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1. 发明公开

US20230278697A1 AIRCRAFT RUDDER PEDAL FRAME 审中-公开
公开(公告)号：US20230278697A1
公开(公告)日：2023-09-07
申请号：US18118125
申请日：2023-03-06
申请人： DASSAULT AVIATION
发明人： Eric GRANIER , Vincent MATEUS
IPC分类号： B64C13/04 , B64C13/50 , B64C13/12 , B64C13/06
CPC分类号： B64C13/044 , B64C13/06 , B64C13/12 , B64C13/50
摘要： An aircraft rudder pedal frame includes a base, a support framework and connection interfaces. Each connection interface is able to connect another part of the rudder pedal to the frame. The support framework connects each connection interface to the base. The support framework includes framework elements arranged in a lattice, at least one of the framework elements extending from each connection interface.

2. 发明申请

US20220185455A1 Device for piloting an aircraft and associated method 有权
公开(公告)号：US20220185455A1
公开(公告)日：2022-06-16
申请号：US17550006
申请日：2021-12-14
申请人： DASSAULT AVIATION
发明人： Fabien COCKENPOT , François PINEAU , Jérôme LE BORLOCH
IPC分类号： B64C13/04 , B64C13/12 , B64C13/06
摘要： A piloting device for piloting an aircraft comprises a first and a second control stick mounted movable on a support. The device comprises a priority selection module configured to switch the first and second control sticks between a piloting configuration and a non-piloting configuration. The device further comprises a detection system for detecting the positions of the first and second control sticks; a first and second actuation system configured to generate respective first and second forces on the respective first and second control stick; and a control module configured to control the actuation system of the control stick which is in a non-piloting configuration such that the positions of the control sticks are identical.

3. 发明授权

US11167838B2 Rudder control unit having a single-piece main module mobile on a curved support frame 有权
公开(公告)号：US11167838B2
公开(公告)日：2021-11-09
申请号：US16417744
申请日：2019-05-21
申请人： Airbus Operations (S.A.S.)
发明人： Bernard Guering , Laurent Saint-Marc
IPC分类号： B64C13/04 , B64C9/02 , B64C13/06 , B64C13/12
摘要： A rudder control unit includes a single-piece main module mobile on a curved support frame. The rudder control unit includes a curved support and guide frame to be mounted in a floor of the aircraft, and a unique main module including the pedals and a set of functionalities, the main module configured such that it is movable and positioned on the support and guide frame using a movement unit, thus making it possible to obtain an extremely simplified architecture with a reduced number of pieces.

4. 发明授权

US10011347B2 Irreversible roller clutch for preventing back drive 有权
公开(公告)号：US10011347B2
公开(公告)日：2018-07-03
申请号：US15194437
申请日：2016-06-27
申请人： The Boeing Company
发明人： David J. Zimmer , Yevgeniy M. Gisin
IPC分类号： B64C13/06 , G05G5/04 , G05G1/40
CPC分类号： B64C13/044 , B64C13/06 , G05G1/40
摘要： Systems and methods are provided for an irreversible clutch to prevent back-drive. The irreversible clutch may transfer torque and/or rotation received at a first end to a second end, but may not transfer torque and/or rotation received at the second end to the first end. The irreversible clutch may prevent unintended adjustment of one or more rudder pedals and/or a rudder pedal assembly.

5. 发明授权

US09856015B2 Rudder bar for an aircraft 有权
公开(公告)号：US09856015B2
公开(公告)日：2018-01-02
申请号：US14961349
申请日：2015-12-07
申请人： Airbus Operations (SAS)
发明人： Laurent Saint-Marc , Christophe Mialhe , Patrick Lieven , Romain Delahaye , Marc Audibert , Nicolas Chatrenet
IPC分类号： B64C19/02 , B64C13/04 , B64C13/06 , G05G1/30
CPC分类号： B64C13/04 , B64C13/06 , G05G1/30
摘要： A rudder bar for an aircraft comprising a floor, a steering connecting rod and a braking connecting rod. The rudder bar comprises a base fixed above the floor, a pedal arm mounted rotatably on the base about a first axis of rotation and having a lower end and an upper end, a pedal mounted rotatably on the lower end about a second axis of rotation, a first transmission assembly configured to transmit a movement to the steering connecting rod when the pedal arm pivots about the first axis of rotation, and a second transmission assembly configured to transmit a movement to the braking connecting rod when the pedal pivots about the second axis of rotation.

