Invention Grant
- Patent Title: Gas turbine engine component having platform cooling channel
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Application No.: US15056116Application Date: 2016-02-29
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Publication No.: US09845687B2Publication Date: 2017-12-19
- Inventor: Lawrence J. Willey , Matthew S. Gleiner , Russell Deibel
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D9/06 ; F01D9/04 ; F01D25/12 ; F04D29/32 ; F04D29/54 ; F04D29/58
Abstract:
A component for a gas turbine engine includes a platform having an outer surface and an inner surface. A cover plate can be positioned adjacent to the outer surface of the platform. The outer surface of the platform can include a pocket and the cover plate is positioned relative to the pocket to establish a platform cooling channel therebetween.
Public/Granted literature
- US20160245096A1 GAS TURBINE ENGINE COMPONENT HAVING PLATFORM COOLING CHANNEL Public/Granted day:2016-08-25
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