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公开(公告)号：US06250589B1
公开(公告)日：2001-06-26
申请号：US09501779
申请日：2000-02-10
IPC分类号： B64C1314
CPC分类号： G05G5/28 , B64C13/14 , Y10T70/5717 , Y10T70/5739
摘要： An apparatus for rigidly interlocking a control stick and the rudder pedals of an aircraft is provided for protecting the control surfaces of the aircraft operated by the control stick and the rudder pedals against wind loads. The apparatus comprises a control stick clamp assembly rigidly connected to one end of a first lever arm and a rudder pedal retaining assembly rigidly connected to another end of the first lever arm. A second lever arm has one end connected to the rudder pedal retaining assembly. The second lever arm is moveable between a collapsed position and an extended position wherein the distal end of the second lever arm is engageable with a support surface such that the second lever arm is able to support the rudder pedal retaining assembly in engagement with each of the rudder pedals and thereby cause, upon the control stick clamp assembly being secured to the control stick, the first lever arm to support the control stick in a selected position.
摘要翻译： 提供一种用于将控制杆和飞行器的方向舵踏板刚性联锁的装置，用于保护由控制杆操纵的飞机的控制表面和方向舵踏板抵抗风力负载。 该装置包括刚性地连接到第一杠杆臂的一端的控制杆夹具组件和刚性连接到第一杠杆臂的另一端的方向舵踏板保持组件。 第二杠杆臂的一端连接到方向舵踏板保持组件。 第二杠杆臂可在折叠位置和延伸位置之间移动，其中第二杠杆臂的远端可与支撑表面接合，使得第二杠杆臂能够支撑方向舵踏板保持组件与每个 由此，在控制棒夹具组件固定到控制杆上时，第一杠杆臂将控制杆支撑在选定位置。
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公开(公告)号：US5911391A
公开(公告)日：1999-06-15
申请号：US878382
申请日：1997-06-18
CPC分类号： B64C13/14 , B60R25/0221 , Y10T70/5717 , Y10T70/5726 , Y10T70/5739 , Y10T70/5889
摘要： A locking apparatus in combination with a locking pin and method for rigidly interlocking a control wheel and the rudder pedals of an aircraft is provided for securing the control surfaces of the aircraft operated by the control wheel and the rudder pedals in a stable position. The locking pin is adapted to be disposed through aligned locking pin receiving holes of the control column and the control panel collar and has a recess formed therein for lockingly receiving a portion of the control column. The locking apparatus includes a pair of control wheel retaining members rigidly connected to one end of a rod member for retainingly engaging the control wheel and a rudder pedal engaging bar rigidly connected to one end of another rod member. The rudder pedal engaging bar is positionable in a V-shaped notch of each of the rudder pedals so as to engage each of the rudder pedals and so as to secure the rudder pedal engaging bar on the rudder pedals. The rod members are disposed in a telescoping relationship with respect to one another and are adjustably securable whereby the control wheel retaining members are rigidly locked in a selected position relative to the rudder pedal retaining bar wherein the control wheel retaining members cooperate with the rudder pedal retaining bar to support the control column in a pin locking position wherein the control column is lockingly disposed in the recess of the locking pin.
摘要翻译： 与锁定销结合的锁定装置和用于将控制轮和飞行器的舵踏板刚性联锁的方法被提供用于将由控制轮和舵踏板操纵的飞行器的控制表面固定在稳定的位置。 锁定销适于通过控制柱和控制面板轴环的对准的锁定销接收孔设置，并且具有形成在其中的凹部，用于锁定地接收控制柱的一部分。 锁定装置包括一对控制轮保持构件，其刚性地连接到杆构件的一端，用于保持接合控制轮和刚性地连接到另一杆构件的一端的舵踏板接合杆。 方向舵踏板接合杆可定位在每个舵踏板的V形槽口中，以便与每个方向舵踏板接合，以便将方向舵踏板接合杆固定在方向舵踏板上。 杆构件相对于彼此以伸缩关系设置并且可调节地固定，由此控制轮保持构件相对于舵踏板保持杆刚性地锁定在选定位置，其中控制轮保持构件与方向舵踏板保持配合 以将控制柱支撑在销锁定位置，其中控制柱被锁定地设置在锁定销的凹部中。
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公开(公告)号：US5713539A
公开(公告)日：1998-02-03
申请号：US653894
申请日：1996-05-28
CPC分类号： B60R25/0221 , B64C13/14 , Y10T70/5726 , Y10T70/5894
摘要： An apparatus and method for rigidly interlocking a control wheel and the rudder pedals of an aircraft is provided for securing the control surfaces of the aircraft operated by the control wheel and the rudder pedals in a stable position. The apparatus comprises a pair of control wheel retaining members rigidly connected to one end of a rod member in a spaced apart, parallel relationship with one another for retainingly engaging opposing radially extending portions of the control wheel and a pair of rudder pedal retaining members rigidly connected to one end of another rod member in a spaced apart, parallel relationship with one another for retainingly engaging a lever of each of the rudder pedals. The rod members are disposed in a telescoping relationship with respect to one another and are adjustably securable whereby the control wheel retaining members are rigidly locked in a selected position relative to the rudder pedal retaining members wherein the control wheel retaining members cooperate with the rudder pedal retaining members to secure the control wheel in a level position, the control column in an inward position, and the rudder pedals in a neutral or centered position.
摘要翻译： 提供一种用于将控制轮和飞行器的方向舵踏板刚性联锁的装置和方法，用于将由控制轮和方向舵踏板操纵的飞行器的控制表面固定在稳定的位置。 该装置包括一对控制轮保持构件，其以彼此间隔开的平行关系刚性地连接到杆构件的一端，用于保持接合控制轮的相对的径向延伸部分和一对舵踏板保持构件刚性连接 以彼此间隔开的平行关系将另一个杆构件的一端固定地接合每个方向舵踏板的杠杆。 杆构件相对于彼此以伸缩关系设置并且可调节地固定，由此控制轮保持构件相对于舵踏板保持构件刚性地锁定在选定位置，其中控制轮保持构件与方向舵踏板保持 将控制轮固定在水平位置，控制柱处于向内位置，方向舵踏板处于中立或中立位置。
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