6. 发明授权

US09545995B1 Control normalization for unmanned autonomous systems 有权
标题翻译：控制无人自主系统的归一化
公开(公告)号：US09545995B1
公开(公告)日：2017-01-17
申请号：US14798715
申请日：2015-07-14
申请人： QUALCOMM Incorporated
发明人： Kiet Tuan Chau , Michael-David Nakayoshi Canoy , Michael Orlando DeVico , Stephen Alton Sprigg
IPC分类号： B64C13/06 , B64C39/02 , G05D1/00 , G05D1/10 , G05B13/04
CPC分类号： B64C13/06 , B64C39/024 , B64C2201/141 , B64C2201/146 , G05B13/04 , G05D1/0022
摘要： Methods, systems, and process-readable media include an autonomous vehicle override control system that receives override commands from a pilot qualified on a first type of unmanned autonomous vehicle (UAV) and translates the inputs into suitable commands transmitted to a target UAV of a second UAV type. A pilot's certification for a first UAV type may be determined from the pilot's login credentials. The system may obtain a first control model for the first UAV type and a second control model for the target UAV. Pilot input commands processed through the first control model may be used to calculate movements of a virtual UAV of the type. The system may estimate physical movement of the target UAV similar to the first physical movement, and generate an override command for the target UAV using the second control model and the second physical movement. Control models may accommodate current conditions and pilot experience.
摘要翻译：方法，系统和过程可读介质包括自动车辆覆盖控制系统，其从在第一类型的无人自主车辆（UAV）上限定的飞行器接收超控命令，并且将输入转换为传输到第二类型的目标UAV的合适命令无人机类型。飞行员的第一个UAV类型的认证可以从飞行员的登录凭据确定。该系统可以获得用于第一UAV类型的第一控制模型和用于目标UAV的第二控制模型。可以使用通过第一控制模型处理的导频输入命令来计算该类型的虚拟UAV的移动。系统可以估计目标UAV的物理运动，类似于第一物理运动，并且使用第二控制模型和第二物理运动生成针对目标UAV的覆盖命令。控制模型可以适应当前条件和飞行员体验。

7. 发明申请

US20160362175A1 CONFIGURABLE CONTROL PANEL FOR AN AIRCRAFT COCKPIT AND METHOD OF CONFIGURATION FOR SUCH A PANEL 审中-公开
标题翻译：用于飞机组合的可配置控制面板及其配置方法
公开(公告)号：US20160362175A1
公开(公告)日：2016-12-15
申请号：US15179580
申请日：2016-06-10
申请人： ZODIAC AERO ELECTRIC
发明人： Romain DE BOSSOREILLE , Michael NAHMIYACE
IPC分类号： B64C13/06 , G06F3/14 , G06F3/041
CPC分类号： B64C13/06 , B64D43/00 , G01C23/00 , G06F3/041 , G06F3/1423
摘要： A configurable control panel for an aircraft cockpit includes a set of universal control modules each comprising at least one screen including at least one manually manipulable control key. Each of the control modules further includes at least one master control module, and at least one universal slave module associated with the master module, and including a screen and at least one control key. The at least one master module is configured to control the screen and the at least one control key of the at least one universal slave module.
摘要翻译：用于飞机驾驶舱的可组态控制面板包括一组通用控制模块，每个通用控制模块包括至少一个包括至少一个可手动操纵的控制键的屏幕。每个控制模块还包括至少一个主控制模块和与主模块相关联的至少一个通用从模块，并且包括屏幕和至少一个控制键。所述至少一个主模块被配置为控制所述屏幕和所述至少一个通用从模块的所述至少一个控制键。

8. 发明授权

US1802117A Adjustable control pedal 失效
标题翻译：可调控制踏板
公开(公告)号：US1802117A
公开(公告)日：1931-04-21
申请号：US22273827
申请日：1927-09-29
申请人： GLENN L MARTIN CO
发明人： LEISY CLIFFORD J
IPC分类号： B64C13/06
CPC分类号： B64C13/06

9. 发明申请

US20190354131A1 VEHICLE INCLUDING CONTROL PEDAL ARRANGEMENT 审中-公开
公开(公告)号：US20190354131A1
公开(公告)日：2019-11-21
申请号：US16469412
申请日：2017-12-12
申请人： AEROMOBIL R&D, S.R.O.
发明人： Doug MACANDREW , Simon ROOMS , Alan ROACH , Slavomir FAZEKAS , Martin GREN
IPC分类号： G05G1/36 , B60F5/02 , B64C3/56 , B64C13/04 , B64C13/06 , B64C13/30
摘要： A control system for use in a vehicle configurable for air use or road use, the vehicle comprising moveable control surfaces for controlling operation of the vehicle in air use, wherein the system comprises: a pedal arrangement of three pedals, comprising a central brake pedal and first and second side pedals, one on either side of the brake pedal, the pedal arrangement having a first configuration for use when the vehicle is configured for road use, and a second configuration for use when the vehicle is configured for air use; wherein in the first configuration, the first (right) side pedal is configured to act as a throttle control; and in the second configuration, the first and second pedals are connected to the moveable control surfaces. A vehicle configurable for air or road use incorporating the control system comprises: a body having road wheels for supporting the body when configured for road use; wings connected to the body and deployable for air use; a tail section at the rear of the body; moveable control surfaces for controlling operation of the vehicle in air use.

10. 发明授权

US10279890B2 Configurable control panel for an aircraft cockpit and method of configuration for such a panel 有权
公开(公告)号：US10279890B2
公开(公告)日：2019-05-07
申请号：US15179580
申请日：2016-06-10
申请人： ZODIAC AERO ELECTRIC
发明人： Romain De Bossoreille , Michael Nahmiyace
IPC分类号： B64C13/06 , B64D43/00 , G01C23/00 , G06F3/041 , G06F3/14
摘要： A configurable control panel for an aircraft cockpit includes a set of universal control modules each comprising at least one screen including at least one manually manipulable control key. Each of the control modules further includes at least one master control module, and at least one universal slave module associated with the master module, and including a screen and at least one control key. The at least one master module is configured to control the screen and the at least one control key of the at least one universal slave module.

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