“Boeing T60”的意思、由来-开放百科全书

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Boeing T60

释义

Variants
Specifications (520-6)
See also
References

name = T60 / Model 520

image =

caption =

}}{{Infobox aircraft engine

type= Turboshaft / Turboprop

manufacturer= Boeing

national origin= United States

first run=

major applications=

number built =

program cost =

unit cost =

developed from = Boeing T50 / Model 502

developed into =

variants with their own articles =
}}

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

YT60-BO-2A: Military turboshaft version for testing.

520-2: (YT60-BO-2A) Free power turbine turboshaft rated at {{convert|475|hp|kW|abbr=on|2}}

520-4: Turboprop rated at {{convert|475|hp|kW|abbr=on|2}}

520-6: Direct drive turboshaft rated at {{convert|550|hp|kW|abbr=on|2}} military power

520-8: Turboprop rated at {{convert|550|hp|kW|abbr=on|2}}

Specifications (520-6)

{{jetspecs
|ref=Jane's All the World's Aircraft 1962-63^[1]
|type=Turboshaft
|length={{convert|54.1|in|mm|abbr=on|0}}
|diameter={{convert|25.14|in|mm|abbr=on|0}} maximum height
|weight={{convert|250|lb|kg|abbr=on|0}}
|compressor=Single-stage centrifugal flow
|combustion=2 reverse flow can combustors
|turbine=1x radial gas generator power turbine stage
|fueltype=Aviation kerosene
|oilsystem=pressure spray/splash, oil specification: MIL-L-7808
|power={{convert|550|hp|kW|abbr=on|2}} military rating at 6,000 output shaft rpm
|thrust=
|compression=6:1
|bypass=
|aircon={{convert|5.5|lb|kg|abbr=on|0}}/s
|turbinetemp=Jet pipe Temperature: {{convert|1,025|°F|°C}}
|fuelcon=
|specfuelcon=0.67 lb/(hp h) (0.41 kg/(kW h))
|power/weight=2.2 hp/lb (3.616 kW/kg)
|thrust/weight=
}}

References

1. ^{{cite book|last=Taylor|first=John W.R. FRHistS. ARAeS|title=Jane's All the World's Aircraft 1962-63|year=1962|publisher=Sampson, Low, Marston & Co Ltd|location=London}}

{{cite book |last= Gunston |first= Bill |title= World Encyclopedia of Aero Engines, 5th Edition |year= 2006 |publisher= Sutton Publishing Limited |location= Phoenix Mill, Gloucestershire, England, UK |isbn= 0-7509-4479-X |pages= 79 }}
{{cite book|last= Leyes II |first= Richard A. |author2=William A. Fleming |title= The History of North American Small Gas Turbine Aircraft Engines |publisher= Smithsonian Institution |location= Washington, DC |year= 1999 |pages= |chapter= |isbn= 1-56347-332-1 |url= }}
{{cite book|last=Taylor|first=John W.R. FRHistS. ARAeS|title=Jane's All the World's Aircraft 1962-63|year=1962|publisher=Sampson, Low, Marston & Co Ltd|location=London}}

1 : Turboshaft engines 1950–1959

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Variants

Specifications (520-6)

See also

References