Invention Grant
- Patent Title: Method for thermal management for an aircraft propulsion system using a flow of compressed fluid extracted from a compressor section
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Application No.: US17164208Application Date: 2021-02-01
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Publication No.: US11897624B2Publication Date: 2024-02-13
- Inventor: Jeffrey Douglas Rambo , Scott Gregory Edens
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Dority & Manning, P.A.
- Main IPC: B64D33/08
- IPC: B64D33/08 ; B64D33/04

Abstract:
A method and structure for thermal management for a vehicle is provided. The method includes extracting a flow of compressed fluid from a compressor section of a propulsion system in which the flow of compressed fluid includes a pressure parameter, and generating an output torque via expanding at least a portion of the flow of compressed fluid across a turbine operably connected to a driveshaft. The turbine is positioned downstream of the compressor section and upstream of a cooling system.
Public/Granted literature
- US20220242587A1 METHOD AND SYSTEM FOR THERMAL MANAGEMENT Public/Granted day:2022-08-04
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