg 30 Pi 3 2 0 50ooEi LE ME NS RE PAG FRE DE EE ER ORE 1 Tat he GE Baa Em a ED Pro es 1 A a a a St SD PS SS HEHE Mats UAE NE A HES SEE EE oT RES pd SE ER EEE RE BR OE et CR BIE POR RS 8 1 RS FR RE 2 lt Ed Ul BE RE 5 Miel at Knit 3 TH 2
246. 1934 5 14 39 1 17 US Pat No 2 143 935 9 4 9 3 2 2 1 4 DI I 6 M G Chandler 2 143 935 9 1 21 I 7 M G Chandler 2 143 935 9 2 G7 N53 2 2 1
247. 2 B 1 674 675 1937 3 5 3968 9 gt 4 N NE SS 1950
248. 5 6 6 70 200 220
249. 135 1956 133 2 4 100 370g HP h E HH E
250. 36 6 0 37 2 800 0 e No 16 1936 12 1935 4 50 106
251. re ADI 176 ADI 2 General Eiectric 2 JADI
252. 5 g 3 E 28 BTDC
253. ADI CHsOH CsHis ADI K D McCutcheon 150in Hg ADI R 2800 C
254. TLycoming R 985 Wasp zz7on M48 Patton V 12 Continental ADVS 1790 5B 88 46 SU Simmonds 570 SS M RE Se TTT RBRBSB EE LE er SS SS 254 68 cf Jan P Norbye 1bid 1st ed pp 37 38 2nd ed pp 30 31 Mergn 530 570 580
255. 198 Si 194 1047 195 A 26 35 9 1989 43 44 1996 95 96 197 Marshall B 29 30 160 B 29
256. 87787 Q930 8 6 100866 1933 5 2 119879 1987 4 5 82 83 127 128 231 232 132
257. B 29 3 E 4 500m 45 8 Mi 38 0 191 6 BD 29 43m 1 910 1945 161 1 m 45 4 500m CO
258. E 127 to 545 128 Packard 100 150 100 180 1157145 2 200HP P 51 H Mustang 1 900HP
259. NO NN a 190 486 1 18 6 7 1961 MM PWR PU PP 910 1945 1990 1946 114 lt 115 190 KN 207 2 Pa A gt J 1 486 4
260. R 3350 7urbo Cyclone EA4 3400HP 2900rpm ary RA1 RA6 DA1 DA2 3250HP 2900rpm ary DA3 DA4 32W 3700HP 2900rpm wetl 34 3250HP 2900rpm ary 91 36W 3500HP 2900rpm wet 89 184 183 Schlanfer 1 Oivil Aeronautics Administration cf 51d p 527 n 24 R 3850 8A 1 F 8 1 38 16 435km 1955 B 29 Lockheed P2V 1 1946
261. etc 89 1 500 1 000 5 1 93 1000 40 95
262. 50 133 278 1960 190 184 ZF 34 135 Vol 28 No 361 11 1929 8 H Oo 177 bOG MO 262 293 1 506 508
263. 300mmHg 2 250mmHg 91 TN 92 3 1I 7101 2 30 a 2 50 I 411 50 92
264. Ex Cell O Aircraft amp Tool Corp Detroit 25 3 Cumpur 1936 E Compur 26 135 REx Cell O Ex Cell O
265. 1500 1800HP V 12 DOHC4 3 2 12 9000m 1500HP 15 Ford 2 12 3 V8 GAA V8 60 525HP 2800rpm M4 Sherman HR 3350 Duplex Cye o7e Bendix Stromberg
266. 75 172 2 20 30 1 500 109 2R14 146x160mm Cal 300mmHg A bmep 13 3kg cm 2 vs 13 6kg cm2
267. O 21 119 cf Ricardo 120 7 7
268. 100 gt t 1941 1945 7 1 1 45 22 PD 0 202
269. 2 EB 100 H 28 F 700km h F 2 E 165 100 IV 83 14 18 8 3 474 1000mmHg 166 449 450
270. 0 7967o 7so 90 24s g HP h 0 367 1 078 0 1H 796X 1 X 0 796X1 073 28 5 507so k 174 18 RM
271. 83 84 f6 2 3 112 62 46 100 83 a 6
272. ADI 1 Gingle Point Injection ml
273. BMW 801 600 2 3kg I 65 600 1 82 4
274. 1932 Deutsche Versuchsanstalt fr Luftfahrt Kari Schnauffer Robert Bosch 34 35 Junkers Bosch Deckel BMW 8s01 Orange DB 601 Ehrich Gratz Maihak 14 DB 600 37 DB601 2 88 800 15
275. P amp W 12 208 191 F1 B 6 7kg cmz
276. 1 500 4 6 000rpm I 85 127 I Oo SS E 8 N 6 H S BS 8 AN 1 86 128 oko En sbm rm 175 a
277. 17 118 cf Judge 7 7 166 Judge 7 7 3rd ed lt Ak oe 18 1 Walker Koivulehto H f cooled E G R
278. 450mm 3 20 2 6 600m E 1 m B 29 104 2 880 Q1 540HP 2 500rpm 2 gt 37 1009 2
279. F E 2 12 26 48 12 27 3 527m 699 9km h NR 624km h Me109R 131 78 1
280. 0 52 92 h 1 4 mi aim 0 52 80
281. 1 111 62 rs 4 0 GYNE WO ER 1253 08 RR YODRL HA33 62 9 d gt gt 14 BMW 801
