Wright R-1820 Cyclone
The Wright R-1820 Cyclone 9 is an American radial engine developed by Curtiss-Wright, widely used on aircraft in the 1930s through 1950s. It was produced under license in France as the Hispano-Suiza 9V or Hispano-Wright 9V, and in the Soviet Union as the Shvetsov M-25.
| R-1820 Cyclone | |
|---|---|
![]()  | |
| Curtiss-Wright R-1820 Cyclone Radial Engine | |
| Type | Radial engine | 
| National origin | United States | 
| Manufacturer | Wright Aeronautical | 
| First run | 1930s | 
| Major applications | Boeing B-17 Flying Fortress  Curtiss P-36 Hawk Douglas B-18 Bolo Douglas DC-3 Douglas SBD Dauntless General Motors FM-2 Wildcat Sikorsky H-34  | 
| Number built | 47,475[1] | 
| Variants | Shvetsov M-25 | 
| Developed into | Wright R-2600  Wright R-3350  | 
Design and development
    
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 in 1931. The engine remained in production well into the 1950s.
The R-1820 was built under license by Lycoming, Pratt & Whitney Canada, and also, during World War II, by the Studebaker Corporation. The Soviet Union had purchased a license for the design, and the Shvetsov OKB was formed to metricate the American specification powerplant for Soviet government-factory production as the M-25, with the R-1820's general design features used by the Shvetsov design bureau for many of their future radials for the Soviet air forces through the 1940s and onwards. In Spain the R-1820 was license-built as the Hispano-Suiza 9V or Hispano-Wright 9V.[2]
The R-1820 was at the heart of many famous aircraft including early Douglas airliners (the prototype DC-1, the DC-2, the first civil versions of the DC-3, and the limited-production DC-5), every wartime example of the Boeing B-17 Flying Fortress and Douglas SBD Dauntless bombers, the early versions of the Polikarpov I-16 fighter (as the M-25), and the Piasecki H-21 helicopter.
The R-1820 also found limited use in armoured vehicles. The G-200 variant developed 900 hp (670 kW) at 2,300 rpm and powered the strictly experimental M6 Heavy Tank.
D-200 Diesel
    
The Wright R-1820 was converted to a diesel during World War II by Caterpillar Inc. as the D-200 and produced 450 hp (340 kW) at 2,000 rpm in the M4A6 Sherman.[3]
Variants
    
