- Wright R-1820
The Wright R-1820 Cyclone 9 was an American
radial engine developed byCurtiss-Wright and widely used on 1930s through 1950s aircraft.History
The R-1820 Cyclone 9 represented a further development of the
Wright P-2 engine dating back to 1925. Featuring a greater displacement and a host of improvements, the R-1820 entered production in1931 . The engine remained in production well into the 1950s.The R-1820 was built under license by Lycoming,
Pratt & Whitney Canada and also, duringWorld War II , by theStudebaker Corporation . TheSoviet Union had purchased a license for the design, designated M-25, and theShvetsov OKB was formed to further develop the engine.The R-1820 was at the heart of many famous aircraft including the early Douglas airliners (prototype DC-1, the DC-2, earliest civilian versions of the DC-3, and the limited-production DC-5),
B-17 Flying Fortress andSBD Dauntless bombers, the early versions of thePolikarpov I-16 fighter (as M-25), and thePiasecki H-21 helicopter.The R-1820 also found limited use in armored vehicles in two forms. The G-200 was a 9-cylinder gas-burning radial that developed 900 hp @ 2,300 rpm and powered the
M6 Heavy Tank . The Wright RD-1820 was converted to a diesel byCaterpillar Inc. as the D-200 and produced 450 hp @ 2,000 rpm in the M4A6 Sherman.Models/Variants
Unit numbers ending in/with 'W' indicate engines fitted with water-methanol emergency power boost system.
* R-1820-1 - 575 hp (429 kW)
* R-1820-80 - 700 hp (522 kW)
* R-1820-78 - 700 hp (522 kW)
* R-1820-4 - 770 hp (574 kW)
* R-1820-F53 -770 hp (574 kW)
* R-1820-33 - 775 hp (578 kW)
* R-1820-G102 - 775 hp (578 kW) , 1,200 hp (895 kW)
* R-1820-F56 - 790 hp (589 kW)
* XR-1820-32 - 800 hp (596 kW)
* R-1820-G3 - 840 hp (626 kW)
* R-1820-50 - 850 hp (634 kW)
* R-1820-45 - 930 hp (694 kW)
* R-1820-22 - 950 hp (708 kW)
* R-1820-34 - 950 hp (708 kW)
* R-1820-53 - 1,000 hp (750 kW)
* GR-1820-G2 - 1,000 hp (750 kW)
* R-1820-G5 - 1,000 hp (750 kW)
* R-1820-G103 - 1,000 hp (750 kW)
* R-1820-G105 - 1,000 hp (750 kW)
* R-1820-G101 - 1,100 hp (820 kW)
* GR-1820-G102A - 1,100 hp (895 kW)
* R-1820-40 - 1,200 hp (895 kW)
* R-1820-60 - 1,200 hp (895 kW)
* R-1820-97 - 1,200 hp (895 kW), Fitted with turbosupercharger
* R-1820-G205A - 1,200 hp (895 kW)
* R-1820-62 - 1,350 hp (1,007 kW)
* R-1820-72W - 1,350 hp (1,007 kW) , 1,425 hp (1,063 kW)
* R-1820-86 - 1,425 hp (1,063 kW)
* R-1820-103 - 1,425 hp (1,063 kW)
* R-1820-74W - 1,500 hp (1,118 kW)
* R-1820-82WA - 1,525 hp (1,137 kW)pecifications (GR-1820-G2)
Applications
* Boeing
B-17 Flying Fortress
*Boeing C-75
*Brewster F2A
* CurtissSBC Helldiver
* CurtissSC Seahawk
*Curtiss-Wright CW-21
*Douglas A-33
*Douglas B-18
*Douglas DC-2
*Douglas DC-3 (DST, G-102 and G-202)
*Douglas DC-5
* DouglasSBD Dauntless
* GrummanAF Guardian
* General Motors FM-2 Wildcat
* GrummanHU-16 Albatross
* GrummanJ2F Duck
* GrummanS-2 Tracker
*Lockheed Lodestar
*Lockheed Hudson
*Martin B-10
*North American O-47
*North American P-64
* North AmericanT-28 Trojan
*Piasecki H-21
* RyanFR Fireball
* Sikorsky H-34 ChocktawVehicles
*
M6 Heavy Tank ee also
Related developments
* Wright Cyclone family
*Wright R-1300 Cyclone 7
*Wright R-2600 Cyclone 14
*Wright R-3350 Cyclone 18 (Duplex Cyclone)
*Shvetsov M-25
*Shvetsov ASh-62 Comparable engines
*Pratt & Whitney R-1830 Wasp
*Pratt & Whitney R-2000 References
* Bridgman, L, (ed.) (1998) "Jane's Fighting Aircraft of World War II." Crescent. ISBN 0-517-67964-7
* Eden, Paul & Soph Moeng, "The Complete Encyclopedia of World Aircraft." Amber Books Ltd. Bradley's Close, 74-77 White Lion Street, London, NI 9PF, 2002, ISBN 0-7607-3432-1), 1152 pp.
*
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