Vibration damper for aircraft engine

Details Vibration damper for aircraft engine Vibration damper for aircraft engine

B - Operations, Transporting

64

D

B64D 35/00 (2006.01) B64D 27/04 (2006.01) F16F 15/10 (2006.01) F16F 15/173 (2006.01)

Patent

CA 2390289

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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