US Patent 10934866 Variable pitch change control method
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Patent abstract
A gas turbine engine includes a fan having a plurality of fan blades configured to rotate about a central axis of the gas turbine engine. Each fan blade is configured to pivot about a pivot axis that extends radially away from the central axis to vary a pitch of the fan blade. The fan further includes a counterforce system configured to resist forces that urge the fan blades away from their pitch positions during operation of the gas turbine engine.
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Patent Inventor Names
Patrick Bailey0
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US Patent 10934866 Variable pitch change control method
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Patent jurisdiction
Patent number
10934866
Date of patent
March 2, 2021
Patent application number
15962550
Date Filed
April 25, 2018
Patent primary examiner
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