发明名称 |
Combustor liner support and seal assembly |
摘要 |
The invention is a combination that includes a gas turbine engine extending along an axis. The gas turbine engine includes an annular combustor with a combustor liner. The combination of the invention also includes a plurality of projections extending from the combustor liner and spaced from one another circumferentially about the axis. The combination of the invention also includes a free-standing ring disposed about the combustor liner and positioned adjacent to the plurality of projections along the axis. The plurality of projections engage a corresponding circumferentially-facing portion of the free-standing ring and circumferentially support the combustor liner while allowing relative radial displacement between the combustor liner and the free-standing ring. The combination of the invention also includes a rolling assembly operably disposed between the free-standing ring and the plurality of projections to reduce binding during the relative radial displacement.
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申请公布号 |
US7900461(B2) |
申请公布日期 |
2011.03.08 |
申请号 |
US20070755793 |
申请日期 |
2007.05.31 |
申请人 |
ROLLS-ROYCE CORPORATION |
发明人 |
VARNEY BRUCE EDWARD;SMILEY VICKIE RAE;TAYLOR TODD S.;PETTY, SR. JACK DWANE |
分类号 |
F02C7/20 |
主分类号 |
F02C7/20 |
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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