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Wright R-4090 Cyclone 22

From Wikipedia, the free encyclopedia
Radial piston engine

R-4090 Cyclone 22
Type22-cylinder air-cooled two-rowradial piston engine
National originUnited States
ManufacturerWright Aeronautical
Number builtc. 3
Developed fromWright R-3350 Duplex-Cyclone

TheWright R-4090 Cyclone 22 was an American experimentalradial piston engine designed and built in prototype form byWright Aeronautical during the 1940s.

Design and development

[edit]

During the 1940s,Wright Aeronautical Corporation was constantly in competition withPratt & Whitney for new engine designs required for civil and military aircraft. Utilizing theWright R-3350 Duplex-Cyclone as a basis, Wright developed a 22-cylinder engine, using R-3350 cylinders arranged as a two-row radial engine with 11 cylinders per row instead of 9.[1]

The air-cooled R-4090 was rated to deliver 3,000 hp (2,200 kW) at 2,800 rpm for take-off, from a total displacement of 4,092 cu in (67.06 L), with a compression ratio of 6.85:1. Improved performance was expected from the R-4090 if there had been further development. A two-speed single-stage supercharger helped maintain rated power to higher altitudes.[1]

The core of the engine was a forged steel crankcase which enclosed the three piece two-throw crankshaft. The cylinders were arranged equally around the crankcase, with each row off-set by 16.3636.° to ensure cooling airflow. Accessories similar to other Cyclone engines were arranged around the rear face of the crankcase and a 0.333:1 planetary reduction gearbox at the front.[1]

Although there are no records of failings of the R-4090, the engine was abandoned to allow development of the R-3350 Duplex-Cyclone series.[1]

Variants

[edit]
XR-4090-1
(790C22AA1), drove a single propeller.[1]
R-4090-3
(792C22AA), drove a contra-rotating propeller shaft and was intended to have a two-speed reduction gearbox to maximize efficiency in cruising flight.[1]

Specifications (XR-4090-1)

[edit]

Data from enginehistory.org,[2] Old Machine Press[1]

General characteristics

  • Type: Air-cooled 22 cylinder two-row radial piston engine
  • Bore: 6.125 in (155.6 mm)
  • Stroke: 6.3125 in (160.3 mm)
  • Displacement: 4,092 cu in (67.06 L)
  • Length: 91 in (2,300 mm)
  • Diameter: 58 in (1,500 mm)
  • Dry weight: 3,230 lb (1,470 kg)

Components

  • Valvetrain: One inlet and one Sodium-cooled exhaust over-head valves per cylinder, driven by pushrods and rocker arms.
  • Supercharger: 14 in (360 mm) diameter impeller, single-stage two-speed supercharger; gear ratios: of 5 to 1 and 7 to 1.
  • Fuel type: Gasoline
  • Reduction gear: 0.333:1 planetary reduction gearbox

Performance

  • Power output: 3,000 hp (2,200 kW) at 2,800 rpm for take-off
  • Compression ratio: 6.85:1

See also

[edit]

Related development

Comparable engines

References

[edit]
  1. ^abcdefgPearce, William (22 March 2013)."Wright Aeronautical R-4090 Cyclone 22".oldmachinepress.wordpress.com. Retrieved24 September 2015.
  2. ^"Curtiss-Wright XR-4090 A 22-Cylinder Radial".enginehistory.org. Retrieved24 September 2015.

Bibliography

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  • 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
  • White, Graham (14 February 2006).R-4360: Pratt & Whitney's Major Miracle. Specialty Press.ISBN 1580071732.
  • USAF US Navy: Engine model designation system (revised 1 January 1950 ed.). Air Material Command. Retrieved24 September 2015.
  • The Wright Cyclones. Wright Aeronautical Corporation. 1942.
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