282. 67 cf Gunston 0 191 PE 3 ditto Rolls Royce 4e7o Engines Somerset 1989 pp 74 80 81 Wilkinson Aircraftt Engines of the World 795Z pp 272 273 Schlaifer 1bid pp 527 528 71 SN SS RS e NN NN 1 2 1957 498 7 36 b d q h m n e i k 497 498 SU Simmonds FF
283. 8 1 31 Bosch Lean Idling 1ever Piston Cylinder Feeler lever Feeler Thermostat Bellows pipe Boost Pressure Feeler CC Boogt preggure el hamber Membrane Chamber of atmospheric pressure ditto p 50 Fig 38 1 32 Bosch 52 Feeler lever OE 2 MM Bellows tl HH_ gt NR AN Nh NRIA i U OUUVOGUUU OOVUUVUVOUUOOSOO OOON 66O SO RS Nx SN N NNNNN Thermostat cartridge Feeler ditto p 51 Fig 39 Orange 70
284. 113718 935 12 16 113719 M G Chandler 195 198 17 1928 7 5 1935 12 3 US Pat No 2 022 653 4 12 23 4 I 3 M G Chandler 2 022 653 1 Ni N NY NY 3 NSR NN ON 1 7
285. 1942 2 27 3 146772 3 12 H 188 2 NO TI 0 H 1940 F 8 12 11 E F 147353 1941 12 23 187 H 24
286. 288 289 301 303 342 343 61 PLOAY QP RAT D AIR AIZ amp FUE NET CEASE YALYE M AA IN OPEN FIST ON REL ASNG MR CORK FLOAT NNNSSSSSSSNNNN M 4 tN N eg 22 NE MN SN FT NN 4S 7A VIEW IN OMIRECTION OF ARROwW A wiTh COVER REMOVED NNN SECTION BB AR OUTLET Seo eS ditto p 60 Hig 48 Float and Pendulum Type De aerator Rolls Royce 2 eey 50 1 41 BMW 801 50 20 2001 154 62 UNOCRCUT 1 wiOC aD CORNCRS AY O QN APSROMATE RAOIUS OF Tn TACC 3 SCALE
287. 3 0 8 800 Eg 3 800 126
288. Oo HN E ezy7 2 1945 2 1 1997 USA RC
289. cf Schlaifer Development of Aircraft Engines pp 106 523 538 539 Q 37 impeller injection 34 Vo1l 2 No 2 1956 2 Bendix Stromberg 132 114 133 115 37 1 15 16 35 Bendix Stronberg
290. 90 2 54 18 180 I 4 M G Chandler 2 022 653 2 RN A 2 NE 4 SS EN lt sc N AN bB KS 2 R SN SSSSSSSSSEEEHE SS Ns 6 oe 22 NSK em OSS re lt A A KS ES x GR a SS N a I LJ 1 2 L 1 rr 23 22 88 40 g77 24 25 2 18 54 26
291. 205 112 220 mm 0 75 600 100 A8 3 6 0 790HP 2 000ml A8C 4 40 DI I 73 800
292. 650rpm 30kg em2 14 60 40 20 3 H 84 mm3 h HI 650rpm I 58 00 00 EE NN NE HH HH i HH 85
293. Bendix Stromberg 32W 1980 ADI R 3350 R 3350 ADI Centaurus A OE EO Ee eR es Centaurus 178 8 6 285072egs R 838350 wet 186
294. 7 12 ZT RN 73022 bh 24e2 8 7301 BR RN GQ F 26027 67307 0 Fb SC VR YY 6 30 in 4 3 9 IM IB dl G06 FI 4 a 2 77 a LO 4027 FH 21 0 417 67 175 147774
295. 121 cf Judge 1bid 3rd ed 167 5 lt 10 6 7 7 0 R 20
296. 5 ka B 29 1 I cf rH 218 258 Oe 2 H j 89 E 0 14 47 1948 1946 1 B 29 30 E v 0 B 29 CO
297. 6 850rpm 30kg cm2 500mm 1 200mm 1 400mm 1 600mm 4 NN 1 200mm i c No 8 1936
298. 93 700 3 41 12 19483 88 15 BMW 801A 39 NR
299. A5 3 1938 7 ee B5 XX ON NN 4
300. 2 11 11 100 EE E 1 23 91 2007szo 2 h 0 323
301. I 51 1 82 NN ll 5 62 3 1985 8 10 11 36 2 3 1 52 83
302. i E 41 Des Champs Bendix Products Division R 3350 2 R 3350 9 R 3350 30 12 Lycoming H 2470 24 2 18
303. 13 35 111 121 O 175 A 26 78 42 31 Se 2 CO
304. B 29 R 3350 Duplex Cyclone Bendix Stromberg Direct Injection System Ex Cell O 1 14 Bendix Stromberg Direct Injection System SLEEVE WOGBLE Nl DISCHARG NO LE CONTROL PLATE CONTROL PUMP CCNT NOL SYNCHRONIZING SHAFT 1962 146 120
305. 1940 6 Ford Motor Co Henry Ford 8V 137 2 18 200 1 B 7 F 13 1800HP 8000rpm 12 HX Xx 152 4mm g 7 5 1998 226 228 Robert Schlaifer Development of Aircraft Engines in R Schleifer and S D Heron Development of Aircraft Engines and Fuels N Y 1950
