1980-12-11
1982-10-12
Stearns, Richard R.
Cutlery
308184R, 415113, F16C 2308, F16C 2704
Patent
active
043536042
ABSTRACT:
A friction damper is mounted in series with a viscous damper to accommodate the normal magnitude vibration and the higher magnitude vibration occasioned from a larger imbalance of a jet engine rotor manifested by a bowed rotor and including a loading spring to allow the recentering of said friction damper when the higher magnitude vibrations subside.
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Dulberger Michael D.
Hibner David H.
Moringiello Donald C.
Friedland Norman
Stearns Richard R.
United Technologies Corporation
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