公开(公告)号：US09663220B2

公开(公告)日：2017-05-30

申请号：US14193330

申请日：2014-02-28

申请人： The Boeing Company

发明人： Giumaa Milad ,  Edward M. Hojnacki ,  William Otto Zschoche

IPC分类号： B64C13/14 ,  B60R25/06

CPC分类号： B64C13/14 ,  Y10T70/40

摘要： Systems and methods for locking a control lever are provided. One system includes a locking device having a body configured to couple to a control lever within an aircraft to prevent the control lever from moving. The locking device also includes at least one hole defined through the body. The one hole is configured to receive one of a lock or a tag therein.

公开(公告)号：US5908178A

公开(公告)日：1999-06-01

申请号：US975849

申请日：1997-11-20

申请人： Robert A. Sandhagen

发明人： Robert A. Sandhagen

IPC分类号： B64C13/14 ,  B64D45/00 ,  B64F1/00 ,  E05B65/00

CPC分类号： B64D45/0015 ,  B64C13/14 ,  B64F1/005 ,  Y10T70/50 ,  Y10T70/5009

摘要： Security apparatus and a method for preventing theft or unauthorized removal of instruments from the cockpit instrument panel of an aircraft and for preventing theft or unauthorized use of the aircraft. The apparatus includes a rigid plate substantially covering the instrument panel and two rigid arms pivotally secured to the plate inwardly of the columns respectively and laterally pivotable rearwardly away from and forwardly toward the plate. Each of the arms include an end portion for restrainably engaging the aircraft flight control yokes against rotation when the arms are pivoted to extend rearwardly away from the plate while the columns are fully rearwardly extended and the yokes are fully rotated to one side. A locking device is engageable with the end portions of the arms for locking the arms rearwardly extended and for cooperating with the yokes to prevent forward displacement of the columns while securing the plate against the instrument panel.

摘要翻译： 用于防止从飞机的驾驶舱仪表板窃取或未经授权的将仪器拆卸并防止飞行器被盗或未经许可使用的安全装置和方法。 该装置包括基本上覆盖仪表板的刚性板和两个刚性臂，它们分别可枢转地固定在板的内侧，并且侧向可枢转地向后远离板向后移动。 每个臂包括端部，用于在臂被完全向后延伸并且轭完全旋转到一侧时当臂枢转以向后延伸离开板时可限制地接合飞行器飞行控制轭而不是旋转。 锁定装置可与臂的端部接合，用于将臂向后延伸并与轭架配合，以防止支柱向前移位，同时将板固定在仪表板上。

公开(公告)号：US4228974A

公开(公告)日：1980-10-21

申请号：US012463

申请日：1979-02-15

申请人： August B. Yates

发明人： August B. Yates

IPC分类号： B64C13/14 ,  B64D47/00

CPC分类号： B64C13/14 ,  B64D47/00 ,  Y10T70/5009 ,  Y10T70/558 ,  Y10T70/5982

摘要： A device for locking the ailerons and elevators of an aircraft controlled by a wheel-operated longitudinally shiftable and rotatable control column, and, at the same time preventing theft of the navigational instruments and radio equipment mounted on the instrument panel in the cockpit of the plane. The protective device takes the form of a cover plate mounted immediately adjacent the instrument panel by means of upper and lower clamping blocks secured about the control column in such a manner as to prevent unauthorized movements of the column and access to the instruments on the panel. The blocks have complementary semi-cylindrical grooves which clamp about the control column, and one block is fixed to the cover plate while the other has sliding, tongue and groove engagement to couple with said one block and clamp the control column against movement. The pair of blocks are held in clamped arrangement by a padlock whose shackle passes through aligned apertures in the blocks.

摘要翻译： 一种用于锁定由轮式纵向可移动和可旋转控制柱控制的飞行器的副翼和电梯的装置，并且同时防止安装在飞机驾驶舱中的仪表板上的导航仪器和无线电设备的被盗 。 保护装置采用紧邻仪表板的盖板的形式，借助于以控制柱固定的上部和下部夹紧块，以防止柱的未经许可的移动和对面板上的仪器的访问。 这些块具有互补的半圆柱形槽，其围绕控制柱夹紧，并且一个块固定到盖板，而另一个具有滑动，榫舌和槽接合以与所述一个块联接并夹紧控制柱以防止运动。 一对块通过挂锁夹紧安置，挂钩穿过块中对齐的孔。

公开(公告)号：US3898823A

公开(公告)日：1975-08-12

申请号：US38190573

申请日：1973-07-23

申请人： LUDEMAN RUSSELL S

发明人： LUDEMAN RUSSELL S

IPC分类号： B64C13/14

CPC分类号： B64C13/14 ,  Y10T70/5726 ,  Y10T70/5765 ,  Y10T70/5894

摘要： A device for resiliently locking the controls of an aircraft having a pedal-controlled rudder and elevators and ailerons controlled by a wheel-operated, longitudinally shiftable and rotatable control column, and, at the same time, locking the main landing gear parking brake, if so desired. In the form shown, the device comprises a tube containing a series of suitable alternating spacer spring seats and interchangeable coil springs and having an adjustable member at one end formed with opposing slots to receive the edges of adjacent rudder pedals and an adjustable slotted element at the other end for receiving the wheel, the wheel receiving member having a rod and spacer extending therefrom into the tube, allowing limited movement thereof in either direction through the tube against the force of the springs. The wheel element and, if desired, the pedal member, are formed to receive a pin or a padlock for either temporarily holding or locking the same in place.

