Pratt & Whitney R-1830 Twin Wasp
The Pratt & Whitney R-1830 Twin Wasp was an American aircraft engine widely used in the 1930s and 1940s. Produced by Pratt & Whitney, it was a two-row, 14-cylinder, air-cooled radial design. It displaced 1,830 cu in (30.0 L) and its bore and stroke measured 5.5 and 5.5 in (140 and 140 mm), respectively. A total of 173,618 R-1830 engines were built.[1] An enlarged version with a slightly higher power rating was produced as the R-2000.
Variants
- R-1830-1 - 800 hp (597 kW)
- R-1830-9 - 850 hp (634 kW), 950 hp (708 kW)
- R-1830-11 - 800 hp (597 kW)
- R-1830-13 - 600 hp (447 kW), 900 hp (671 kW), 950 hp (708 kW), 1,050 hp (783 kW)
- R-1830-17 - 1,200 hp (895 kW)
- R-1830-21 - 1,200 hp (895 kW)
- R-1830-25 - 1,100 hp (820 kW)
- R-1830-33 - 1,200 hp (895 kW)
- R-1830-35 - 1,200 hp (895 kW) Fitted with GE B-2 turbosupercharger
- R-1830-41 - 1,200 hp (895 kW) Fitted with GE B-2 turbosupercharger
- R-1830-43 - 1,200 hp (895 kW)
- R-1830-45 - 1,050 hp (783 kW)
- R-1830-49 - 1,200 hp (895 kW)
- R-1830-64 - 850 hp (634 kW), 900 hp (671 kW)
- R-1830-65 - 1,200 hp (895 kW)
- R-1830-66 - 1,000 hp (746 kW), 1,050 hp (783 kW), 1,200 hp (895 kW)
- R-1830-72 - 1,050 hp (783 kW)
- R-1830-82 - 1,200 hp (895 kW)
- R-1830-86 - 1,200 hp (895 kW)
- R-1830-88 - 1,200 hp (895 kW)
- R-1830-90 - 1,200 hp (895 kW)
- R-1830-90-B - 1,200 hp (895 kW)
- R-1830-92 - 1,200 hp (895 kW)
- R-1830-94 - 1,350 hp (1,007 kW)
- R-1830-S1C3-G - 1,050 hp (783 kW), 1,200 hp (895 kW)
- R-1830-S3C4 - 1,200 hp (895 kW)
- R-1830-S3C4-G - 1,200 hp (895 kW)
- R-1830-S6C3-G - 1,100 hp (820 kW)
- R-1830-SC-G - 900 hp (671 kW)
- R-1830-SC2-G - 900 hp (671 kW), 1,050 hp (783 kW)
- R-1830-SC3-G - 1,065 hp (749 kW) Swedish unit built under license by SFA company for Finnish VL Myrsky II
Applications
Specifications (R-1830-S1C-G)
Data from [2]
General characteristics
- Type: Fourteen-cylinder two-row supercharged air-cooled radial engine
- Bore: 5.5 in (139.7 mm)
- Stroke: 5.5 in (139.7 mm)
- Displacement: 1,829.4 in³ (30 l)
- Length: 59.06 in (1,500 mm)
- Diameter: 48.03 in (1,220 mm)
- Dry weight: 1,250 lb (567 kg)
Components
Performance
See also
- Related development
- Comparable engines
- Related lists
References
- Angelucci, Enzo (1988, Revised Edition 2006). Complete Book of World War II Combat Aircraft. VMB Publishers. ISBN 978-88-540-0829-8.
- Bridgman, Leonard, ed. Jane's All The World's Aircraft 1951–1952. London: Samson Low, Marston & Company, Ltd 1951.
External links
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