306. 1942 153 155 63 cf Bingham 7 7 pp 20 30 64 ight 1941 5 6 zzzo 211D P M Heldt Fuel Injection for Aircraft Engines Automotive Industries Vol 85 No 6 1941 10 1 1942 DB 601 65 H Nockolds The Magic of a Name 1938 70 RR Battle of Britain Miss Shilliing s orifice
307. 35 37 35 36 139 80 1 000 AgC 40 BE 26 1 1940 5 BE 9 12 1834 139 mm 1 94 140 1 89 90 I 95
308. 1 63 115 II 21 IL 1130HP 1190HP 515km h 6 000m 555km h 6 100m 40kmh 169 555km h 6 100m 6 000m 553km h 21 170 115 II 2 E
309. 140 32 62 4 3 162 1943 11
310. CaHzSe 0 4 87 92 92 96 E 41 9 142 8 141 O ara 3 HH 1 0 1 1 93 100 2 90 100 3
311. 1978 247 264 1960 E 527 529 Wasp zz7o7 580 ml hy 73 SU 10 8 8 7 8 7 69 ME 7
312. kgcm2 1 6 1 8 1 6 1 8 50 50 0 3 0 92 1940 K 151 1940 7 1 K 154 41 3 K 169 41 3 5
313. 1 23 5 1971 4 FE 1987 208 217 5 Stromberg 2 22 27 23 40 97 99 2 1997
314. 12 14 18 75 f E 3 1942 2 37 38 1986
315. 26 10 NE 742 3 1943 2 R 3350
316. 1000 1600rpm 400rpm 1 48 650 OSN HH WTWAWffah 2 EE i 4 HE 1 4 i 1 SF RE Em WW 1 _ 7 3 E RE ER Ri BB 1 lt i bl EH Er BH 1300 theo 1500 Ye 2 8 se 2 RN 49 650 79 3 E HHEEHE EE ML 2 TH 4 Ti EE 300 400 500 7600 1 9 206 22
317. R ts 23 100 H 73 150 114
318. 1 62 N N N Ns W gg NAN NN ek SS RS NN TT NNNSN NN N N LN N A Go NR NN RS NN 4 N NN N 11 97 8 Q9 1 79 1
319. 16 6 DB 601E 8 2 87 100 DB 601Q 9 I 34 Daimler Benz DB 601 E DB 603 am shaft 6 26 4 4 N lt Ro11er tappet Return spring ransmission nose 6 4 N 3 kee AO Contro1 bushing Contro rod lt a Adjustment Balancing groove Piston op ylinder 7 i mn Suction chamber Return chamber Pressure valve onnection ditto p 45 Fig 35 47 DB 601A DB 601N 1275HP 2600rpm 55
320. 1936 10 67 SN 1 93 700 Claudel Stromberg Stronberg Stronberg Bristol 2
321. 2 Ne De 18 lt 1 E E
322. 3 5 Z ditto p T1 Hig 55 11 3 12 11 BMW 801 801 Deckel BMW 132 801
323. R 3350 cf H R Ricardo The High Speed Internal Combustion Engine 4th ed London and Glasgow 1953 pp 313 314 204 8 8 R 3350 wet R 3350 3700 7urbo Cye oze 82W Schlaifer 7 185 Lockheed P2V 7 Neptune 2 32W
324. 0 40 9 WM 37 Northrop Gamma TWA Cyclone 1940 TWA EEN v i
325. 1 RS S Si NNN WATER FEED uNE SOLENOID VALVE TANK DRAIN PUMP SEAL DRAIN LILz TO DERICHMENT TO REAR OIL PRESSURE YALVE OIL PRESSURE SwiTCH FLOW _ WARNING LIGH BATTERY FLOW WARNING LIGHT CONNECTION 1 WATER INLET SoLENOID 4 METERING PRESSORE 7 DERICHMENT VALVE CONTROL 2 5 MAIN WATER JET 8 INTERyIEDIATE REAR CANKCASE HECK VALVE sett 6 DELAY BLEEDS WATER ENRICHMENT VALVE 158 134 Bendix Stromberg PR 58 3 Water Inlet Solenoid Control Valve AD1 ON Met
326. 210 6kg cm2 6 5 10 NE eae
327. 3 Battle of Britain 47ez777 1940 E 7 10 SU Bendix Stromberg Mk 70 76 77 85 66 1941 3 Miss Shilling s orifice 1942 48 Mark 66 Merlin SU Mer7zn 3 RAE Miss Tilly Shilling
328. 4 9 1940 9 E E 1 5 13 Schey cf Robert Schlaifer i C E Taylor N A C A C EK 1931 C E N A C A Q 5x7in hz7x177 8mm ML I T N A C A
329. 3 140 516 517 A S T M American Society of Testing Material 12 539 6 TT A S TLM 1940 1942 41 43 46 48 1943 79 81 181 E 208 214
330. 4 94 8 133 I 89 87 4 134 PED HH 86 3 3 2 4 42 2 2 1 90 42 2 22 33 32 10 15 34 3 In A 3 20 lt 30 3 G8
331. 86 37 2 EE 8 36 4 200m 50 1 070 E 7 800 PH 86 1 10 2kg cmz
332. i Bristol Rolls Royce 1931 A A Griffth Centaurus 1944 ezcz es 100 60 1945 59 AMercury 1942 H V Bendix Stromberg 60 ATDC 0
