发明名称 |
TURBINE ENGINE NOZZLE |
摘要 |
A turbine engine nozzle assembly has an upstream flap and a downstream flap pivotally coupled thereto for relative rotation about a hinge axis. An actuator linkage is coupled to the downstream flap along a forward portion thereof for actuating the upstream flaps and downstream flaps between a number of throat area conditions while permitting mode changes.
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申请公布号 |
US2007039328(A1) |
申请公布日期 |
2007.02.22 |
申请号 |
US20030625997 |
申请日期 |
2003.07.21 |
申请人 |
PETTY DALE W;SIMPSON ALEX J |
发明人 |
PETTY DALE W.;SIMPSON ALEX J. |
分类号 |
B64D33/04;F02K1/06;F02K1/12 |
主分类号 |
B64D33/04 |
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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