专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

21. 发明授权

EP3305653B1 AIRFRAME FOR CERTIFIED ULTRALIGHT AND / OR LIGHT AIRCRAFT 有权
公开(公告)号：EP3305653B1
公开(公告)日：2020-04-01
申请号：EP17194817.7
申请日：2017-10-04
申请人： C.A.I. Confident Aircraft Industry S.R.L.
发明人： LICCARDO, Giuseppe , LICCARDO, Domenico , LICCARDO, Rosario
IPC分类号： B64C1/08 , B64C1/26 , B64C13/06 , B64C13/14 , B64D45/00

22. 发明公开

EP2917102A1 MODULAR, ABOVE-THE-FLOOR RUDDER AND BRAKE CONTROL SYSTEM 有权
标题翻译：模块化舵和制动控制系统安装地板
公开(公告)号：EP2917102A1
公开(公告)日：2015-09-16
申请号：EP13799708.6
申请日：2013-11-11
申请人： Mason Electric Co.
发明人： CARNER, Fred , SALAMAT, Bijan
IPC分类号： B64C13/04 , B64C13/06 , B64C13/50
CPC分类号： B64C13/06 , B64C13/04 , B64C13/503
摘要： A modular brake and rudder control system usable in an aircraft. The modular system mounts atop the flight deck floor (16) without penetrating through the floor when the system is operatively connected to the aircraft's fly-by-wire brake and rudder systems. Pedal assemblies (66) extending from the housing (40) are rotatable and longitudinally moveable relative to the housing. A brake control system fully contained in the housing is connected to the pedal assemblies and provides a signal via an electrical connector (28) to the fly-by-wire brake system upon rotation of the pedals. A rudder control system is fully contained in the housing and is operable independent of the brake control system. The rudder control system detects longitudinal motion of the pedal assemblies and provides a signal via an electrical connector (28) to the fly-by-wire rudder system. The housing, the electrical connectors, the pedal assemblies, the brake control system and the rudder control system define a modular component installable and removable from the cockpit as a unit.

23. 发明公开

EP2632794A4 HELICOPTER AMUSEMENT APPARATUS 审中-公开
标题翻译：游戏直升机DEVICE
公开(公告)号：EP2632794A4
公开(公告)日：2014-05-07
申请号：EP11835732
申请日：2011-10-09
申请人： ABA SCIENCE PLAY LTD
发明人： GOLDNER GAL , GEVA IFTAH
IPC分类号： B64C13/06
CPC分类号： A63G1/12 , A63G1/22 , A63G1/30

24. 发明授权

EP2081816B1 CUSTOMIZABLE PEDAL SYSTEM FOR AN AVIATION CONTROL SYSTEM 有权
标题翻译：独立适应踏板系统FOR一种车辆空调的控制系统
公开(公告)号：EP2081816B1
公开(公告)日：2014-03-12
申请号：EP07864364.0
申请日：2007-11-14
申请人： Bell Helicopter Textron Inc.
发明人： SPINA, Pasquale , LINTON, Brad
IPC分类号： B64C13/06
CPC分类号： B64C13/06 , G05G1/40 , G05G1/44 , G05G1/46 , G05G11/00 , Y10T74/2039 , Y10T74/20528
摘要： A pedal system including a support base, a first lever including a root portion and a terminal portion formed such that the terminal portion interfaces with the root portion at a bend in the first lever of a first predetermined angle, the root portion of the first lever being pivotally mounted to the support base such that the first lever is rotatable in a first plane of rotation about an axis of rotation at or near the support base, a second lever including a root portion and a terminal portion formed such that the terminal portion interfaces with the root portion at a bend in the second lever of a second predetermined angle, the root portion of the second lever being pivotally mounted to the support base such that the second lever is rotatable in a second plane of rotation about the axis of rotation.

25. 发明授权

EP2340994B1 Helicopter control stick support assembly 有权转让
标题翻译：对于直升机控制杆紧固装置
公开(公告)号：EP2340994B1
公开(公告)日：2012-02-08
申请号：EP09425543.7
申请日：2009-12-30
申请人： AGUSTAWESTLAND S.p.A.
发明人： Bandera, Gian Luigi c/o AGUSTAWESTLAND S.p.A.
IPC分类号： B64C13/06
CPC分类号： B64C13/06

26. 发明公开

EP2340994A1 Helicopter control stick support assembly 有权转让
标题翻译： BefestigungsvorrichtungfüreinenHubschraubersteuerknüppel
公开(公告)号：EP2340994A1
公开(公告)日：2011-07-06
申请号：EP09425543.7
申请日：2009-12-30
申请人： Agusta S.p.A.
发明人： Bandera, Gian Luigi
IPC分类号： B64C13/06
CPC分类号： B64C13/06
摘要： A support assembly (4) for helicopter control sticks (5) has a supporting structure (6); an instrument panel (20) fixed to the supporting structure (6); and a connecting device (30) for connecting the sticks (5) to the supporting structure (6). The connecting device (30) has a longitudinally elongated arm (31) fitted on one end (33) with the sticks (5); and the arm (31) slides to move the sticks to/from the supporting structure (6), and rotates about a horizontal axis (10) to adjust the height of the sticks (5).
摘要翻译：用于直升机控制棒（5）的支撑组件（4）具有支撑结构（6）; 固定到所述支撑结构（6）上的仪表板（20）; 以及用于将棒（5）连接到支撑结构（6）的连接装置（30）。连接装置（30）具有与杆（5）一体地装配在一端（33）上的纵向细长臂（31）。并且所述臂（31）滑动以使所述棒与所述支撑结构（6）移动，并且围绕水平轴线（10）旋转以调节所述棒（5）的高度。

