| T50 |
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| A QH-50D anti-submarine drone aboard the USS Allen M. Sumner (DD-692) in the late 1960s, with the T50 engine visible on the right |
| Type |
Turboshaft |
| National origin |
United States |
| Manufacturer |
Boeing |
| Major applications |
QH-50 DASH |
The Boeing T50 (company designation Model 502) was a small turboshaft engine produced by Boeing. Based on Boeing's earlier Model 500 gas generator, the T50's main application was in the QH-50 DASH helicopter drone of the 1950s. An up-rated version designated Model 550 was developed to power the QH-50D and was given the military designation T50-BO-12.
Variants[edit]
- T50-BO-4
- 270 hp (201.34 kW) at 6,000 output rpm, military rating turboprop.[1]
- T50-BO-6
- T50-BO-8
- 300 hp (223.71 kW) at 5,950 output rpm, revised reduction gear ratio, fuelsystem and other changes.[1]
- T50-BO-8A
- T50-BO-10
- 330 hp (246.08 kW) at 6,000 output rpm[1]
- T50-BO-12
- 502-10C
- 502-10V
- (T50-BO-4)
- 502-10VB
- 325 hp (242.35 kW) at 3,000 output rpm, variant of -10V / T50-B0-4 with revised reduction gear ratio.[1]
- 502-10VC
- (T50-BO-8)
- 502-11
- 502-12B
- 502-W
- 502-14
- (T50-BO-10)
- 550-1
- (T50-BO-12)
Applications[edit]
- T50 (Model 502)
- GT502
Specifications (T50-BO-10 / 502-14)[edit]
Data from Jane's All the World's Aircraft 1962-63[1]
General characteristics
- Type: Turboshaft
- Length: 37.2 in (945 mm)
- Diameter: 22.5 in (572 mm)
- Dry weight: 215 lb (98 kg)
Components
- Compressor: Single-stage centrifugal flow
- Combustors: 2 can combustors
- Turbine: 1x axial gas generator power turbine stage + 1x axial free-power turbine stage
- Fuel type: Aviation kerosene
- Oil system: pressure spray/splash, oil specification: MIL-L-7808
Performance
See also[edit]
- Related lists
- ^ a b c d e Taylor, John W.R. FRHistS. ARAeS (1962). Jane's All the World's Aircraft 1962-63. London: Sampson, Low, Marston & Co Ltd.
References[edit]
- Taylor, John W.R. FRHistS. ARAeS (1962). Jane's All the World's Aircraft 1962-63. London: Sampson, Low, Marston & Co Ltd.
- Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. p. 79. ISBN 0-7509-4479-X.
- Leyes II, Richard A.; William A. Fleming (1999). The History of North American Small Gas Turbine Aircraft Engines. Washington, DC: Smithsonian Institution. ISBN 1-56347-332-1.
External links[edit]
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