发明名称 THRUST REVERSER
摘要 The thrust reverser is used with an aircraft gas turbine engine and includes upper and lower doors pivotable between a stowed position and a deployed position. Whe n deployed, the doors redirect a portion of the efflux to generate a nose-down pitching moment on an aircraft to improve handling during thrust reversing on a runwa y.
申请公布号 CA2639079(A1) 申请公布日期 2009.05.16
申请号 CA20082639079 申请日期 2008.08.15
申请人 PRATT & WHITNEY CANADA CORP. 发明人 LAIR, JEAN-PIERRE
分类号 F02K1/56 主分类号 F02K1/56
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