发明名称 |
Flexible seal system for a gas turbine engine |
摘要 |
<p>A flexible seal system (16) for a gas turbine engine (10) includes an annular mounting bracket (92), an annular support bracket (96), an annular flexible seal (40) and a plurality of mounting spacers (100). The flexible seal (40) extends axially between a first mounting segment (56) and a second mounting segment (58). The first mounting segment (56) is connected axially between the mounting bracket (92) and the support bracket (96), and includes a plurality of mounting apertures (68) that extend axially through the first mounting segment (56). Each of the mounting spacers (100) is arranged within a respective one of the mounting apertures (68), and extends axially between the mounting bracket (92) and the support bracket (96).
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申请公布号 |
EP2594744(A3) |
申请公布日期 |
2014.03.05 |
申请号 |
EP20120184441 |
申请日期 |
2012.09.14 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DAMGAARD, JOCELYN C.;ROBERTS, STEVEN D.;DALE, TIMOTHY |
分类号 |
F01D11/00 |
主分类号 |
F01D11/00 |
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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