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 代理人
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