发明名称 |
Flap seal for gas turbine engine movable nozzle flap |
摘要 |
A gas turbine engine nozzle (14) includes a flap (18) movable relative to a structure (20). A seal assembly (22) is supported by one of the structure (20) and the flap (18) and includes a seal (26) hinged about an axis. The seal (26) has a sealing profile engaging a seal land of the other of the structure (20) and the flap (18). A biasing member (36) is configured to urge the hinged seal (26) toward the seal land. |
申请公布号 |
EP2562363(A3) |
申请公布日期 |
2016.08.31 |
申请号 |
EP20120180917 |
申请日期 |
2012.08.17 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
MCMAHON, SHAWN M.;SHUTE, KIRK A. |
分类号 |
F01D11/00;F01D25/30;F02K1/12;F02K1/80 |
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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