发明名称 |
Mounting assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor |
摘要 |
A mounting assembly for an aft end of a liner of a gas turbine engine combustor including a support member, wherein a longitudinal centerline axis extends through the gas turbine engine. The mounting assembly includes a pin member extending through each one of a plurality of circumferentially spaced openings in a portion of the support member for the combustor and into a plurality of partial openings formed in the aft end of the liner, with each pin member including a head portion at one end thereof, and a device positioned within each opening in the support member so as to retain the pin members therein. The pin members and the support member are able to slide radially and/or axially with respect to the liner aft end as the support member experiences thermal growth greater than the liner.
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申请公布号 |
US6895761(B2) |
申请公布日期 |
2005.05.24 |
申请号 |
US20020326209 |
申请日期 |
2002.12.20 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
MITCHELL KRISTA ANNE;BULMAN DAVID EDWARD;NOE MARK EUGENE;HANSEL HAROLD RAY;WELLS THOMAS ALLEN;GLYNN CHRISTOPHER CHARLES;BIBLER JOHN DAVID;DARKINS, JR. TOBY GEORGE;CHARNESKI JOSEPH JOHN;BURNS CRAIG PATRICK |
分类号 |
F23R3/00;F23R3/60;(IPC1-7):F02C7/20 |
主分类号 |
F23R3/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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