Invention Application
- Patent Title: GAS TURBINE COMPONENT WITH PLATFORM COOLING
- Patent Title (中): 气体涡轮组件与平台冷却
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Application No.: US14854213Application Date: 2015-09-15
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Publication No.: US20160108738A1Publication Date: 2016-04-21
- Inventor: Matthew A. Devore , Matthew S. Gleiner
- Applicant: United Technologies Corporation
- Main IPC: F01D5/18
- IPC: F01D5/18 ; 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
- US10465523B2 Gas turbine component with platform cooling Public/Granted day:2019-11-05
Information query