333. 98 10 5 18 5mm 19 0mm lt 1600rpm 150kg cm2 750mm3 1400rpm 3 76 2000HP 5 99 3 5HP 16 8kg DS4 82B 15 6kg 3kg 1 3 5kg 14 14
334. E 1 147 E
335. E11 E Morris SU Skinner s Union Carburetor Company RR SU Mk 100 MerZn 1 RR 1
336. P amp W 14 ADI
337. X R 3850 Wright Cyclone 18 CR 1 Boeing B 29 Duplex 9 cf O W Schey and J D Clark Comparative Performances of Engine Using a Carburetor Manifold Injection and Cyhnder Injection 4 C4 Technical Note No 688 1939 2 1 4 3 H 2
338. es aut Eras HH HH HH HH HHHHH HH BRNBH8H i i EE 1600 Ioo 1800 HH 11 HH i HH 2 9 5
339. B 29 Chester Marshall 2001 0 2 41 1939 1 2 6 2 4 1941 2 H f 12 5 42 14 49 1949 f 231 23 H 55 225 331 333 COs gt lt lt
340. H 7kg cm j 5 5kg cm2 70C 80 50 200mmHg 70C 10X20 90 112 162 0 5 70C 5 X6 2 5 2 5 j 7 23 5 S3 1 500HP 2 500rpm 1 800HP 2 000m 1 200HP 6 000m S2 50 130 0 3 44 4 40 DB 601 61 22 dnb 13 15 92
341. ce 9 RA 5 ew EE Ss FE Ss SS Dt Fr gt gt a a FRE FO et ars ox 7 lt i Sri Mi oo EE PE TE EE ORE RSE ER GE Ga EG CEs GE RE DEBE 52 30 NO Eee 29 EE Se Fl RE GE Ga EO SNR a i tm RE te SL EE IEEE EE EG EE i gt tt rt pS ee Es i a a 9 gt lt lt mm mm ee Fd We ts Wa GN RE DE SR 24 KS EE PR ha Rm TNE SE SEE DER 5 iss SAE ES SSE HOSP WET IRS RSE Ga DAS SA BOIS Po AR SE SB EEE ER gt Sh DS EE RA CCO 3 EA IR 85 at 9 kt Gn IS GS TERE FEE A Fs et tS DE Rt HR Us Ua a CEO FE RS 2 Ct DR EMR VC ER FE EHS EG FL YL SER The LIE BR TEE SE Br 26 fa A 9 Ba RG 5 i i Wa 3
342. 2 8 DB 601A DB 601A Me209 OM NUM 2 0 SN 2 100 E E 7 E 30 1 130 78
343. 42 DW ve 1 I 22 42 SERVO PISTON VANE PISTON 124379 1938 3 31 1935 8 22 255 258 43 TT 7 BELLONS FANGE WAVE ADIUS THNG SSCPEMN ALTITOUOE BELLOWS 7 PST ON OO 1 1
344. 11 23 42 8 DB 601A 43 62 EE 2 62 H E 3 100 DB 601A m 3
345. E Jumo 12 A 4 E Or 12 2mm E
346. 1 42 12 44 11 606 564 42 152 Fe 104 42 11 18 2R19 150 x 170mm 54 12 g 6 5 1900HP 2 450rpm 270mmHg 1610HP 2 350rpm 6 100m 2 151 2001 109 110 152 4 4 1959 208 217 1994 196 213 113 119
347. 46 BLANK NV CYLINOERS No A147 7 WV NOZZLE BLANK PLUG M 3 7 ON INSIOE OF Cr INOER BANK SAARK PLUG AERE SPARK PLUG OTATIONS FRONT fHEAR ERTED LVOTATIONS 2 LS MASERTED DEE TKEN WAITH FESPECT 7 ENGNNE LAY OUT ditto p 31 Fig 24 1 26 ditto D 30 2 2 Junkers gz2o211 Fig 23 23kg cm2 2 Ri 43 1953 114 E E 1957 116
348. FEF C53 3 H E 102 3 1mm 82 c b a de
349. R 3350 XPBB 1 Sea Ranger R 3350 1 R 8350 42 F 41 42 P amp W R 2800
350. 4 4 b 62 100 NM 3 SN I 5 62 1
351. I 98 42 2 18 1 tf b 28 40 14 14 14 28 21 22 87 23 91 145 42 2 14 11 28 2R14 150x170mm 1 859HP 2 600rpm 1 680HP 3 500m
352. 1
353. 185 R 3350 42WA 8800 57 42WA 7ezo 4 Zace aze Bear Grumman F8F Bear Cg7 R 3350 DC 7 4000 4700HP 3 200rpm 3 700 R 3350 2 186 cf Wilkinson Aircratt Engines of the World 792Z pp 256 257 266 267 DC 7 R 3350 EA1 Bosch
354. 1941 6 5 1942 1 22 526 41 P amp W 200 177 3 P amp W RR 179 176 lt i77
355. Bendix Stromberg 190 194 Stromberg Eclipse 1929 Bendix 9 12 5 Cyelone 552 10 1800rpm 1900rpm H 2 9
356. 140X150mm 0 83 1 91 0 26 80 91 1 3 13 6 1 50 163 84 0 2 0 3 r k b
357. 151 206 1943 12 ms ff NE ADI 4 67 839 12 40 9
358. 1941 12 8 100 Ss x B 10 41 44 1 E 4 h 1 6
359. 2 214 2 E 18 42 1 1 2 214 C 42 81 10 214 42 21 g 6 7 44 183 IN 153 154 No 32
360. 211 Zzzzo 213 TN Arsenal 12A 12H 52 ce oze R 2600 5mm 52 Gunston BMW 801 Shvetsov ASH 82 114 116 Bill 1996
