发明名称 Thrust reverser utilizing integrated structural bypass duct
摘要 A thrust reverser having an engine cowl, a nacelle, a blocker door, a nacelle door and a cascade vane. The engine cowl has a hollow body that shrouds a jet engine and which includes a cowl opening. The nacelle surrounds the engine cowl and includes a nacelle opening that is positioned outwardly of the cowl opening. The blocker door is associated with the engine cowl and movable between a first position, wherein the blocker door closes the cowl opening, and a second position, wherein the blocker door is disposed in the propulsive air flow and substantially clears the cowl opening. The nacelle door is associated with the nacelle and movable between a forward position, which substantially closes the nacelle opening, and a rearward position, which substantially clears the nacelle opening. The cascade vane is disposed between the engine cowl and the nacelle and positioned between the cowl and nacelle openings.
申请公布号 US7124981(B2) 申请公布日期 2006.10.24
申请号 US20030379029 申请日期 2003.03.04
申请人 THE BOEING COMPANY 发明人 PARHAM DEAN
分类号 F02K3/04;F02K1/62;F02K1/70 主分类号 F02K3/04
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