-
-
公开(公告)号：EP1989466A1
公开(公告)日：2008-11-12
申请号：EP07705310.6
申请日：2007-03-01
申请人： Airbus UK Limited
IPC分类号： F16H25/20
CPC分类号： F16H25/205 , B64C13/28 , B64C25/30 , F16H2025/2059 , Y10T74/18576 , Y10T74/18672
摘要： An actuator (2) comprises first and second linear motion devices, each able to extend the actuator (2) and arranged such that jamming of one of the first or second linear motion devices does not preclude operation of the other. The first linear motion device comprises a first linear screw (10), a first nut (12), and a first prime mover (14) arranged to impart relative linear motion between the screw and nut. Similarly, the second linear motion device comprises a second linear screw (20), a second nut (22), and a second prime mover (24) arranged to impart relative linear motion between the second screw and nut. The first linear screw (10) may have a bore (18) in which the second linear screw (20) is accommodated when the actuator (2) is in the retracted position.
-
公开(公告)号：EP3020632B1
公开(公告)日：2018-12-26
申请号：EP14193083.4
申请日：2014-11-13
摘要： An aircraft landing gear assembly (10) includes lock link (16) and a rotary electromechanical actuator (18) which includes motor and gearbox unit (20) arranged to move a pawl (22) into contact with the lock link to break the lock link. A release mechanism is provided to enable the lock link to be made in the event of the motor and gearbox unit jamming.
-
公开(公告)号：EP3106389B1
公开(公告)日：2018-02-14
申请号：EP15382312.5
申请日：2015-06-15
发明人： ABARCA LOPEZ, Ramon , BARTH, Marcus , WOOD, Norman
IPC分类号： B64C25/00
摘要： The invention refers to a method for operating a landing gear system, preferably in a tricycle configuration, wherein main landing gear (MLG) and the nose landing gear (NLG) are operable from a retracted position where they are housed respectively inside landing gear bays, to a fully extended position where they are extended for landing the aircraft. According to the invention, the extension of the nose landing gear (NLG) is delayed in time with respect to the extension of the main landing gear (MLG), and the nose landing gear (NLG) is kept retracted during a major part of the time that the main landing gear doors (MLGD) are extended. In this manner, vibrations on the main landing gear doors are reduced and incidents caused by fatigue are also reduced, with in turn implies that the maintenance cost of the aircraft is greatly reduced.
-
公开(公告)号：EP3106389A1
公开(公告)日：2016-12-21
申请号：EP15382312.5
申请日：2015-06-15
发明人： ABARCA LOPEZ, Ramon , BARTH, Marcus , WOOD, Norman
IPC分类号： B64C25/00
摘要： The invention refers to a method for operating a landing gear system, preferably in a tricycle configuration, wherein main landing gear (MLG) and the nose landing gear (NLG) are operable from a retracted position where they are housed respectively inside landing gear bays, to a fully extended position where they are extended for landing the aircraft. According to the invention, the extension of the nose landing gear (NLG) is delayed in time with respect to the extension of the main landing gear (MLG), and the nose landing gear (NLG) is kept retracted during a major part of the time that the main landing gear doors (MLGD) are extended. In this manner, vibrations on the main landing gear doors are reduced and incidents caused by fatigue are also reduced, with in turn implies that the maintenance cost of the aircraft is greatly reduced.
摘要翻译： 本发明涉及一种用于操作起落架系统的方法，优选为三轮车配置，其中主起落架（MLG）和前起落架（NLG）可从分别容纳在起落架舱内的缩回位置操作， 到达完全延伸的位置，在那里它们被延伸以着陆飞机。 根据本发明，前起落架（NLG）的延伸相对于主起落架（MLG）的延伸在时间上延迟，而起落架（NLG）在主要起落架 主起落架门（MLGD）延伸的时间。 以这种方式，主起落架门的振动减少，疲劳引起的事故也减少，这又意味着飞机的维护成本大大降低。
-
6.发明公开Actionneur télescopique à tige principale et tige auxiliaire, et procédé faisant application 有权伸缩式致动与主和辅助极，并利用所述致动器的方法
公开(公告)号：EP1801007A1
公开(公告)日：2007-06-27
申请号：EP06291962.6
申请日：2006-12-18
申请人： MESSIER-BUGATTI
发明人： Bucheton, Daniel , Charuel, Hervé
CPC分类号： F16H25/205 , B64C25/30 , F16H2025/2059 , F16H2025/2075 , Y10T74/18576 , Y10T74/186
摘要： L'invention concerne un actionneur télescopique comportant un corps (1) dans lequel une tige principale (2) est montée pour coulisser télescopiquement selon un axe de coulissement (X) entre une position rentrée et une position sortie. L'actionneur comporte une tige auxiliaire (20) montée pour coulisser télescopiquement dans la tige principale selon le dit axe de coulissement entre une position rentrée et une position sortie, l'actionneur comportant des moyens commandés de retenue (30,31,32,33) de la tige auxiliaire en position rentrée dans la tige principale.
