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1. 发明公开

EP2328805A2 HOCHAUFTRIEBSSYSTEM FÜR EIN FLUGZEUG MIT EINER HOCHAUFTRIEBSKLAPPE UND VERFAHREN ZUR VERSTELLUNG DER HOCHAUFTRIEBSKLAPPE 审中-公开
标题翻译：高升力系统用于飞机有用于调整高电梯门的高电梯门和方法
公开(公告)号：EP2328805A2
公开(公告)日：2011-06-08
申请号：EP09778200.7
申请日：2009-08-28
申请人： Airbus Operations GmbH
发明人： RECKZEH, Daniel , SCHINDLER, Klaus
IPC分类号： B64C13/04
CPC分类号： B64C9/24 , B64C9/28 , Y02T50/32
摘要： The invention relates to a high-lift system for an aircraft with at least one high-lift flap arranged on each of the main wings (1) of the aircraft, comprising a pilot input device for generating flight-phase related commands for the at least one high-lift flap, wherein at least one start command is included in the commands, a control device with functional connection to the pilot input device with a converter function by means of which the flight-phase related commands are converted into control actions for operating a drive device for setting or adjusting the at least one high-lift flap adjustment position, wherein a defined flight phase is the start phase and the conversion function of the control device is designed such that said device, on a start command, generates control action at the drive device, such that the leading edge flap (3) of the at least one high lift flap is arranged in an adjustment position wherein there is a gap between the leading edge flap (3) and the main wing (1) with a gap width of 0.1% to 0.4% based on the local wing depth. The invention further relates to a method for adjusting at least one high lift flap on each of the main wings (1) of an aircraft.

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

EP2851292A1 Control interface for leading and trailing edge devices 有权
标题翻译： SteuerungsschnittstellefürEin- und Austrittskantenvorrichtungen
公开(公告)号：EP2851292A1
公开(公告)日：2015-03-25
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
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.
摘要翻译：用于控制飞行器的高升力装置的系统（500）可以包括用于放置在飞行器的飞行甲板中的接口（502）。接口（502）可以包括用于控制高升降装置的位置的边缘控制装置（504）。接口（502）可以用于选择多个控制设备位置（510）中的任何一个。多个控制装置位置（510）中的每一个可对应于飞行器的不同飞行阶段。边缘控制装置可操作以响应于第一控制装置位置的选择而接合基于与第一控制装置位置相关联的飞行阶段以自动方式致动高升降装置的指令模式。

6. 发明公开

EP2692632A4 HIGH-LIFT DEVICE FOR AIRCRAFT 有权
标题翻译：高升力装置 - 飞机
公开(公告)号：EP2692632A4
公开(公告)日：2014-12-31
申请号：EP12764943
申请日：2012-03-28
申请人： SOCIETY OF JAPANESE AEROSPACE COMPANIES , KAWASAKI HEAVY IND LTD
发明人： ISOTANI KAZUHIDE , HAYAMA KENJI
IPC分类号： B64C9/16 , B64C23/00
CPC分类号： B64C9/18 , B64C3/58 , B64C9/16 , B64C9/28 , B64C21/02 , B64C2230/22 , Y02T50/166 , Y02T50/44
摘要： A high-lift device (3) of a flight vehicle includes: a flap main body (11) provided at a trailing edge portion of a main wing (2) of the flight vehicle so as to be extracted from and be retracted in the trailing edge portion and extending in a wing span direction of the main wing (2); and a vortex suppressing portion (100, 200, 300, 400, 500, or 600) provided at a tip end portion of the flap main body (11) in a wing span direction of the flap main body (11) and configured to suppress a vortex rolling up from a lower surface of a tip end portion (11a) of the flap main body (11) to an upper surface of the tip end portion (11a).
摘要翻译：飞行器的高升降装置（3）包括：设置在飞行车辆的主翼（2）的后缘部分处的翼片主体（11），以便从后退中抽出并缩回边缘部分并且沿着主翼（2）的翼展跨度方向延伸; 以及在所述翼片主体（11）的翼展方向上设置在所述翼片主体（11）的前端部的涡流抑制部（100,200,300,400,500,600），并且被构造成抑制从翼片主体（11）的前端部（11a）的下表面向前端部（11a）的上表面卷起的涡流。

7. 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。

8. 发明授权

EP2027518B8 PROCEDE DE PILOTAGE D'UN AERONEF EN PHASE D'APPROCHE 有权转让
公开(公告)号：EP2027518B8
公开(公告)日：2009-11-11
申请号：EP07788845.1
申请日：2007-06-07
申请人： AIRBUS OPERATIONS , Airbus Deutschland GmbH
发明人： DELAPLACE, Franck , RICHTER, Martin , LANG, Dieter
IPC分类号： G05D1/06 , B64C13/18
CPC分类号： B64C9/28 , G05D1/0676
摘要： According to the invention, high lift leading-edge slats (13) and high lift flaps (14) are simultaneously deployed, when the speed of the aircraft is equal to and less than an AES threshold.

9. 发明授权

EP2027518B1 PROCEDE DE PILOTAGE D'UN AERONEF EN PHASE D'APPROCHE 有权转让
标题翻译：一种用于控制飞机搭载在进场着陆
公开(公告)号：EP2027518B1
公开(公告)日：2009-09-02
申请号：EP07788845.1
申请日：2007-06-07
申请人： AIRBUS France , Airbus Deutschland GmbH
发明人： DELAPLACE, Franck , RICHTER, Martin , LANG, Dieter
IPC分类号： G05D1/06 , B64C13/18
CPC分类号： B64C9/28 , G05D1/0676
摘要： According to the invention, high lift leading-edge slats (13) and high lift flaps (14) are simultaneously deployed, when the speed of the aircraft is equal to and less than an AES threshold.

10. 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.

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