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Pratt & Whitney R-2180-E Twin Wasp E
American radial aircraft engine From Wikipedia, the free encyclopedia
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The Pratt & Whitney R-2180-E Twin Wasp E was a radial aircraft engine developed in the United States by Pratt & Whitney. It had two rows of seven cylinders each. Its only production application was on the post-World War II Saab 90 Scandia airliner.
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Design and development
The R-2180-E is effectively a fourteen-cylinder simplification of the twenty-eight cylinder R-4360 Wasp Major engine; its cylinders are the same size and displacement as those of the Wasp Major.[1]
The R-2180-E Twin Wasp E was available in a "power-egg" installation certificated in 1945 for use as an engine upgrade for the Douglas DC-4.[2]
Applications
Specifications (R-2180-E1)
Data from Aviation Week[4]
General characteristics
- Type: 14-cylinder, supercharged, air-cooled, twin-row radial engine
- Bore: 5.75 in. (146 mm)
- Stroke: 6.00 in. (152 mm)
- Displacement: 2,181 in³ (35.7 L)
- Length: 76.20 in (1.94 m)
- Diameter: 54 in (1.37 m)
- Dry weight: 1,870 lb (850 kg)
Components
- Fuel system: Stromberg AR-48C1
- Fuel type: 100/130 octane
- Cooling system: Air-cooled
Performance
- Power output:
- Take-off without water injection: 1,650 hp (1,230 kW)
- Take-off with water injection: 1,800 hp (1,300 kW)
- Max continuous: 1,400 hp (1,000 kW)
- Normal: 1,300 hp (970 kW)
- Compression ratio: 7:1
See also
Related development
- Pratt & Whitney R-2180-A Twin Hornet
- Pratt & Whitney R-1830 Twin Wasp
- Pratt & Whitney R-2000 Twin Wasp
- Pratt & Whitney R-2800 Double Wasp
- Pratt & Whitney R-4360 Wasp Major
Related lists
References
External links
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