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    • 3. 发明授权
    • Aircrew restraint system
    • 机组约束系统
    • US07275710B2
    • 2007-10-02
    • US11154100
    • 2005-06-15
    • Charles E. VanDruffEric KawabataChristopher C. Culbertson
    • Charles E. VanDruffEric KawabataChristopher C. Culbertson
    • B64C1/00
    • B64D25/06
    • A mobile aircrew restraint system includes a track system and a trolley which runs along the track and carries a retractor which releases a webbing strap attached to a harness. The track is preferably an extruded or sectioned track which follows contours of an aircraft interior and may be removable and/or retractable to allow additional room for oversize cargo. The trolley includes an interlock pin which cooperates with interlock holes spaced one to two feet apart along the track, and includes a release handle for disengaging the interlocking pin. The strap retractor is attached to the trolley and is controllable to limit the payout of the webbing strap. The harness is worn by an aircrew member and is attached to the webbing strap by releasable buckles.
    • 移动机组约束系统包括轨道系统和手推车,该轨道系统和手推车沿着轨道运行并且携带卷扬器,其释放附接到线束的带状带。 轨道优选地是沿着飞行器内部的轮廓的挤压或分段的轨道,并且可以是可移动的和/或可缩回的,以允许用于超大货物的附加空间。 手推车包括互锁销,其与沿着轨道间隔开一至两英尺的互锁孔配合,并且包括用于分离联锁销的释放手柄。 带卷收器连接到手推车上,并且可控制以限制带状带的支付。 线束由空勤人员佩戴,并通过可释放的扣环连接到带子带上。
    • 6. 发明授权
    • Supersonic engine, multi-port thrust reversing system
    • 超音速发动机,多端口推力反向系统
    • US5987880A
    • 1999-11-23
    • US889403
    • 1997-07-08
    • Christopher C. Culbertson
    • Christopher C. Culbertson
    • F02K1/70F02K3/02
    • F02K1/70Y02T50/671
    • A thrust reverser system for a gas turbine engine 10 of the type which includes an outer nacelle 16 spaced apart from a core engine to define an annular bypass duct 32 therebetween and having a fan 22 disposed in an inlet for providing forced air to the bypass duct 32 and core engine. The thrust reverser system includes at least one passageway 40 through the nacelle 16 having a plurality of vanes 42 disposed therein. An internal reverser door 44 is disposed to be movable between a closed position wherein the internal reverser door 44 generally covers the at least one passageway 40 and an open position so as to allow at least a portion of air flow in the bypass duct 32 to pass through the at least one passageway 40. At least one mixer lobe 54 is disposed upstream of the at least one passageway 40. The at least one mixer lobe 54 is rotatable from a first position for mixing air from the bypass duct 32 into a core stream airflow and a second position corresponding with the open position of the internal reverser door 44 for directing air from the bypass duct 32 through the at least one passageway 40 for generating a reverser thrust.
    • 一种用于燃气涡轮发动机10的推力反向器系统,其包括与核心发动机间隔开的外部机舱16,以在其间限定环形旁通管道32,并且具有设置在入口中的风扇22,以将强制空气提供到旁路管道 32和核心引擎。 推力反向器系统包括通过机舱16的至少一个通道40,其具有设置在其中的多个叶片42。 内部反向门44设置成可在关闭位置之间移动,其中内部反向门44通常覆盖至少一个通道40和打开位置,以允许旁路管道32中的至少一部分空气流通过 通过至少一个通道40.至少一个混合器凸角54设置在至少一个通道40的上游。至少一个混合器凸角54可从第一位置旋转,用于将来自旁路管道32的空气混合成芯流 气流和与内部反向门44的打开位置相对应的第二位置,用于引导来自旁路管道32的空气通过至少一个通道40,以产生反向推力。