361. 38 2694 90 990 39 1 I 87 90 28 1939 3 20 4
362. DB 601 G13 7 No 2 1943 6 78 79 NR 9 12 ul 1 9
363. 1 H 119 s RB 3 4 62 87 2 1937 4
364. 137 188 428 553 179 RM SAN ee 1941 12 Hy E 5 I 109 43
365. 1943 E5 5 3 50 1 Bristol 3 4 1 4 40 4 Stromberg a My Stronberg 1 1
366. 3 193 E gt A MM 192 W1 FILE 1986 12 26 1981 228 231 258 259 193 160 161 163 202
367. KO Fg a 253 87 300g HP h 50 1 6 i
368. 939 3 DB 601A 40 60 V 12 1 106 40 lt i Co jo IIE in NN NN 0 IK No 2
369. DB 601E 1 3 Ea
370. Deckel 1 42 BMW 801 AUTOMATIC MIXTURE CONTROL SPRING LOADED PINONS KEYED TO PLUNGERS HOUSING FOR ENGINE CONTROL MECHANISM CIRCULAR RACK ditto p 60 Fig 49 51 2 64 BMW 801 RA I 48 BMW 801
371. Stefan Zima Entwickkung Schnellautender Hochleistungmotoren in Friedrichshafen Dusseldorf 1987 S 698 Bild 248 Bosch PZ 12 HP 110 19 1 35 Daimler Benz DB 601 E DB 603 Winding edge Groove Return hole Filling hole Full Delivery Partial Delivery ditto p 46 Fig 36
372. H 1999 4 1969 1957 2 h 300mmHg 1 6 DB 6 1A 200mmHg 92 25 85 40 z 203 205 4
373. MI HH 3A 147349 142 BMW 801A I 96 3A 4 E 12 28 509 4 3 3 02 3 _ EK No 2 68
374. MS os So oe Tt Gs So Se Sn or Too Fs Ss De Fo Fo Es a Fs Ge Et Fs FS St nt et Da DS nn Rn a De Fs ove PR 4 u uqq EEFE EE i 9 fmm BE SF ESE ME VE RCT ZS EE FEEL EE EE ZR Ft Wt EEE Sl CS ES REE BE ES no a Pas BAR A EME TE EE 108 135
375. je ks o CzHs4Pb E A E 3 ps 70 30 0 145 H 2 000rpm 650 dopes 75
376. 444 445 18 108 109 110 P amp W R 2000 7wzn Wasp 14 cf S D Heron Development of Aviation Fuels in R Schleifer and S D Heron Development of Aircraft Engines 427 Fuels pp 646 651 Robert Schlaifer Development of Aircraft Engines ditto pp 222 230 15 cf A W Judge Automobile and Aircratt Engines London 1924 pp 456 457 ditto Srd ed 1936 pp 547 548 H R Ricardo The High Speed Internal Combustion Engine 4th ed London and Glasgow 1953 pp 37 39 314 110 4 2010 3 165
377. CK 101_ 1 102 9 1943 11 OH5A 9 0 5 Xx5 30 101 40 1981 18 62 1988 259 272 151
378. E 5 En FF
379. 100 62 1 207 100 150 10 0 5 2 400rpm 109 75 90 161 87 50 105 150 S3 11 830 2 5 0 18 S3 15 2 0 3 43 21
380. 1880 15 B Hopkinson 1913 14 50HP 3 172 h Sprayer 12 FE
381. 1927 MI 3 ft Y S 6 1945 3 1942 6 115 117 N A C A National Advisory Committee for Aeronautics NASA
382. 23 14BA10 5 s 5 145A 2 H OT OO 42 2 H 3
383. 4 1 m 3 000m 157 ME 4 14 1945 1 1 m 2 155 107 108 145 147 203 228
384. 29 80 50 33 33 54 2 81 32 31 32 I 5 M G Chandler 2 022 653 3 19 Z 27 28 P amp W Wasp 9 85 18 Msp Curtis Cozgze7or Wright Cyclone
385. 37 j 64 Clerk Standards 1919 4 120 65 x 152 4mm 6 76 2x127 0mm 3 482 fF 1 13 3 312 h pint 0 472 13 6 199 3g BHP h
386. RE C Mock E 84 1935 n Bendix Stromberg 9 14 R 1535 2wz Wasp Junior 2 1936 1
387. 1 500HP 2 600rpm 5 800m 160 20 161 62 7 3 20 1080HP 15 amp 10 500m 6 000m 8 000m 100 62
388. 11 fF 1940 12 18 148607 549 cooled EGR GGuper compression 3 LEMAJ No 487 2007 5 EGR H 1942 2 25 M 1 1
389. 177g HP h 192g HP h 220g HP h 1 600 F 195g HP h 12 210g 200g 177g 85 24 26 115 1 76 800 El HH ht EE 20 2
390. 183 Cyclone 7 975C18CB1 26WB ary 7urbo Cyclone R 3350 R 3350 wet
391. 1929 Stromberg 1940 39 R 975 Whirlwind R 1340 Wasp 1
392. x X 71 5 20 12 4 21 10kt 18 52kmh 910 1945 368 384 11 12 0 430 23 1H 175
