Invention Grant
- Patent Title: Gas turbine component with platform cooling
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Application No.: US14854213Application Date: 2015-09-15
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Publication No.: US10465523B2Publication Date: 2019-11-05
- Inventor: Matthew A. Devore , Matthew S. Gleiner
- 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, P.C.
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D25/12 ; F01D9/02
Abstract:
A gas turbine engine component includes an airfoil that extends from a first side of a platform and a cooling passage that extends through the platform and includes an inlet located on a second opposite side of the platform. The inlet is located axially upstream of the airfoil.
Public/Granted literature
- US20160108738A1 GAS TURBINE COMPONENT WITH PLATFORM COOLING Public/Granted day:2016-04-21
Information query
