Invention Grant
- Patent Title: Turbine engine component and method of cooling
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Application No.: US16356544Application Date: 2019-03-18
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Publication No.: US10941664B2Publication Date: 2021-03-09
- 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: F01D25/00
- IPC: F01D25/00 ; F01D5/18 ; F04D29/58 ; F02C7/18 ; F01D9/04 ; F01D9/06
Abstract:
A component for a turbine engine includes a body having a wall separating a combustion air flow path from a cooling air flow path. The component can include an isolation chamber formed in the cooling air flow path. The component can also include at least one cyclone separator having a cooling air inlet fluidly coupled to the cooling air flow path.
Public/Granted literature
- US20200300266A1 TURBINE ENGINE COMPONENT AND METHOD OF COOLING Public/Granted day:2020-09-24
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