393. 1 36 BMW 801 2 a 9 i ditto p 66 Fig 52 2 1 37 BMW 801 58 ditto p 69 Hig 54 RNN SN a NN SN SS 12NM 801A 1 a 0 EE TS 4 2 3 SS SS a ES 3 eS MM 0 OIL FROM ENGINE SYSTEM a NS NN G2 NN NNNNNN OIL OUTLET
394. 140 145 140 141 119 38 TPuelcharger M 3 Lincoln 10 E 37 1954 57 838 3
395. Allison E XP En i 8 1to3 V 12 9 14 American Bosch Eclipse Ex Cell O Eclipse
396. F 460 8 a 3 385 J 161 171 53 168 1 5 58 31 1944 11
397. FR FR SE log FE 5 We d Fr RE EE FE TS fea et 1300 P38 EE ER Et 5 EE EEE SEE RS SE EE HR OG ci gt a TO FE OE ae BC Bo RA EY 7 2 RK TMR RE SR BRR MP WS TE fs OF SM 4 KS oh 1 pem Fm 5 ma FEFFFFF FE FFSE
398. lt 1 m 2300km 167 c lt 0 4 112 IL IV 1 m 630 627 km h 1945
399. 40 8 Bendix 1939 N A C A R 1820 Cye oze Eclipse Eclipse Compur Bosch Robert Bosch American Bosch i i OTCTHDEET Compur 2
400. No 82 1982 7 4 1986 1987 110 lt 111 1999 18 30 189 8 E ADI 153 104 3 X 43 5 H 214 42 20
401. le ADI E 1 2 E ADI
402. 1 900rpm 500 1 960rpm 550 I 66 600 104 RE 0 1400 1500 690 iT00 00 400 000 2100 1 67 mmHgs H e0 0 00 200 300 105 T 68 nmHg 250 200 I50 100 50 0 00 200
403. 14 1 1 2mm3 77 I 50 1 77 2 1 81 64
404. 26 141 1 88 3 k 4 1940 1 10 39 2
405. 6 14 600 E 600 820HP 2 800rpm MR gt E 2R14 140 X150 82 32 650HP 2 100m A4 3 Ra 7 600HP 1931 NN 5 3 3 000m 600 1
406. Bayerische 155 5X156 1 2 3 1 6 57 1 801 801 23 801 801A 9 12 0mm 3 1 6
407. 1 28BHP 232g HP h RAE R 3270 Hobson R A E BL BH5 Ce gz Hobson R A E 49 0 1955 wet operation 3150HP 2800rpm L 867 868 140kg cem2 1 81 59 D R Pye 1943 206 209
408. 1576 47ez77 141 433 1 g 1 g 327 1200 zzzo 211 2400rpm 13 2m s 47ez777 3600rpm 18 288ams 84
409. 2004 129 cf The Engines of Pratt amp Whitney A Technicai History Maryland 2010 pp 135 pp 143 145 Doub7e Wasp 174 R 3350 P amp W 2 6 HO 4 1 i 3 1939 4 26 P amp W
410. 41 R 3350 0 1941 P amp W R 2800 41 1935 41 10
411. 43 5 50 96 97 23 22 22 54 C 47 H 53 99 20 21 22 23 H 52 DC 3 1 2
412. 9 B 1953 121 99 B 2 1 8000rpm 4 6000rpm 4 zzzo211 2300rpm 12 65m s
413. Victor F Bingham Major Piston Aero Engines of World War II Bath 1998 p 113 Derichment Valve Water Pressure Gage Connection M J Kroes T W Wild R D Bent J L Mckinley Aircraft Power Plants 6th ed N Y et al 1990 pp 146 147 EH 125 Kroes Wild Bent and Mckinley zzd pp 146 147 171 TO ENGINE FUEL DISCHARGE NOZZCE ss Fa oo eee TO UNMETERED FUEL CHAMBER 7 ia P GAGE CoONNECTION TO BLOWER THROAT ZZZ YAPOR VENT UNE NN a 5 WATER QUANTITY a AA 8 CA NN oO TL 2 ye 2 a 8
414. 75 2 DI 2 9 3 I 81 3 122 rj asnar mg b EO A 3 1 85 I 82 3 123 H 83
415. C F R C ER Coordinating Research Council American Petroleum Institute A PI Waukesha Motor Company 1933 8 6 15 tn A 2 NO C EFR
416. OH4A 20 1 33 Daimler Benz DB 601A Orange 53 83 3 mn ditto p 41 Fig 32 1941 3 3 ee RE 4 7o Yn 73 MM BA 86 Ve Oa THOIS Ve Prren S52 ym DIA NN ett tha RS LATER TYPE 7 es MN i NN 2 m f 4 gt NN N NA NUN NANNRR NN NN FARuY TvPE a hh OiA a79 mn OIA 6 HOLES 32 mn iA SQ k ENLARGED DETAIL OF TIP OF NOZZLE Daimler Benz DB 601E DB 603 EE 54 DB 601E 42 102 103
417. f 0 1 000 100 118 UA 10 El gt A E E H H
418. 5 23 H FE Yee 7 20 79 80 40 a 145 121584 185206 1937 3 15 rg ye 1936 1 23 241 148 1941 8 23 ara 1941 8 26 1941 8 br 1942 5 12 18 1942 5 22
419. 600 I 79 2 2 87 1941 1941 12 2002 111 SS 120 77 I 80 2 121 H