摘要翻译： 一种用于弹性地锁定具有踏板控制的方向舵的飞机的控制装置，以及由轮式操作的纵向可移动和可旋转的控制柱控制的电梯和副翼，并且同时锁定主起落架驻车制动器，如果 所以希望。 在所示的形式中，该装置包括管，该管包含一系列合适的交替的间隔弹簧座和可互换的螺旋弹簧，并且在一端具有可调节构件，该可调构件形成有相对的狭槽，以容纳相邻的方向舵踏板的边缘，以及可调节的开槽元件 用于接收车轮的另一端，车轮接收构件具有杆和从其延伸到管中的间隔件，允许其克服弹簧的力在任一方向上受到限制的运动。 轮子元件，如果需要的话，踏板部件被形成为接收销或挂锁，用于将其暂时保持或锁定在适当位置。

公开(公告)号：US3169731A

公开(公告)日：1965-02-16

申请号：US26580363

申请日：1963-03-18

申请人： PHILLIPS PAUL B ,  WILSON BYRON R

发明人： PHILLIPS PAUL B ,  WILSON BYRON R

IPC分类号： B64C13/14

CPC分类号： B64C13/14 ,  Y10T74/20189

公开(公告)号：US2584038A

公开(公告)日：1952-01-29

申请号：US1387948

申请日：1948-03-09

申请人： BOEING CO

发明人： MORRISON JOHN A

IPC分类号： B64C13/14

CPC分类号： B64C13/14 ,  Y10T74/20238

公开(公告)号：US20180148167A1

公开(公告)日：2018-05-31

申请号：US15826851

申请日：2017-11-30

申请人： AIRBUS HELICOPTERS

发明人： Jean-Romain BIHEL ,  Zouhair SASSI

IPC分类号： B64C27/56 ,  B64C13/14 ,  B64C27/82

CPC分类号： B64C27/56 ,  B64C11/30 ,  B64C13/0421 ,  B64C13/044 ,  B64C13/14 ,  B64C27/82 ,  B64C2027/8227 ,  B64D31/04

摘要： A control member that is operable by a pilot to vary thrust from a thrust system of an aircraft. The control member comprises a stick and a movable assembly including a grip. The grip is linked to the stick via a helical link, rotation of the grip about the stick giving rise to movement in translation of the grip together with the movable assembly along the stick, the grip being movable in translation in both a first direction in translation and in a second direction in translation that is opposite to the first direction in translation.

公开(公告)号：US6116065A

公开(公告)日：2000-09-12

申请号：US133695

申请日：1998-08-13

申请人： Charles Richard Hale

发明人： Charles Richard Hale

IPC分类号： B64C13/14 ,  B64D45/00 ,  F16H57/00

CPC分类号： B64C13/14 ,  B64D45/0015 ,  Y10T70/40 ,  Y10T70/5726 ,  Y10T70/5765

摘要： An anti-theft device for precluding the flying of an airplane comprises a pair of arm members telescopically interengaged and having axially outwardly open U-shaped hooks for engaging with two flight control components in the cockpit of an airplane to preclude the displacement of the elevators, ailerons or rudder necessary to fly the airplane. The anti-theft device is releasably locked between the flight control components.

摘要翻译： 用于防止飞机飞行的防盗装置包括一对可伸缩地相互接合并具有轴向向外开口的U形钩的臂构件，用于与飞机的驾驶舱中的两个飞行控制部件接合以排除电梯的移位， 飞机所需的副翼或方向舵。 防盗装置可释放地锁定在飞行控制部件之间。

公开(公告)号：US5713539A

公开(公告)日：1998-02-03

申请号：US653894

申请日：1996-05-28

申请人： Richard T. Russ ,  Thomas C. Williams

发明人： Richard T. Russ ,  Thomas C. Williams

IPC分类号： B60R25/02 ,  B64C13/14

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。

公开(公告)号：US5129603A

公开(公告)日：1992-07-14

申请号：US683737

申请日：1991-04-11

申请人： Lawrence J. Wippler

发明人： Lawrence J. Wippler

IPC分类号： B64C13/14

CPC分类号： B64C13/14 ,  Y10T70/5735 ,  Y10T70/5757 ,  Y10T70/5774 ,  Y10T70/5841 ,  Y10T70/5894

摘要： An aircraft control locking apparatus for a control yoke on a control shaft extending from an instrument panel in an aircraft is provided. The aircraft control locking apparatus utilizing a pair of elastic shock cords, a first mechanism for connecting an upper end of each of the elastic shock cords in a spaced apart relationship to the control yoke and a second mechanism for connecting a lower end of each of the elastic shock cords in a spaced apart relationship to a fixed point on the instrument panel below the control shaft. The control lock retains the control yoke in a neutral position, keeping the control surfaces of the aircraft from moving freely, thereby preventing damage to the aircraft stored outdoors during periods of strong gusty winds in severe weather.

摘要翻译： 提供了一种用于在飞机上从仪表板延伸的控制轴上的控制轭的飞行器控制锁定装置。 利用一对弹性冲击帘线的飞行器控制锁定装置，用于将每个弹性冲击帘线的上端以与控制轭相隔开的关系连接的第一机构，以及用于连接每个弹性冲击绳的下端的第二机构 与控制轴下方的仪表板上的固定点间隔开的弹性冲击绳。 控制锁将控制叉保持在中立位置，保持飞行器的控制面免于自由移动，从而防止在恶劣天气下的强阵风期间对存储在户外的飞机造成损坏。