US Patent 10436064 Bowed rotor start response damping system
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Patent abstract
A method of bowed rotor start response damping for a gas turbine engine is provided. A spring rate and a damping characteristic of one or more bearing supports in the gas turbine engine are selectively modified while a shaft of the gas turbine engine rotates below a speed which is adversely affected by a bowed rotor condition of the gas turbine engine.
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Patent Inventor Names
Gregory M. Savela0
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Patent Number
104360640
Date of Patent
October 8, 2019
0Patent Application Number
150423460
Date Filed
February 12, 2016
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US Patent 10436064 Bowed rotor start response damping system
Infobox
Is a
Patent jurisdiction
Patent number
10436064
Date of patent
October 8, 2019
Patent application number
15042346
Date Filed
February 12, 2016
Patent primary examiner
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