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1. 发明公开

EP2178748A2 HOCHAUFTRIEBSSYSTEM FÜR EIN FLUGZEUG 有权
标题翻译： HOCHAUFTRIEBSSYSTEMFÜREIN FLUGZEUG
公开(公告)号：EP2178748A2
公开(公告)日：2010-04-28
申请号：EP08785397.4
申请日：2008-08-06
申请人： Airbus Operations GmbH
发明人： VOSS, Timo , LOERKE, Joachim
IPC分类号： B64C9/16 , B64C9/28
CPC分类号： B64C9/16 , B64C9/02 , B64C9/28
摘要： The invention relates to a high lift system for an aircraft, comprising a main wing (1), a flap (2) disposed on the main wing (1) of the aircraft that can be adjusted between a retracted position and several extended positions relative to the main wing (1) by means of flap actuating means and a drive device, said system further comprising a carrier part (3; 21) disposed on the main wing (1) to which the flap actuating means are coupled and relative to which the flap actuating means for adjusting the flap (2) can be moved, wherein the carrier part (3; 21) is disposed on the main wing by means of a bearing device (10) comprising an adjusting device with which the orientation of the carrier part relative to the orientation of the main wing can be adjusted.
摘要翻译：本发明涉及一种用于飞机的高升力系统，包括主翼（1），设置在飞机的主翼（1）上的翼片（2），其可以在缩回位置和相对于所述主翼（1）借助襟翼致动装置和驱动装置，所述系统还包括设置在所述主翼（1）上的托架部件（3; 21），所述襟翼致动装置联接到所述托架部件上，用于调节襟翼（2）的襟翼致动装置可以移动，其中，通过包括调节装置的支承装置（10）将支架部件（3; 21）布置在主翼上，利用该调节装置，支架部件相对于主翼的方向可以进行调整。

2. 发明公开

EP2964520A1 HIGH LIFT CONTROL METHOD AND SYSTEM FOR AIRCRAFT 有权转让
标题翻译：高升控制系统和程序的飞机
公开(公告)号：EP2964520A1
公开(公告)日：2016-01-13
申请号：EP14712034.9
申请日：2014-02-26
申请人： Bombardier Inc. , Short Brothers Plc
发明人： YOUNG, Robert , GRENIER, Yves , SADEK, Hany
IPC分类号： B64C9/28 , B64C13/04 , B64C13/16
CPC分类号： B64C13/04 , B64C9/28 , B64C13/16 , B64D2045/001
摘要： A high lift control system for an aircraft having at least one high lift surface includes a selector having a predetermined number of discrete positions, at least one of the predetermined positions corresponding to different positions of the at least one high lift surface.

3. 发明授权

EP2178748B1 HOCHAUFTRIEBSSYSTEM FÜR EIN FLUGZEUG 有权
公开(公告)号：EP2178748B1
公开(公告)日：2013-05-08
申请号：EP08785397.4
申请日：2008-08-06
申请人： Airbus Operations GmbH
发明人： VOSS, Timo , LOERKE, Joachim
IPC分类号： B64C9/16 , B64C9/28
CPC分类号： B64C9/16 , B64C9/02 , B64C9/28

4. 发明授权

EP1619119B1 Wing assembly for an ultralight aircraft, and ultralight aircraft provided with such wing assembly 有权转让
标题翻译：对于轻型飞机和超轻型飞机这样的机翼组装机翼组装件
公开(公告)号：EP1619119B1
公开(公告)日：2007-09-05
申请号：EP05106775.9
申请日：2005-07-22
申请人： I.C.P. S.r.l.
发明人： Razzano, Tancredi
IPC分类号： B64C31/028 , B64C9/16 , B64C9/28
CPC分类号： B64C9/28 , B64C31/028

5. 发明公开

EP4039583A1 AN AIRCRAFT WING SECTION ASSEMBLY 审中-实审
公开(公告)号：EP4039583A1
公开(公告)日：2022-08-10
申请号：EP22153145.2
申请日：2022-01-25
申请人： Airbus Operations Limited
发明人： KELLY, Mark Shaun , KELLY, Peter , ALEXANDER, Stuart Strachan
IPC分类号： B64C3/50 , B64C3/56 , B64C9/28
摘要： An aircraft wing section assembly 103 comprises a structural spine 108, a movement mechanism 120 comprising a support rod 121 extending through the structural spine, a first lever 130, for connection to and for moving a first moveable control surface 115, pivotally mounted to the support rod, a second similar lever 192 for connection to and for moving a second moveable control surface 114, and a connection mechanism 191a, 191b for connecting the first and second levers such that pivotal movement of the first lever causes pivotal movement of the second lever, and an actuation mechanism 160 for actuating pivotal movement of the first lever, such that, in use, when the actuation mechanism actuates pivotal movement of the first lever, the second lever also pivotally moves, thus causing movement of both the first and second moveable control surfaces. Also disclosed is an aircraft wing assembly 100, an aircraft 10 and a method of operating an aircraft.

