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Clerget 7Z

From Wikipedia, the free encyclopedia
7Z
TypeRotary engine
National originFrance
ManufacturerClerget-Blin
First run1913
Major applicationsAvro 504
Number built600 (French production)
347 (British production)
Developed fromClerget 7Y

The Clerget 7Z was a seven-cylinder rotary aircraft engine of the World War I era designed by Pierre Clerget. First appearing in 1913 it was nominally rated at 80 horsepower (60 kW). In addition to the 600 engines built in France by Clerget-Blin,[1] 347 examples were built under license in Britain by Gordon Watney & Co Ltd of Weybridge and Gwynnes Limited of Hammersmith.[2]

A French twin engine Caudron G4 fitted with Clerget rotary engines

Applications

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Specifications (Clerget 7Z)

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Data from Lumsden and Gunston.[2][3][4]

General characteristics

Components

  • Valvetrain: 1 each overhead inlet and exhaust valves operated by pushrods and rockers
  • Fuel system: Bloctube carburettor
  • Fuel type: Gasoline with Castor oil lubricant
  • Oil system: Castor oil mixed with fuel
  • Cooling system: Air-cooled

Performance

See also

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Comparable engines

Related lists

References

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Notes

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  1. Hartmann, Gerard (2003). "La société des moteurs Clerget" [The Clerget Motor Company] (PDF) (in French). Retrieved 11 September 2024.
  2. 1 2 Lumsden 2003, p. 133.
  3. Gunston 1989, p, 41.
  4. Grey, C.G. (1969). Jane's All the World's Aircraft 1919 (Facsimile ed.). David & Charles (Publishing) Limited. pp. 1b to 145b. ISBN 978-0-7153-4647-1.

Bibliography

[edit]
  • Grey, C.G. (1969). Jane's All the World's Aircraft 1919 (Facsimile ed.). David & Charles (Publishing) Limited. pp. 1b to 145b. ISBN 978-0-7153-4647-1.
  • Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.