- R-1820-04
 - 700 hp (520 kW)
 - R-1820-1
 - 575 hp (429 kW)
 - R-1820-4
 - 770 hp (570 kW)
 - R-1820-19
 - 675 hp (503 kW)
 - R-1820-21
 - 690 hp (510 kW)
 - R-1820-22
 - 950 hp (710 kW)
 - R-1820-25
 - 675 hp (503 kW), 750 hp (560 kW), 775 hp (578 kW)
 - R-1820-32
 - 1,000 hp (750 kW)
 - XR-1820-32
 - 800 hp (600 kW)
 - R-1820-33
 - 775 hp (578 kW)
 - R-1820-34
 - 940 hp (700 kW), 950 hp (710 kW)
 - R-1820-34A
 - 1,200 hp (890 kW)
 - R-1820-40/42
 - 1,100 hp (820 kW), 1,200 hp (890 kW)
 - R-1820-41
 - 850 hp (630 kW)
 - R-1820-45
 - 800 hp (600 kW), 930 hp (690 kW)
 - R-1820-49
 - 975 hp (727 kW)
 - R-1820-50
 - 850 hp (630 kW)
 - R-1820-52
 - 1,000 hp (750 kW)
 - R-1820-53
 - 930 hp (690 kW), 1,000 hp (750 kW)
 - R-1820-56
 - 1,200 hp (890 kW), 1,350 hp (1,010 kW)
 - R-1820-57
 - 1,060 hp (790 kW)
 - R-1820-60
 - 1,200 hp (890 kW)
 - R-1820-62
 - 1,350 hp (1,010 kW)
 - R-1820-66
 - 1,200 hp (895 kW), 1,350 hp (1,007 kW)
 - R-1820-67/69
 - 1,200 hp (890 kW), fitted with turbosupercharger
 - R-1820-72W
 - 1,350 hp (1,010 kW), 1,425 hp (1,063 kW)
 - R-1820-74W
 - 1,500 hp (1,100 kW)
 - R-1820-76A,B,C,D
 - 1,425 hp (1,063 kW)
 - R-1820-77
 - 1,200 hp (890 kW)
 - R-1820-78
 - 700 hp (522 kW), 1,100 hp (820 kW)
 - R-1820-80
 - 700 hp (520 kW), 1,535 hp (1,145 kW)
 - R-1820-82WA
 - 1,525 hp (1,137 kW)
 - R-1820-84
 - 1,525 hp (1,137 kW)
 - R-1820-86
 - 1,425 hp (1,063 kW)
 - R-1820-97
 - 1,200 hp (890 kW), fitted with turbosupercharger
 - R-1820-103
 - 1,425 hp (1,063 kW)
 - SGR-1820-F3
 - 710 hp (530 kW), 720 hp (540 kW)
 - SGR-1820-F2
 - 720 hp (540 kW)
 - R-1820-F53
 - 770 hp (570 kW)
 - R-1820-F56
 - 790 hp (590 kW)
 - GR-1820-G2
 - 1,000 hp (750 kW)
 - R-1820-G3
 - 840 hp (630 kW)
 - R-1820-G5
 - 950 hp (710 kW)
 - R-1820-G101
 - 1,100 hp (820 kW)
 - R-1820-G102
 - 775 hp (578 kW)
 - GR-1820-G102A
 - 1,100 hp (820 kW)
 - R-1820-G102A
 - 1,100 hp (820 kW)
 - R-1820-G102A
 - 1,100 hp (820 kW)
 - R-1820-G202A
 - 1,200 hp (890 kW)
 - R-1820-G103
 - 1,000 hp (750 kW)
 - R-1820-G105
 - 1,000 hp (750 kW)
 - R-1820-G205A
 - 1,200 hp (890 kW)
 
Notes: Unit numbers ending with W indicate engine variants fitted with water-methanol emergency power boost systems.
Hispano-Suiza 9V
    
The Hispano-Suiza 9V is a licence-built version of the R-1820.[4]
- Hispano-Suiza 9Vr
 - 9V with reduction gear
 - Hispano-Suiza 9Vb
 - Hispano-Suiza 9Vbr
 - variant of the 9Vb with reduction gear[4]
 - Hispano-Suiza 9Vbrs
 - variant of the 9Vb with reduction gear and supercharger
 - Hispano-Suiza 9Vbs
 - variant of the 9Vb with supercharger[4]
 - Hispano-Suiza 9Vd
 - variant of the 9V[4]
 - Hispano-Suiza 9V-10
 - 429 kW (575 hp) driving fixed-pitch propeller
 - Hispano-Suiza 9V-11
 - as -10 but RH rotation
 - Hispano-Suiza 9V-16
 - 480 kW (650 hp) driving variable-pitch propeller, LH rotation
 - Hispano-Suiza 9V-17
 - as -16 but RH rotation
 
Applications
    
- Bloch MB.221
 - Boeing B-17 Flying Fortress
 - Boeing 307 Stratoliner
 - Brewster F2A Buffalo
 - Curtiss AT-32-A Condor
 - Curtiss SBC-4 Helldiver
 - Curtiss P-36 Mohawk
 - Curtiss SC Seahawk
 - Curtiss-Wright CW-21
 - Douglas A-33
 - Douglas B-18 Bolo
 - Douglas DC-2
 - Douglas DC-3 (DST, G-102 and G-202)
 - Douglas R4D-8/C-117D
 - Douglas DC-5
 - Douglas DF Wright SGR-1820G-2
 - Douglas SBD Dauntless
 - FMA AeMB.2 Bombi
 - General Motors FM-2 Wildcat
 - Grumman TF-1 / C-1 Trader
 - Grumman E-1 Tracer
 - Grumman FF
 - Grumman F3F
 - Grumman XF5F Skyrocket
 - Grumman XP-50
 - Grumman HU-16 Albatross
 - Grumman J2F Duck
 - Grumman S-2 Tracker
 - Lockheed Model 14 Super Electra
 - Lockheed Model 18 Lodestar
 - Lockheed Hudson
 - Martin B-10
 - North American A-27
 - North American O-47
 - North American P-64
 - North American T-28B/C/D Trojan
 - Northrop N-3PB
 - Northrop YC-125 Raider
 - Piasecki H-21
 - Polikarpov I-16
 - Ryan FR Fireball
 - Sikorsky S-58/HUS/HSS/H-34
 - Vultee V-1
 