420. 32 33 48 1939 DB 601A 100 Ue A NS NSR 39 40 1 25 500 100 39 193 62 64 54 2
421. F 454 8 4 I 63 99 7 pLV HaA 9 MM 1 MM 7 82
422. i Junkers Zumo 211 Junkers Flugzeug und MotorenWerke A G 1936 211 mv12V 150x165 150 V 12 E 39 mo 37 cf Jan P Norbye Automotive Fuel Injection Sys7e729 A Technical Guide Rngland 1st ed Sparkford 1982 2nd ed ditto 1988 ch 4 7 1960 508 532 1963 372 P H Smith 38
423. 2 E G 36 Wasp E 87 Hy 3 4 2 E 24 1961
424. FrOSi TIOM Or FORAT RELATIVE TO PLUNGER OEVCLOFED VICw Or METER NG CARIN ES ditto p 67 Fig 53a 53b 1 4 801A 1600HP 1880HP 15100ft
425. Marshall B 29 30 327 328 1 8 09 157 4 500m A 374 2 B 29 1 m a ce gt B 29 i
426. 1 1 4 E 6 E 3 100 1 i 120 F re
427. 1280HP 2500rpm 300mmHg 2000m 1185HP 2500rpm 300mmHg 6000m The information contained in this manual was collected and compiled by Middletown Air Materiel Area Maintenance Division Personel under the supervision of T2 Collection Division Air Materiel Comand Wright Field Dayton Ohio 106 No 18 1978 11 O 157 I 108 62 tt 100 1 109 62 158 110 62
428. 1942 7 92 169 2 0 1 SI 92 2 EE 2 91 2 92 91
429. 4 5 78 1I 1 1 14 9 kg 15 5 10 kg 1 1 1 1 mm 185 180 mm 250 195 1kg I 56
430. 50 DS 4 82B IS 44 42 IG 43 12 i J 7 I8 6 i 8 7 6 1941 12 708 3 7 9 11 2 Stronberg 1948 12 667 669 1940 56 58 8 1942 61 61 1 64 62 Stromberg 46 3
431. 190g HP h R 8350 Cyclone 18 3 7 Centaurus 878 178 10 18 5 9 9 9 2 ADI
432. 3 9 re J 129 OO B Bosch 1936 2 3 1
433. 7 000ft 12 000ft GM 86 0 hl E Hy 37 25 P 26B 34 V 12 10 a 4 4 E 23
434. ANEROID AIR VENTURI TUBE lt THROT TLE UNIT REGULATOR MANUAL CONTROL LINK THROTTLE CONTROL LINK SPRAY NOZZLE ABOUT 5 PRESSURE SUPERCHARGER C Norcrodd and J D Quinn The Aviation Mechanic N Y and London 1941 p 897 Fig 887 1943 9 1961 62 63 75 77
435. ENRPICHMENT SC PISTON CON TOL CONTAOL CHAAMEER SELLOWS CONTEOL SCFEW ditto p 22 Fig 15 p 23 Hig 16 2 I 23 44 LORM GEAR FOR EXTERNAL a TON MANUAL CONT EOL ADIUSTNIENTS FCRK AND FOR 7 7Z VG LALVE OAT FIOIOST 4 SFESSURE ALANVIFOLD OUT SERVO LALVE AODLUSTMENT ER ALVE GEAR WAICH PETURFN OIL TT ROM _ 6 gt OM FACH NINSECTOR MANIFOLD FRESSURE CONTROL LINKAGE TEMPERATURE EZ 5 ditto p 19 Hig 13 1 24 45 Ot TRANSEER GRIOVE EROM PORT 3 TOLOLUME ON LEFT SIOE OF PISTON SECTION OF MALVE ANO PISTON IS TAKEN THRU THE PISTON PORTS THESE ARE DESIGNATED 1 2 3 4 NOICATES Z FILLEO PORTION OF A NOICATES OL FILLED PORTION OF MECHANISM AT
436. g de Havilland Spztfier 65 ercules 815 wetl2300HP 2900rpm Hobson R A E BI BH19M 2 2 Cezzgzgzzzs 173 2R18 146X178mm wet 2850HP 2800rpm Hobson R A E BI BC19M 2 2 62
437. 143 8 42 2 a 1940 9 3 42 2 42 2 41 9 42 2 3 9 12 DB 601 96
438. 149 600 1000 2 1 1 gt 2 100 9 0mm 28 10 5 Bosch 1 7
439. 91 4 12 C43 22 450mm 2 450mm 91 40 1 1
440. 20 1943 4 1 105 1949 1007 910 1945 429 62 112 L 100 92 wet 1580HP 2600rpm 500mmHg dry 1200HP 2500rpm 300mmHg wet 1620HP 2600rpm 500mmHg 900m wet 1490HP 2500rpm 300mmHg 5000m 1200HP 2500rpm 300mmHg rt
441. 31 31 2 34 lt I 15 9 DH93 23 RD 22 NN rN 8 1 11 8 12 10 9 489 4 1 38 3 7 12 25 4 8 9 10
442. 7 30 1941 12 23 88 ee 473 509 510 124 1940 10 7 1941 12 28 147853
443. ADI 3 ADI 200 215 E 1
444. 19 96 ab Q1 32 C Q4 bc A 29 D 242 19 26 ad 101 1 83 30 a g gt j
445. 4 338 7 1 1 1967 7 8 1962 3 1 5 1 1959 1 27 Convair 880 558 7 6 2 1954 92 6 14 35 85kg cm2
