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1. 发明授权

US09663220B2 Systems and methods for locking a control lever 有权
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.

2. 发明授权

US5908178A Aircraft security apparatus and method 失效
标题翻译：飞机安全装置及方法
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。

3. 发明授权

US4228974A Protective device for instruments and locking of aircraft controls 失效
标题翻译：用于仪器的保护装置和飞机控制器的锁定
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。

4. 发明授权

US3898823A Device for resiliently locking aircraft controls 失效
标题翻译：弹性锁定飞机控制装置
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。

5. 发明授权

US3169731A Aircraft control locking device 失效
标题翻译：飞机控制锁定装置
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

6. 发明授权

US2584038A Aircraft control lock 失效
标题翻译：飞机控制锁
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

7. 发明授权

US12006023B2 Aircraft inceptor apparatus and aircraft flight control system 有权
公开(公告)号：US12006023B2
公开(公告)日：2024-06-11
申请号：US17673961
申请日：2022-02-17
申请人： Lilium eAircraft GmbH
发明人： Rodrigo Rizzi Starr , Robert Austen Fox , Markus Scherdel , Alex Duarte Gomes , Vincente Martínez Martínez , Fabio Wilson Rodrigues , Rogério De Cerqueira Lario
IPC分类号： B64C13/04 , B64C13/10 , B64C13/12 , B64C13/14 , B64C13/50 , G05D1/00
CPC分类号： B64C13/0421 , B64C13/10 , B64C13/12 , B64C13/14 , B64C13/503 , G05D1/0077
摘要： An inceptor apparatus for an aircraft having a primary inceptor member provided in the form of a stick member having a grip portion, at which the stick member can be gripped by a pilot's hand, and a secondary inceptor member provided at an upper portion of the primary inceptor member and having an actuating portion, at which the secondary inceptor member can be manually actuated by a pilot's thumb. Both inceptor members have associated a respective sensor assembly which is provided to generate electronic flight control signals or commands in response to at least one of i) pivoting movements of the respective inceptor member around each of two independent maneuvering axes associated to the inceptor member, ii) forces acting on or via the respective inceptor member in pivoting directions with respect to each of the maneuvering axes, and iii) lateral flexing or bending of the respective inceptor member.

8. 发明公开

US20240140592A1 FOLDING CONTROL STICK AND LOCKING MECHANISM 审中-公开
公开(公告)号：US20240140592A1
公开(公告)日：2024-05-02
申请号：US17974824
申请日：2022-10-27
申请人： Lockheed Martin Corporation
发明人： John Stephen Yerant , Timothy Heising Bean , Stephen V. Poulin
IPC分类号： B64C13/14 , B64C13/04
CPC分类号： B64C13/14 , B64C13/0421
摘要： A control input operable by a user for controlling movement of an aircraft includes a base portion configured for coupling to a support surface, the base portion biased towards a neutral position defined along a central axis and pivotable to a plurality of angular positions relative to the central axis. The control input also includes a grip portion having inputs for controlling movement of the aircraft and pivotally coupled to the base portion, the grip portion pivotable between a first position in which the grip portion extends from the base portion and a second position in which the grip portion is pivoted relative to the base portion. Further, the control input includes a lock mechanism for locking the grip portion in the first position wherein releasing the lock mechanism allows the grip portion to move to the second position.

9. 发明授权

US10870482B2 Aircraft control selector levers 有权
公开(公告)号：US10870482B2
公开(公告)日：2020-12-22
申请号：US15952778
申请日：2018-04-13
申请人： Hamilton Sundstrand Corporation
发明人： Samuel Neff , Christopher Dias , Andrew Hanley
IPC分类号： B64C13/14 , B64C13/04
CPC分类号： B64C13/14 , B64C13/042
摘要： Selector lever systems of aircraft are provided. The selector lever systems include a selector lever configured to control operation of one or more aircraft control surfaces, the selector lever having a handle configured to enable manual operation of the selector lever, a touch sensor arranged on the handle, and a controller arranged in communication with the touch sensor, the controller configured to at least one of generate a notification when a signal is received from the touch sensor and unlock the selector lever from a locked state.

10. 发明申请

US20180148167A1 CONTROL MEMBER, A ROTARY WING AIRCRAFT, AND A METHOD 审中-公开
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.

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