Vibration damper for aircraft engine
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United States of America Patent
Stats
-
Apr 26, 2005
Grant Date -
May 15, 2003
app pub date -
Feb 11, 2002
filing date -
Nov 14, 2001
priority date (Note) -
Expired
status (Latency Note)
Importance
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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