Top Qs
Timeline
Chat
Perspective

Pratt & Whitney R-2180-E Twin Wasp E

American radial aircraft engine From Wikipedia, the free encyclopedia

Pratt & Whitney R-2180-E Twin Wasp E
Remove ads

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.

Quick Facts R-2180-E Twin Wasp E, Type ...
Remove ads

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

Related lists

References

Loading related searches...

Wikiwand - on

Seamless Wikipedia browsing. On steroids.

Remove ads