6. 发明授权

EP2692632B1 HIGH-LIFT DEVICE OF FLIGHT VEHICLE 有权
公开(公告)号：EP2692632B1
公开(公告)日：2019-09-04
申请号：EP12764943.2
申请日：2012-03-28
申请人： The Society of Japanese Aerospace Companies , Kawasaki Jukogyo Kabushiki Kaisha
发明人： ISOTANI, Kazuhide , HAYAMA, Kenji
IPC分类号： B64C21/02 , B64C9/16 , B64C9/28 , B64C9/18

7. 发明授权

EP2851292B1 Control interface for leading and trailing edge devices 有权
标题翻译：的入口和出口边缘设备控制接口
公开(公告)号：EP2851292B1
公开(公告)日：2016-11-09
申请号：EP14185978.5
申请日：2014-09-23
申请人： The Boeing Company
发明人： Moser, Matthew A , Finn, Michael R , Thoreen, Adam
IPC分类号： B64C13/04 , B64C13/16 , B64C9/28
CPC分类号： B64C13/16 , B64C9/28 , B64C13/04 , Y02T50/32
摘要： A system (500) for controlling a high-lift device of an aircraft may include an interface (502) for placement in a flight deck of an aircraft. The interface (502) may include an edge control device (504) for controlling a position of the high-lift device. The interface (502) may be operable to select any of a plurality of control device positions (510). Each one of the plurality of control device positions (510) may correspond to a different flight phase of the aircraft. The edge control device may be operable to engage, in response to a selection of a first control device position, a command mode for actuating the high-lift device in an automated manner based on the flight phase associated with the first control device position.

8. 发明公开

EP1619119A3 Wing assembly for an ultralight aircraft, and ultralight aircraft provided with such wing assembly 有权转让
标题翻译：对于轻型飞机和超轻型飞机这样的机翼组装机翼组装件
公开(公告)号：EP1619119A3
公开(公告)日：2006-05-17
申请号：EP05106775.9
申请日：2005-07-22
申请人： I.C.P. S.r.l.
发明人： Razzano, Tancredi
IPC分类号： B64C31/028 , B64C9/16 , B64C9/28
CPC分类号： B64C9/28 , B64C31/028
摘要： In an ultralight aircraft (1), each wing (3) has an intermediate elongated portion (4) integrally connected to the fuselage (B), and two movable elongated portions (5)(6) arranged on opposite sides of the intermediate elongated portion(4); the position of both the movable elongated portions (5) (6) can be adjusted with respect to the intermediate elongated portion(4) simultaneously and in a synchronised manner by operating one single main actuator (15) connected to the movable elongated portions (5) (6) which are moved by means of a mechanical lever transmission (17).

9. 发明公开

EP1619119A2 Wing assembly for an ultralight aircraft, and ultralight aircraft provided with such wing assembly 有权转让
标题翻译：对于轻型飞机和超轻型飞机这样的机翼组装机翼组装件
公开(公告)号：EP1619119A2
公开(公告)日：2006-01-25
申请号：EP05106775.9
申请日：2005-07-22
申请人： I.C.P. S.r.l.
发明人： Razzano, Tancredi
IPC分类号： B64C31/028 , B64C9/16 , B64C9/28
CPC分类号： B64C9/28 , B64C31/028
摘要： In an ultralight aircraft (1), each wing (3) has an intermediate elongated portion (4) integrally connected to the fuselage (B), and two movable elongated portions (5)(6) arranged on opposite sides of the intermediate elongated portion(4); the position of both the movable elongated portions (5) (6) can be adjusted with respect to the intermediate elongated portion(4) simultaneously and in a synchronised manner by operating one single main actuator (15) connected to the movable elongated portions (5) (6) which are moved by means of a mechanical lever transmission (17).
摘要翻译：在一超轻型飞行器（1），每个翼（3）具有在中间细长部分（4）一体地连接到所述机身（B），和两个可移动细长部（5）（6）布置在中间细长部分的相对侧（4）; 这两个可移动细长部的位置（5）（6）可相对于中间细长部分被调整（4）同时并通过操作连接到所述可动的细长部分中的一个单一的主致动器（15）以同步的方式（5 ）（6），其是通过机械杠杆传动（17来移动）。

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