446. ii Marvel Marvel Carburetor Co 1928 Borg Warner Co 1926 M G Chandler 22 2 C E Taylor and E S Taylor 1942 E 1938 60 167 168 171 22 Stromberg Milton E Chandler
447. 1 34 2 H RR
448. 1 800 2 000 2 200rpm 3 000m 4 000m 5 000m 1 600 1 800 2 000 2 200rpm 80mmHg 2 000rpm 220g HP h 230g HP h 10g 5 500rpm
449. 1942 6 2 1 1941 148719 gt 1938 1837802 F 11 187 1 28 616 188 189 1942 4 10 585 O
450. 2SN A GA i NN ee 4 gt gt NS SA 2 NN NAN SL a A YNS gt 77 7 N RN NEA 2 2 SS2 St A SN Sv IENN NE NN 2 2 Il_ 1 NI EES SS A EL s 0 2 NN NN S ll NS SS 3 NN A 1 MO 21 I 8 M G Chandler 2 143 935 9 3 22 8 a lt MRR gt RR EN a NN NNN 2 NN gt N A NN A A MY 2 ES ON NN AA gt RR DL 1933 23 Wasp
451. 159 500mmHg I ESDP NE 1 E T 17 58 amp 10 720m IL SN 158 159 160 15 259 gt 2 H DB 601 40 228 289 100 92 V 188 112 I 62
452. 159 161 2 348 497 552 lt 553 PE 149955 1 6 51 RS 1945 115 116 161 1 273 F _ eS EC 206 3 j 26 I 1941 1 28 1 151268
453. Merlin 28 03 2 V 1710 2005 1973 286 L 170 257 265 196 H 130 0X150 0mm Merlin 187 2X152 4mm V 1710 139 7 X152 4mm 447ez77 V 1710 4 2 140x150 50x170
454. OZ TO AK ditto p 9 Hig 6 I 20 Junkers 2 L HOLES FOR RE FUEL METERING 7 _ ZZ cv CHECK VALVE MERSIN 2 c zezel cz EARANEE 05 22o lt 0 7 SS 2 Ne DENT ON AER THA S _ DRAWING 13 NOT_ TO C44 4 PL ONGER o BARREL 27 6 F547 EE LEARANEE 0003 0002 222 i ditto p 10 Fig 7 2 fi 41 B 40 I 21 NGA NN RSS C D
455. P amp W 1940 R 3350 41
456. amp W 3 Vol 2 No 4 1956 3 V 1710 v Victory The Story of the Allison V 1710 Aircraft Engine 1929 1948 Pennsylvanna 1998 pp 159 167 ADI cf Daniel D Whitney Lees tor P amp W 1979 127 124
457. of Aeronautics Vol I London 1938 p 260 Fig 21 68 NN A Anilole i P amp amp W ADI Roy Fedden Bristol 1988 RR 40 Anti Detonation Injection ADT Pratt amp Whitney
458. 1 x 1 95 F 2 2 92 1 3 90 4 87 5 85 6 77 91 92 2 0 1 100 90 1 2 92 91
459. 1 22 500mmHg zep 20 v 172 3 5
460. 1kg cm2 LH HA Bosch Eclipse i 2 N A C A 140kg cm2 10 20 1500rpm 1900rpm 7 cf C F Taylor E S Taylor and G L Williams Fuel Injection with Spark Ignition in an Otto Cycle Engine 4 E Transactions Vol 26 1931 8 1 Bendix Stromberg 112318 1932 6 21 85 9 21 1931 6 20 1 2 1
461. 2 12 V gzzzo 211 A DB 601 46 20 12LA107 o 107o 10mmm 10mm
462. 2 75 H Nayler amp E Ower Aviation of To Day London 1930 p 392 76 C F Taylor and E S Taylor 192 193 C FR 1921 27 1934 FH 4 H 64 5 65 64 68 Delco T Midgley 1 Lorraine 400HP upiter 420HP
463. 22 81 23 DS4 82B 1941 12 1942 7 698 68 6 2
464. 45 178 109 100 HI E 1017 97 850 198 174 l 7 3 91 3
465. 4501 35 9 86 3 4 5 I 59 600 91
466. E BI BH11 69 2 2 Rolls Royce 83 1927 1932 1 RR KKestre RAE Condor 50 62 o RR Merlin gzzzo 211
467. NNs I 72 110
468. RETURN OIL PRESSURE PINOICATES SAME AT BOOST OL PRESSURE PLISTON 1S SHONWN IN BALANCED POSITION EUAEN 2 FRO ORIVE NLECTOR ditto p 24 Fig 17 2 El I 25 Junkers Zumo 211
469. ering Pressure Control Valve ADI Check Valve Deley Breeds ADI ADI Full Rich Emergency Rich 172 Derichment Valve
470. pm 4 000m 80 5 b 2 k I 60 600 bb t i 7 750HP 2 200rpm 15C 94 I 61 600 EEE 8 HH HI i EE HE Fb EE HH HE H i BE
471. rplanes SAE Quarterly Transactions 2 1948 iv 1940 41 B 29 R 8350 Duplex Cyclone Bendix Stromberg Adapter injection R 3350
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