Invention Grant
- Patent Title: Engine core assistance
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Application No.: US15419040Application Date: 2017-01-30
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Publication No.: US10934935B2Publication Date: 2021-03-02
- Inventor: Manish Ashvinkumar Dalal , Paul Robert Gemin
- Applicant: GE Aviation Systems LLC
- Applicant Address: US MI Grand Rapids
- Assignee: GE Aviation Systems LLC
- Current Assignee: GE Aviation Systems LLC
- Current Assignee Address: US MI Grand Rapids
- Agency: Dority & Manning, P.A.
- Main IPC: F02C7/32
- IPC: F02C7/32 ; F02C6/14 ; F02C6/20 ; F02C7/36 ; F02C6/00 ; F02C9/16 ; F01D15/10 ; H02P101/30

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.
Public/Granted literature
- US20180216526A1 Engine Core Assistance Public/Granted day:2018-08-02
Information query
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