Pratt & Whitney XH-3130
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| XH-3130 / XH-3730 | |
|---|---|
| Type | 24-cylinder H-engine |
| National origin | United States |
| Manufacturer | Pratt & Whitney |
The Pratt & Whitney XH-3130 (sometimes called the XL-3130[citation needed]) was an H-block aircraft engine project developed for the United States Navy in the late 1930s.[1] The design was later enlarged as the XH-3730), but the project was canceled in 1940 in favor of Pratt & Whitney developing the R-4360 Wasp Major air-cooled radial engine.[2]
Contents
Specifications
General characteristics
- Type: 24 cylinder H-engine
- Bore: 6.00 in (152.4 mm)
- Stroke: 5.50 in (139.7 mm)
- Displacement: 3,732.2 cu in (61.16 L)
Components
Performance
- Power output: 2,900 hp
See also
- Related development
- Comparable engines
- Related lists
References
Notes
Bibliography
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