发明名称 THRUST REVERSER NOZZLE FOR A TURBOFAN GAS TURBINE ENGINE
摘要 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.
申请公布号 CA2660001(C) 申请公布日期 2012.06.12
申请号 CA20072660001 申请日期 2007.08.29
申请人 PRATT & WHITNEY CANADA CORP. 发明人 LAIR, JEAN-PIERRE
分类号 F02K1/56;F02K1/58 主分类号 F02K1/56
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