Walter Venus

The Walter Venus was a seven-cylinder, air-cooled, radial engine for aircraft use, built in Czechoslovakia in the late 1920s.

Venus
Type Radial aircraft engine
National origin Czechoslovakia
Manufacturer Walter Aircraft Engines
First run 1929

Applications

Specifications

Data from Flight.[1]

General characteristics

  • Type: seven-cylinder radial engine
  • Bore: 105 mm (4.1 in)
  • Stroke: 120 mm (4.7 in)
  • Dry weight: 178 kg (393 lb)

Components

  • Valvetrain: Overhead valve, one inlet and one exhaust valve per cylinder
  • Fuel system: Zenith Type 50J carburettor
  • Fuel type: Petrol
  • Oil system: Pressure and scavenge pump
  • Cooling system: Air-cooled
  • Reduction gear: Direct-drive

Performance

See also

Related lists

References

  1. Flight - 25 July 1929, p. 762. Retrieved: 29 May 2012
  • Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 168.
  • Němeček, V. (1968). Československá letadla. Praha: Naše Vojsko.
  • moraviation.com
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.