Vibration damper for aircraft engine

Details Vibration damper for aircraft engine Vibration damper for aircraft engine

2005-04-26

2005-04-26

Carone, Michael J. (Department: 3641)

Aeronautics and astronautics

Aircraft power plants

Transmission of power

C244S017110, C244S017270, C074S574300, C074S604000, C416S140000

Reexamination Certificate

active

06883752

ABSTRACT:
An internal combustion engine for an aircraft is described. The internal combustion engine includes a crankshaft defining first and second ends, a propeller, and a transmission disposed between the first end of the crankshaft and the propeller, operatively connecting the propeller to the crankshaft. A torsion bar is disposed between the first end of the crankshaft and the transmission, operatively connecting the crankshaft to the transmission. A torsional vibration damper is operatively connected at one of the first and the second ends of the crankshaft.

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