Lawrance A-3
The Lawrance A-3 or Lawrance Model A was an American twin-cylinder aircraft piston engine. Designed by Charles Lawrance in the mid-1910s the engine was produced by the Lawrance Aero Engine Company and under license by Excelsior. Weighing 200 lb (90 kg) the engine produced 28 horsepower (21 kW).[1] A feature of this engine was the shared use of a single crankpin for both cylinders, this caused vibration as the pistons moved in the same direction.[1]
Applications
- Breese Penguin (flightless ground training aircraft)
- Driggs Dart
- Waco Cootie
- Shinnecock lightplane
Specifications
Data from Gunston.[1]
General characteristics
- Type: Two-cylinder, air-cooled horizontally opposed piston aircraft engine
- Dry weight: 200 lb (91 kg)
Components
- Cooling system: Air-cooled
Performance
- Power output: 28 hp (21 kW)
See also
- Comparable engines
- Related lists
References
- Notes
- 1 2 3 Gunston 1989, p. 92.
- Bibliography
- Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9