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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

Engines on display

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) at 1400 rpm

See also

Comparable engines

Related lists

References

Notes
  1. ^ a b c Gunston 1989, p. 92.
Bibliography
  • Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
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