Invention Application
- Patent Title: GAS TURBINE ENGINE THERMAL MANAGEMENT
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Application No.: US17188668Application Date: 2021-03-01
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Publication No.: US20220275757A1Publication Date: 2022-09-01
- Inventor: Jeffrey Douglas Rambo , Brandon Wayne Miller , Kevin Robert Feldmann , Patrick Michael Marrinan , Robert Jon McQuiston
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Main IPC: F02C7/18
- IPC: F02C7/18 ; F01D25/12
Abstract:
A method is provided of controlling a cooled cooling air system for an aeronautical gas turbine engine. The method includes: receiving data indicative of an ambient condition of the aeronautical gas turbine engine, data indicative of a deterioration parameter of the aeronautical gas turbine engine, data indicative of an operating condition of the aeronautical gas turbine engine, or a combination thereof; and modifying a cooling capacity of the cooled cooling air system in response to the received data indicative of the ambient condition of the aeronautical gas turbine engine, data indicative of the deterioration parameter of the aeronautical gas turbine engine, data indicative of an operating condition of the aeronautical gas turbine engine, or the combination thereof.
Public/Granted literature
- US11788470B2 Gas turbine engine thermal management Public/Granted day:2023-10-17
Information query
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