Pratt & Whitney XH-3130: Difference between revisions
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Revision as of 06:03, 25 August 2015
| 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]
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
- Connors, Jack (2010). The Engines of Pratt & Whitney: A Technical History. Reston. Virginia: American Institute of Aeronautics and Astronautics. ISBN 978-1-60086-711-8.
{{cite book}}: Cite has empty unknown parameter:|coauthors=(help) - Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. ISBN 0-7509-4479-X.
{{cite book}}: Cite has empty unknown parameter:|coauthors=(help) - Gunston, Bill (1999). The Development of Piston Aero Engines, 2nd Edition. Sparkford, Somerset, England, UK: Patrick Stephens, Haynes Publishing. ISBN 0-7509-4478-1.
{{cite book}}: Cite has empty unknown parameter:|coauthors=(help)
