发明名称 |
Thrust reverser nozzle for a turbofan gas turbine engine |
摘要 |
<p>A 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 (40) closer to the central axis (32) than the other (44).</p> |
申请公布号 |
EP1903205(B1) |
申请公布日期 |
2015.10.14 |
申请号 |
EP20070253690 |
申请日期 |
2007.09.18 |
申请人 |
PRATT & WHITNEY CANADA CORP.;THE NORDAM GROUP, INC. |
发明人 |
LAIR, JEAN-PIERRE |
分类号 |
F02K1/60 |
主分类号 |
F02K1/60 |
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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