From Wikipedia, the free encyclopedia
The
Boeing T60
(company designation
Model 520
) was a family of small
turboshaft
/
turboprop
engines produced by
Boeing
, based on Boeing's earlier Model 500 gas generator and
Model 502 (T50)
turboshaft engines.
Variants
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]
- YT60-BO-2A
- Military turboshaft version for testing.
- 520-2
- (YT60-BO-2A) Free power turbine turboshaft rated at 475 hp (354.21 kW)
- 520-4
- Turboprop rated at 475 hp (354.21 kW)
- 520-6
- Direct drive turboshaft rated at 550 hp (410.13 kW) military power
- 520-8
- Turboprop rated at 550 hp (410.13 kW)
Specifications (520-6)
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]
Data from
Jane's All the World's Aircraft 1962?63
[1]
General characteristics
- Type:
Turboshaft
- Length:
54.1 in (1,374 mm)
- Diameter:
25.14 in (639 mm) maximum height
- Dry weight:
250 lb (113 kg)
Components
- Compressor:
Single-stage centrifugal flow
- Combustors
:
2 reverse flow can combustors
- Turbine
:
1x radial gas generator power turbine stage
- Fuel type:
Aviation kerosene
- Oil system:
pressure spray/splash, oil specification: MIL-L-7808
Performance
See also
[
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]
Related development
Related lists
References
[
edit
]
- ^
Taylor, John W.R. FRHistS. ARAeS (1962).
Jane's All the World's Aircraft 1962?63
. London: Sampson, Low, Marston & Co.
- 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
.
- Taylor, John W.R. FRHistS. ARAeS (1962).
Jane's All the World's Aircraft 1962-63
. London: Sampson, Low, Marston & Co Ltd.
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