- Patent Title: Cooling passages for a gas path component of a gas turbine engine
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Application No.: US14955167Application Date: 2015-12-01
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Publication No.: US10458252B2Publication Date: 2019-10-29
- Inventor: Brandon W. Spangler , Atul Kohli
- 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 ; F01D5/14 ; F01D9/02 ; F01D11/08 ; F01D25/12 ; F02C3/04 ; F01D5/28
Abstract:
A gas path component for a gas turbine engine includes an element configured to be exposed to a gas path. The element includes a plurality of internal cooling passages. At least one of the internal cooling passages includes a cross section having a plurality of asymmetrical filleted corners.
Public/Granted literature
- US20170152751A1 COOLING PASSAGES FOR A GAS PATH COMPONENT OF A GAS TURBINE ENGINE Public/Granted day:2017-06-01
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