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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
North American T-28 Trojan
Number built 47,475[1]
Variants Shvetsov M-25
Developed into Wright R-2600
Wright R-3350

Design and development edit

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 edit

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 edit

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 edit

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 edit

Vehicles edit

Engines on display edit

Preserved Wright R-1820 engines are on display at the following museums:

Specifications (GR-1820-G2) edit

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

Performance

See also edit

Related development

Comparable engines

Related lists

References edit

  1. ^ (PDF). Archived from the original (PDF) on 2021-10-10. Retrieved 2023-09-18.
  2. ^ Lage(2004) pp. 157-162
  3. ^ Conners 2013.
  4. ^ a b c d Hartmann, Gustave. Hispano-Suiza, Les moteurs de tous les Records.pdf (in French).
  5. ^ May, Joseph (8 January 2013). "Flagship Knoxville — an American Airlines Douglas DC-3". Hearst Seattle Media. Retrieved 3 August 2014.
  6. ^ Bridgman 1998, p. 314.

Bibliography edit

  • Bridgman, L, (ed.) (1998) Jane's Fighting Aircraft of World War II. Crescent. ISBN 0-517-67964-7.
  • Conners, Chris (2013). "Medium Tank M4 Sherman". American Fighting Vehicle Database. Retrieved 9 January 2014.
  • 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.
  • . Archived from the original on 2006-10-07. Retrieved 2006-10-03.

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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 North American T 28 Trojan Number built 47 475 1 Variants Shvetsov M 25 Developed into Wright R 2600 Wright R 3350 Contents 1 Design and development 1 1 D 200 Diesel 2 Variants 2 1 Hispano Suiza 9V 3 Applications 3 1 Vehicles 4 Engines on display 5 Specifications GR 1820 G2 5 1 General characteristics 5 2 Components 5 3 Performance 6 See also 7 References 8 BibliographyDesign and development editThe 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 amp 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 edit 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 editR 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 edit 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 rotationApplications editBloch 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 edit M4A6 tank M6 heavy tankEngines on display editPreserved Wright R 1820 engines are on display at the following museums American Airlines C R Smith Museum 5 Fleet Air Arm Museum citation needed Delta Flight Museum citation needed National Air and Space Museum citation needed National Museum of the U S Air Force citation needed nbsp Wright R 1820 Cyclone 9 engine of restored Douglas DC 3 Flagship Knoxville at American Airlines C R Smith Museum nbsp Wright R 1820 cutaway at the Museum of Aviation nbsp Wright R 1820 at the Museum of AviationSpecifications GR 1820 G2 editData 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 in 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 editRelated 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 Alfa Romeo 128 BMW 114 Nakajima Hikari Pratt amp Whitney R 1830 Twin Wasp Bristol Pegasus Related lists List of aircraft enginesReferences edit 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 2013 a b c d 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 edit nbsp Wikimedia Commons has media related to Wright R 1820 Bridgman L ed 1998 Jane s Fighting Aircraft of World War II Crescent ISBN 0 517 67964 7 Conners Chris 2013 Medium Tank M4 Sherman American Fighting Vehicle Database Retrieved 9 January 2014 Eden Paul amp 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 Retrieved from https en wikipedia org w index php title Wright R 1820 Cyclone amp oldid 1200583606, wikipedia, wiki, book, books, library,

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