Wright R-4090 Cyclone 22
| R-4090 Cyclone 22 | |
|---|---|
| Type | 22 cylinder air-cooled two-row radial piston engine |
| National origin | United states of America |
| Manufacturer | Wright Aeronautical Corporation |
| Number built | ~3 |
The R-4090 Cyclone 22 was an experimental radial piston engine designed and built in prototype form in the United States during the 1940s.[1]
Design and development
During the 1940s, Wright Aeronautical Corporation was constantly in competition with Pratt & Whitney for new engine designs required for civil and military aircraft. Utilising the Wright R-3350 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.[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 it was proceeded with. 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 Cyclone 18 series.[1]
Variants
- 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 maximise efficiency in cruising flight.[1]
Specifications (XR-4090-1)
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
References
Further reading
- White, Graham (1995). 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, PA: Soc. of Automotive Engineers. ISBN 978-1560916550.
- 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. Retrieved 24 September 2015.
- The Wright Cyclones. Wright Aeronautical Corporation. 1942.