Invention Grant
- Patent Title: Turbine engine component and method of cooling
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Application No.: US16356595Application Date: 2019-03-18
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Publication No.: US11306655B2Publication Date: 2022-04-19
- Inventor: Daniel Endecott Osgood , Jonathan Russell Ratzlaff , Kirk D. Gallier
- 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: McGarry Bair PC
- Main IPC: F01D25/32
- IPC: F01D25/32 ; F01D25/12 ; F02C7/052 ; F02C7/18 ; F01D9/04 ; B01D45/16
Abstract:
A component for a turbine engine includes a body having a wall at least partially defining an interior and separating a combustion air flow path from a cooling air flow path. The component also includes at least one fluid inlet supplying cooling air to the interior of the body, as well as a cyclone separator.
Public/Granted literature
- US20200300163A1 TURBINE ENGINE COMPONENT AND METHOD OF COOLING Public/Granted day:2020-09-24
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