Invention Grant
- Patent Title: Liner for a combustor of a gas turbine engine with metallic corrugated member
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Application No.: US15221373Application Date: 2016-07-27
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Publication No.: US11619387B2Publication Date: 2023-04-04
- Inventor: Ted Joseph Freeman , Bruce E. Varney , Adam L. Chamberlain
- Applicant: Rolls-Royce Corporation , Rolls-Royce North American Technologies, Inc.
- Applicant Address: US IN Indianapolis; US IN Indianapolis
- Assignee: Rolls-Royce Corporation,Rolls-Royce North American Technologies, Inc.
- Current Assignee: Rolls-Royce Corporation,Rolls-Royce North American Technologies, Inc.
- Current Assignee Address: US IN Indianapolis; US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/06 ; F23R3/10
Abstract:
A liner for a combustor includes a support member, an intermediate member, and a liner member. The intermediate member is positioned intermediate the support member and the liner member and has a plurality of protrusions and a plurality of recesses. The support member is coupled to the intermediate member at a tangent of each protrusion. Additionally, the liner member is comprised of a ceramic matrix composite material. The liner member is coupled to the intermediate member at a tangent of each recess.
Public/Granted literature
- US20170138596A1 LINER FOR A COMBUSTOR OF A GAS TURBINE ENGINE Public/Granted day:2017-05-18
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