发明名称 |
THRUST REVERSER NOZZLE FOR A TURBOFAN GAS TURBINE ENGINE |
摘要 |
<p>The thrust reverser comprises a first reverser door (24) and a second reverser door (26) asymmetrically pivotable between a stowed position and a deployed position, one having a pivot axis closer to the central axis (32) than the other.</p> |
申请公布号 |
WO2008034214(A1) |
申请公布日期 |
2008.03.27 |
申请号 |
WO2007CA01531 |
申请日期 |
2007.08.29 |
申请人 |
PRATT & WHITNEY CANADA CORP.;LAIR, JEAN-PIERRE |
发明人 |
LAIR, JEAN-PIERRE |
分类号 |
F02K1/56;F02K1/58 |
主分类号 |
F02K1/56 |
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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