Walter Regulus
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| Regulus | |
|---|---|
| 300px | |
| Walter Regulus II | |
| Type | Radial aero engine |
| National origin | Czechoslovakia |
| Manufacturer | Walter Aircraft Engines |
| First run | 1934 |
The Walter Regulus was a Czechoslovakian five-cylinder, air-cooled radial engine for powering light aircraft that first ran in 1934. The engine produced 186 kW (250 hp).[1][2]
Contents
Engines on display
A preserved example of the Walter Regulus engine is on display at the following museum:
Specifications (Regulus)
General characteristics
- Type: 5-cylinder radial piston engine
Components
- Valvetrain: One intake and one exhaust valve per cylinder
- Fuel system: Carburettor
- Fuel type: Petrol
- Cooling system: Air-cooled
Performance
- Power output: 186 kW (250 hp)
See also
- Comparable engines
- Related lists
References
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Notes
- ↑ Gunston 1989, p. 174.
- ↑ Flight - November 1934 Retrieved: 19 October 2010
Bibliography
- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
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