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公开(公告)号：US20130283959A1
公开(公告)日：2013-10-31
申请号：US13879660
申请日：2011-10-14
摘要： A brake handle assembly for an aircraft emergency/parking brake includes a handle movable between a non-actuated position wherein the brake is disengaged and a full actuated position wherein, during movement therebetween, the brake applies a modulated braking force in an emergency brake state. A button actuator is disposed on the handle. Movement of the handle from the intermediate stop position to the full actuated position is obstructed to prevent inadvertent operation of the brake in the parking brake state unless the button actuator is depressed.
摘要翻译： 用于飞机紧急/驻车制动器的制动手柄组件包括可在非致动位置（其中制动器分离）和完全致动位置之间移动的手柄，其中在其间的运动期间，制动器在紧急制动状态下施加调制制动力。 按钮致动器设置在手柄上。 手柄从中间停止位置到完全致动位置的移动被阻碍，以防止制动器在驻车制动状态下的意外操作，除非按钮致动器被按下。
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公开(公告)号：US20120132742A1
公开(公告)日：2012-05-31
申请号：US13384480
申请日：2011-10-14
申请人： Charles T. O'Connell
发明人： Charles T. O'Connell
CPC分类号： B64C25/50 , B64C25/14 , B64C2025/006 , F16C11/02 , F16C11/045 , F16C2326/43 , Y10T403/602
摘要： A torque link member for aircraft landing gear includes a first end for connecting to a lower portion or an upper portion of the aircraft landing gear and a second end for connecting to another torque link member. A locking pin is disposed on one of the upper portion, the lower portion, the first end or the second end. The locking pin is axially movable between an engaged position wherein the pin protrudes for interengagement with a cooperating aperture on the first end, the second end, the upper portion, the lower portion, or the second end of the other torque link member, and a disengaged position. The locking pin is biased toward the engaged position and movable against the biasing to the disengaged position.
摘要翻译： 用于飞行器起落架的扭矩连杆构件包括用于连接到飞行器起落架的下部或上部的第一端和用于连接到另一扭矩连杆构件的第二端。 锁定销设置在上部，下部，第一端或第二端中的一个上。 锁定销可在接合位置之间轴向移动，其中销突出以与另一扭矩连杆构件的第一端，第二端，上部，下部或第二端上的协作孔相互接合，并且 脱离位置 锁定销朝向接合位置偏置，并且能够抵抗偏压移动到脱离位置。
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公开(公告)号：US09120566B2
公开(公告)日：2015-09-01
申请号：US13384480
申请日：2011-10-14
申请人： Charles T. O'Connell
发明人： Charles T. O'Connell
CPC分类号： B64C25/50 , B64C25/14 , B64C2025/006 , F16C11/02 , F16C11/045 , F16C2326/43 , Y10T403/602
摘要： A torque link member for aircraft landing gear includes a first end for connecting to a lower portion or an upper portion of the aircraft landing gear and a second end for connecting to another torque link member. A locking pin is disposed on one of the upper portion, the lower portion, the first end or the second end. The locking pin is axially movable between an engaged position wherein the pin protrudes for interengagement with a cooperating aperture on the first end, the second end, the upper portion, the lower portion, or the second end of the other torque link member, and a disengaged position. The locking pin is biased toward the engaged position and movable against the biasing to the disengaged position.
摘要翻译： 用于飞行器起落架的扭矩连杆构件包括用于连接到飞行器起落架的下部或上部的第一端和用于连接到另一扭矩连杆构件的第二端。 锁定销设置在上部，下部，第一端或第二端中的一个上。 锁定销可在接合位置之间轴向移动，其中销突出以与另一扭矩连杆构件的第一端，第二端，上部，下部或第二端上的协作孔相互接合，并且 脱离位置 锁定销朝向接合位置偏置，并且能够抵抗偏压移动到脱离位置。
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