Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 13-Feb-2020

This American company has developed an engine that mixes theories of four-stroke and two-stroke engines.

Computerized representation of the engine
"Computerized representation of the engine"

-With oscillating plate and without valves to create cycles. It uses ports.

-Below wee see a test prototype in a photograph of its presentation during an Air Meeting in the year 2003.

Compound Engine on a test bench
"Compound Engine on a test bench"

-This test engine performs four effective strokes per revolution, and does not require pressure lubrication. It is very compact and hardly vibrates.

-It has an inner 2:1 reduction.

-It is a double-cylinder engine with a displacement of 1,200 cc. The delivered power is expected to be 80 hp evolving to 100 hp.

Engines of COMPOUND ENGINE CORP

Model: 80/100 HP (4T+2T)

Arquitecture: 2-cylinder Horizontally opposed
Cooling:
Total Displacement: 1200 cc
Bore / Stroke:
Power: 80 / 100 HP @ rpm
Weight:

Other details:

This test engine performs four effective strokes per revolution, and does not require pressure lubrication. It is very compact and hardly vibrates. It has an inner 2:1 reduction. With oscillating plate and without valves to create cycles. It uses ports.

Compound engine on a test bench

"Compound engine on a test bench"