27. 发明公开

EP0374737A2 Translating center control system 失效
标题翻译： Translator ch。。。。。。。。。。。。。。。。。
公开(公告)号：EP0374737A2
公开(公告)日：1990-06-27
申请号：EP89123154.0
申请日：1989-12-14
申请人： ROCKWELL INTERNATIONAL CORPORATION
发明人： Adams, William J. , DellaRovere, Robert H. , JexCourter, Barbara G.
IPC分类号： B64D11/00 , B62D1/18 , B64C13/06
CPC分类号： B64C13/06 , B64D11/00
摘要： A flight management console (10) for an air vehicle. The console (10) includes an elongated pedestal (24) connected at a first end to a rigid support structure (26) located forward and below the front instrument panel (28) of the vehicle. The elongated pedestal (24) is capable of translating up and aft or down and forward relative to the front instrument panel (28) and is positioned forward of an associated seat (16,18) along a plane which bisects that associated seat (16,18) and is parallel to the pitch plane of the vehicle. Primary flight controls are mounted on a second end of the pedestal (24). The console (10) includes adjustment means (56) for positioning the pedestal (24) at the desired location along the plane which is parallel to the pitch plane. Therefore, the console (10) allows easy ingress, egress and control of the primary flight controls according to the individual crewmember's (14) anthropometry.
摘要翻译：飞机管理控制台（10）。控制台（10）包括在第一端处连接到位于车辆的前仪表板（28）前方和下方的刚性支撑结构（26）的细长基座（24）。细长基座（24）能够相对于前仪表板（28）向上和向下或向下平移并且相对于相关联的座（16,18）向前平移，所述平面将相关联的座（16， 18）并且平行于车辆的俯仰平面。主飞行控制装置安装在基座（24）的第二端上。控制台（10）包括用于将基座（24）沿着平行于俯仰平面的平面定位在所需位置的调节装置（56）。因此，控制台（10）允许根据个人机组人员（14）人体测量法容易地进入，出口和控制主要飞行控制。

28. 发明公开

EP4406832A1 ACTIVE THROTTLE ARRANGEMENT AND CONTROL SYSTEM 审中-公开
公开(公告)号：EP4406832A1
公开(公告)日：2024-07-31
申请号：EP23275015.8
申请日：2023-01-25
申请人： BAE SYSTEMS plc
发明人： The designation of the inventor has not yet been filed
IPC分类号： B64C13/04 , B64C13/12 , B64D43/00 , B64C13/06
CPC分类号： B64C13/04 , B64C13/12 , B64D43/00 , B64C13/06
摘要： Described herein is a method of controlling a multi-quadrant active throttle assembly. The method comprises: receiving force and position data for a plurality of levers in the multi-quadrant active throttle assembly; analysing the force and position data to determine whether a threshold is exceeded; in response to determining that the threshold is not exceeded, operating in a first mode of operation in which the plurality of levers are controlled collectively; and in response to determining that the threshold is exceeded, operating in a different mode of operation in which the plurality of levers are not controlled collectively.

29. 发明公开

EP4361028A1 PEDAL MECHANISM 审中-公开
公开(公告)号：EP4361028A1
公开(公告)日：2024-05-01
申请号：EP22306649.9
申请日：2022-10-31
申请人： Ratier-Figeac SAS
发明人： Picard, Pierre-Alex , Soulié, Arnaud , Mazars, Benoit
IPC分类号： B64C13/04 , B64C13/06
CPC分类号： B64C13/044 , B64C13/06
摘要： A pedal mechanism (100) for an aircraft, the pedal mechanism (100) comprising: a pedal arm (106, 106A) connectable to a pedal (120, 120A) at a pedal connection point (116, 116A), the pedal arm (106, 106A) rotatable about a pedal arm rotation point (108, 108A) on translation of the pedal (119); and a stature adjustment mechanism, the stature adjustment mechanism actuatable, during a stature adjustment process, to move the pedal arm rotation point (108, 108A).

30. 发明公开

EP4242102A1 PALONNIER D AÉRONEF AVEC CHAÎNE CINÉMATIQUE MÉCANIQUE DE TRANSMISSION 审中-实审
公开(公告)号：EP4242102A1
公开(公告)日：2023-09-13
申请号：EP23160471.1
申请日：2023-03-07
申请人： Dassault Aviation
发明人： PISTIAUX, Laurent , MATEUS, Vincent
IPC分类号： B64C13/04 , B64C13/12 , B64C13/06
摘要： L'invention concerne un palonnier (22) d'aéronef comprenant un bâti (28), une paire de pédales (32), un arbre de sortie (36) et une chaîne cinématique mécanique (38) de transmission à l'arbre de sortie (36) d'un déplacement d'au moins une des pédales (32) par rapport au bâti (28).
La chaîne cinématique mécanique (38) comprend une pièce centrale de transmission (62), la pièce centrale de transmission (62) étant propre à être mise en rotation par rapport au bâti (28) par un déplacement d'une des pédales (32) par rapport au bâti (28), la chaîne cinématique mécanique (38) comprenant aussi un mécanisme de transmission (66) joignant la pièce centrale de transmission (62) à l'arbre de sortie (36), le mécanisme de transmission (66) comprenant une association homocinétique de deux joints de cardan (74) entre ladite pièce centrale de transmission (62) et l'arbre de sortie (36).

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式