Vehicles
    
Engines on display
    
Preserved Wright R-1820 engines are on display at the following museums:
- American Airlines C.R. Smith Museum[5]
 - Fleet Air Arm Museum
 - Delta Flight Museum
 - National Air and Space Museum
 - National Museum of the U.S. Air Force
 
Wright R-1820 Cyclone 9 engine of restored Douglas DC-3 "Flagship Knoxville" at American Airlines C.R. Smith Museum
Wright R-1820 cutaway at the Museum of Aviation
Wright R-1820 at the Museum of Aviation
Specifications (GR-1820-G2)
    
Data from Jane's. [6]
General characteristics
    
- Type: Nine-cylinder single-row supercharged air-cooled radial engine
 - Bore: 6.125 in (155.6 mm)
 - Stroke: 6.875 in (174.6 mm)
 - Displacement: 1,823 cu in (29.87 L)
 - Length: 47.76 in (1,213 mm)
 - Diameter: 54.25 in (1,378 mm)
 - Dry weight: 1,184 lb (537 kg)
 
Components
    
- Valvetrain: Two overhead valves per cylinder with sodium-filled exhaust valve
 - Supercharger: Single-speed General Electric centrifugal type supercharger, blower ratio 7.134:1
 - Fuel system: Stromberg PD12K10 downdraft carburetor with automatic mixture control
 - Fuel type: 87 octane rating gasoline
 - Oil system: Dry sump with one pressure and one scavenging pump
 - Cooling system: Air-cooled
 
Performance
    
- Power output: 1,000 hp (746 kW) at 2,200 rpm for takeoff
 - Specific power: 0.46 hp/in³ (20.88 kW/L)
 - Compression ratio: 6.45:1
 - Specific fuel consumption: 0.6 lb/(hp•h) (362 g/(kW•h))
 - Oil consumption: 0.35-0.39 oz/(hp•h) (13-15 g/(kW•h))
 - Power-to-weight ratio: 0.84 hp/lb (1.39 kW/kg)
 
See also
    
Related development
- Wright Cyclone family
 - Wright R-1300 Cyclone 7
 - Wright R-2600 Cyclone 14 (Twin Cyclone)
 - Wright R-3350 Cyclone 18 (Duplex Cyclone)
 - Shvetsov M-25
 - Shvetsov ASh-62
 
Comparable engines
Related lists
References
    
- "SUMMARY OF WRIGHT ENGINE SHIPMENTS 1920 – 1930" (PDF). Archived from the original (PDF) on 2021-10-10. Retrieved 2023-09-18.
 - Lage(2004) pp. 157-162
 - Conners, Medium Tank M4A1 Sherman (2013).
 - Hartmann, Gustave. Hispano-Suiza, Les moteurs de tous les Records.pdf (in French).
 - May, Joseph (8 January 2013). "Flagship Knoxville — an American Airlines Douglas DC-3". Hearst Seattle Media. Retrieved 3 August 2014.
 - Bridgman 1998, p. 314.
 
Bibliography
    
- 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.
 - Gunston, Bill. World Encyclopedia of Aero Engines: From the Pioneers to the Present Day. 5th edition, Stroud, UK: Sutton, 2006.ISBN 0-7509-4479-X
 - White, Graham. Allied Aircraft Piston Engines of World War II: History and Development of Frontline Aircraft Piston Engines Produced by Great Britain and the United States During World War II. Warrendale, Pennsylvania: SAE International, 1995. ISBN 1-56091-655-9
 - Lage, Manual (2004). Hispano Suiza in Aeronautics. Warrendale, USA: SAE International. ISBN 0-7680-0997-9.
 - "Aircraft Engines in Armored Vehicles". Archived from the original on 2006-10-07. Retrieved 2006-10-03.
 
