Invention Grant
- Patent Title: Gas turbine engine component having platform cooling channel
- Patent Title (中): 燃气涡轮发动机部件具有平台冷却通道
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Application No.: US13539977Application Date: 2012-07-02
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Publication No.: US09303518B2Publication Date: 2016-04-05
- Inventor: Lawrence J. Willey , Matthew S. Gleiner , Russell Deibel
- Applicant: Lawrence J. Willey , Matthew S. Gleiner , Russell Deibel
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D9/06 ; F01D9/04
Abstract:
A component for a gas turbine engine according to an exemplary embodiment can include 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
- US20140003961A1 GAS TURBINE ENGINE COMPONENT HAVING PLATFORM COOLING CHANNEL Public/Granted day:2014-01-02
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