Invention Grant
- Patent Title: Gas turbine engine wall assembly with circumferential rail stud architecture
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Application No.: US15038906Application Date: 2014-08-29
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Publication No.: US10088161B2Publication Date: 2018-10-02
- Inventor: Christopher Drake , Stanislav Kostka, Jr. , Frank J. Cunha
- 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/US2014/053502 WO 20140829
- International Announcement: WO2015/094430 WO 20150625
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F02C7/18
Abstract:
A liner panel for use in a gas turbine engine. The liner panel has a hot side and a cold side. The liner panel includes a rail extending from the cold side and a multiple of studs extending from the cold side. At least one of the multiple of studs extends from, in part, the rail.
Public/Granted literature
- US20170159935A1 GAS TURBINE ENGINE WALL ASSEMBLY WITH CIRCUMFERENTIAL RAIL STUD ARCHITECTURE Public/Granted day:2017-06-08
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