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Contents

   



(Top)
 


1 Applications  





2 Bristol Theseus on public display  





3 Variants  





4 Specifications (Theseus Th.21)  



4.1  General characteristics  





4.2  Components  





4.3  Performance  







5 See also  





6 References  



6.1  Notes  





6.2  Bibliography  







7 External links  














Bristol Theseus






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From Wikipedia, the free encyclopedia
 


Theseus
Preserved Bristol Theseus
Type Turboprop
Manufacturer Bristol Siddeley
First run 18 July 1945
Major applications Handley Page Hermes

The Theseus was the Bristol Aeroplane Company's first attempt at a gas-turbine engine design. A turboprop delivering just over 2,000 hp (1,500 kW) was chosen rather than compete with companies that were already developing turbojets. A heat exchanger to transfer waste heat from the exhaust to the compressor exit was necessary to meet a requirement for a fuel consumption comparable to a piston engine. However, the heat exchanger was abandoned after tests showed that it had a high pressure loss and only produced a fuel saving of 8%. Furthermore overall performance was reduced [1] [2]

As well as being one of the first engines to feature a free propeller turbine, the Theseus was the first turboprop in the world to pass a type test in January 1947.[3] Following 156 hours of ground runs and the receipt of a test certificate from the Ministry of Supply on 28 January 1947, two Theseus engines were fitted in the outer positions of a four-engined Avro Lincoln for air tests.[4] After ground and taxying test the Lincoln first flew on 17 February 1947.[4]

The engine was also installed in two Handley Page Hermes 5 development aircraft.[5]

It was soon superseded by the Proteus design with more power.

Applications

[edit]

Bristol Theseus on public display

[edit]

East Midlands Aeropark Castle Donington.

Variants

[edit]
Theseus Series TH.11
Variant without heat exchanger. Ran for first time July 18, 1945
Theseus Series TH.21
Variant with heat exchanger. Ran for first time in December, 1945
Theseus 502

Specifications (Theseus Th.21)

[edit]

Data from Aircraft Engines of the world 1946[7]

General characteristics

Components

Performance

See also

[edit]

References

[edit]

Notes

[edit]
  1. ^ Making Jet Engines in World War II: Britain, Germany, and the United States', Hermione Giffard 2016,University of Chicago,p.114-115
  • ^ Turbojet History And Development 1930-1960 Volume 1, Antony Kay2007, ISBN 978 1 86126 912 6, p.139
  • ^ http://www.flightglobal.com/pdfarchive/view/1947/1947%20-%200602.html [dead link]
  • ^ a b "Theseus Air Testing - First Bristol Airscrew Turbines Fly in a Lincoln : Some Features Discussed". Flight: 270. 27 March 1947.
  • ^ Gunston 1989, p.34.
  • ^ Test bed only
  • ^ Wilkinson, Paul H. (1946). Aircraft Engines of the world 1946. London: Sir Isaac Pitman & Sons. pp. 284–285.
  • ^ a b c d e f Practical Mechanics, February 1947, p.172
  • ^ a b Practical Mechanics, January 1947, p.116-118
  • Bibliography

    [edit]
    • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
    [edit]
    Retrieved from "https://en.wikipedia.org/w/index.php?title=Bristol_Theseus&oldid=1176417423"

    Categories: 
    1940s turboprop engines
    Bristol aircraft engines
    Mixed-compressor gas turbines
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    This page was last edited on 21 September 2023, at 16:11 (UTC).

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