US Patent 6883752 Vibration damper for aircraft engine
Patent 6883752 was granted and assigned to Brp-Rotax Gmbh & Co Kg on April, 2005 by the United States Patent and Trademark Office.
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Patent 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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Patent Number
Patent Inventor Names
Johann Bayerl0
Thomas Koch0
Date of Patent
April 26, 2005
0Patent Application Number
100712330
Date Filed
February 11, 2002
0Patent Primary Examiner
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US Patent 6883752 Vibration damper for aircraft engine
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