- Patent Title: Spring loaded and sealed ceramic matrix composite combustor liner
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Application No.: US14917736Application Date: 2014-08-14
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Publication No.: US10436446B2Publication Date: 2019-10-08
- Inventor: Bryan Robert Dery
- Applicant: GENERAL ELECTRIC COMPANY
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: General Electric
- Agent Kristi Davidson
- International Application: PCT/US2014/050988 WO 20140814
- International Announcement: WO2015/038274 WO 20150319
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/60

Abstract:
A combustor liner assembly of a gas turbine engine comprises a dome having a central axis aligned with an engine axis, the dome arranged at an inlet end of a combustor, a first spring disposed at a radially outward position of the dome, an outer liner retainer engaging a radially outer cowl and, the outer liner retainer having a sealing surface disposed in a radial plane for receiving an axial force, a ceramic matrix composite outer combustor liner having an outer liner sealing surface which is seated against the outer liner retainer, the first spring forcing the outer liner in an axial direction against the liner outer liner retainer, a ceramic matrix composite inner combustor liner having an inner liner sealing surface and engaging a radially inward surface of the dome, a second spring engaging the radially extending surface of the inner combustor liner, acting in an axial direction.
Public/Granted literature
- US20160215981A1 SPRING LOADED AND SEALED CERAMIC MATRIX COMPOSITE COMBUSTOR LINER Public/Granted day:2016-07-28
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