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词条 Northrop-Hendy XT37
释义

  1. Design and development

     Turbodyne I  XT37 

  2. Specifications (Northrop-Hendy Turbodyne I)

  3. See also

  4. References

{{short description|1940s American turboshaft engine}}
name= T37image=caption=

}}{{Infobox Aircraft Engine

type= Turbopropnational origin = United Statesmanufacturer= Turbodynefirst run= 1944major applications= Northrop EB-35B proposednumber built =program cost =unit cost =developed from =developed into =variants with their own articles =
}}

The Northrop-Hendy T37 Turbodyne was an American turboprop engine developed by the Turbodyne Division of Northrop in the late 1940s.

Design and development

Turbodyne I

Northrop undertook a private venture to develop a turboprop engine from 1939 and was awarded a joint US Army/US Navy contract in 1941 for design, analysis and fabrication of a researchcompressor for the proposed engine. The contract was amendedl ater to call for construction of two complete engine prototypes.

Northrop had neither the space or expertise to fabricate the engines in a reasonable time-scale so they joined forces with the Joshua Hendy Iron Works in 1944 to form the Northrop-Hendy company. the two prototype engines were completed and test run in late 1944, but the first engine compressor failed, destroying the engine. Meanwhile the USN cancelled their interest in the engine in 1945, leaving the US Army to carry on. Testing continued with the second engine until that too failed, terminating the programme.[1]

Throughout testing the prototype engines failed to meet performance estimates due to poor compressor and turbine efficiencies.[1]

XT37

Northrop-Hendy continued their parftnership to develop the XT37, a large turboprop, expected to deliver ca {{cvt|10000|shp}}, but this too failed to deliver on the promised performance.[1]

Specifications (Northrop-Hendy Turbodyne I)

{{jetspecs
|ref=[2], [3], NASM[1]
|type=Turboprop
|length={{cvt|93|in}}
  • Width: {{cvt|41|in}}
  • Height: {{cvt|63|in}}

|weight={{cvt|7000|lb}}
|compressor= 18-stage axial compressor
|combustion=annular combustion chamber with eight flame tubes
|turbine=4-stage axial-flow
|fueltype=JP-4
|oilsystem=Pressure spray with scavenge
|power={{cvt|2400|shp}} at 10,000 rpm
|thrust=
|compression=
|bypass=
|aircon=
|turbinetemp=
|fuelcon=
|specfuelcon={{cvt|0.58|lb/hp/h}}
|power/weight={{cvt|2.32|hp/lb}} eqivalent
|thrust/weight=
}}

See also

{{Aircontent
|related=
|similar engines=
|lists=
  • List of aircraft engines

|see also=
}}

References

1. ^{{cite web |title=Northrop-Hendy Turbodyne I Turboprop Engine |url=https://airandspace.si.edu/collection-objects/northrop-hendy-turbodyne-i-turboprop-engine |website=National Air and Space Museum |accessdate=6 February 2019 |language=en |date=17 March 2016}}
2. ^{{cite book |last1=Earnes |first1=J.P. |title=Turbine- and Jet-propelled Aircraft Powerplants |date=1954}}
3. ^{{cite web |last1=Culy |first1=Doug |title=Wright's T35 Turboprop Engine, et al. |url=http://www.enginehistory.org/GasTurbines/Wright/T35/WrightT35.shtml |website=www.enginehistory.org |accessdate=6 February 2019}}
{{USAF gas turbine engines}}{{DEFAULTSORT:Northrop T37}}

1 : Turboprop engines 1940–1949

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