- Patent Title: Gas turbine engine wall assembly with enhanced flow architecture
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Application No.: US15039108Application Date: 2014-12-31
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Publication No.: US10234140B2Publication Date: 2019-03-19
- Inventor: Frank J. Cunha , Stanislav Kostka
- 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: O'Shea Getz P.C.
- International Application: PCT/US2014/072928 WO 20141231
- International Announcement: WO2015/103357 WO 20150709
- Main IPC: F02C7/18
- IPC: F02C7/18 ; F23R3/00 ; F23R3/06 ; F01D5/18 ; F01D25/12
Abstract:
A liner panel is provided for use in a gas turbine engine. The liner panel includes an intermediate rail that extends from a cold side of a liner panel. The liner panel also includes a multiple of heat transfer augmentors, which generally decrease in height with respect to a distance from the intermediate rail.
Public/Granted literature
- US20170159936A1 GAS TURBINE ENGINE WALL ASSEMBLY WITH ENHANCED FLOW ARCHITECTURE Public/Granted day:2017-06-08
Information query
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