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US Patent 10934935 Engine core assistance

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Is a
Patent
Patent

Patent attributes

Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
10934935
Date of Patent
March 2, 2021
Patent Application Number
15419040
Date Filed
January 30, 2017
Patent Citations
‌
US Patent 10090676 Aircraft DC power distribution systems and methods
Patent Citations Received
‌
US Patent 11988098 Increasing surge margin and compression efficiency via shaft power transfer
0
Patent Primary Examiner
‌
Gerald L Sung
Patent abstract

One example aspect of the present disclosure is directed to a method for operating a gas turbine engine. One example aspect of the present disclosure is directed to a method for operating a gas turbine engine, the gas turbine engine including at least a high pressure spool and a low pressure spool. The method includes causing, by one or more control devices, electrical power to be drawn from the high pressure spool and the low pressure spool into a power distribution system. The method includes determining, by the one or more control devices, a power adjustment event associated with the high pressure spool. The method includes initiating, by the one or more control devices, a power assist operation to redirect electrical power to the high pressure spool based at least in part on the power adjustment event.

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