摘要翻译： 致动器具有一个气缸（1）一个限定腔，其中主杆（2）被安装，并在辅助杆（20）安装成沿着回缩状态之间的滑动轴主杆可伸缩地滑动，并延伸至的位置。 受控保持单元保持在主杆内的缩回位置所述杆（20），并包括锁扣（30）。 该单元具有从锁定位置和释放位置在杆（20）和一个锁定套筒（32）的端部设置有台阶（31），通过在解锁马达（33）轴向移动。 因此独立claimsoft包括用于使用在致动器的方法。
-
公开(公告)号：EP3366581A1
公开(公告)日：2018-08-29
申请号：EP18157968.1
申请日：2018-02-21
CPC分类号： B64C25/30 , B64C25/20 , B64C25/24 , B64D2221/00 , H02J4/00
摘要： Système d'extension de secours d'au moins un atterrisseur d'aéronef, le système d'extension de secours comprenant des actionneurs électromécaniques, chaque actionneur électromécanique comportant un composant d'identification agencé pour attribuer audit actionneur électromécanique un identifiant qui dépend notamment d'une fonction réalisée par ledit actionneur électromécanique, et une carte électrique (20) comprenant un composant de retard agencé pour retarder un actionnement dudit actionneur électromécanique d'un retard d'actionnement qui dépend de l'identifiant attribué audit actionneur électromécanique, les actionneurs électromécaniques du système d'extension de secours étant ainsi agencés pour être actionnés successivement selon une séquence d'actionnement définie par les retards d'actionnement.
-
公开(公告)号：EP2602184B1
公开(公告)日：2018-03-07
申请号：EP12194845.9
申请日：2012-11-29
CPC分类号： E05C3/12 , B64C25/30 , E05B2047/0013 , E05B2047/002 , E05B2047/0024 , E05C3/24 , Y10T292/0947
-
9.发明公开AIRCRAFT LANDING GEAR DOOR ACTUATION MECHANISM WITH INTEGRATED EMERGENCY ACTUATION ASSEMBLY 审中-公开FLUGZEUGFAHRWERKTÜRBETÄTIGUNGSMECHANISMUSMIT INTEGRIERTERNOTFALLBETÄTIGUNGSANORDNUNG
公开(公告)号：EP3141477A1
公开(公告)日：2017-03-15
申请号：EP16187980.4
申请日：2016-09-09
申请人： Embraer S.A.
发明人： Rogulski Filho, Carlos , Dias Ferraz, David , Tognozzi Lopes, Graco , Nunes De Mattos, Arilton , De Martino, Claudio
CPC分类号： B64C25/16 , B64C25/10 , B64C25/30 , B64C2025/125
摘要： Landing gear doors may be opened in an emergency event, e.g., a failure of the normal landing gear actuation system that requires a gravity free-fall deployment. The retractable aircraft landing gear door actuation mechanism will include a landing gear door (12-1) and a door support bracket (22) attached to the landing gear door. The support bracket (22) is attached to aircraft structure (10-1) for pivotal movement about a pivot axis (22-1a) between a closed condition whereby the landing gear door covers an aircraft landing gear when retracted relative to the aircraft structure, and an opened condition whereby the landing gear door is moved laterally and upwardly relative to the aircraft landing gear when extended relative to the aircraft structure. A gear door actuation assembly (40) is operatively connected to the door support bracket (22) for moving the door support bracket and the gear door supported thereby between the closed and opened conditions thereof. The gear door actuation assembly will include an over-the-center spring assembly (50) which assists in pivotal movement of the door support bracket (22) and the gear door (12-1) supported thereby from the closed condition into the opened condition thereof.
摘要翻译： 起落架门可能在紧急情况下打开，例如需要重力自由落体部署的正常起落架致动系统的故障。 可伸缩飞机起落架门致动机构将包括起落架门（12-1）和附接到起落架门的门支撑架（22）。 支撑托架（22）附接到飞行器结构（10-1），用于在关闭状态之间围绕枢转轴线（22-1a）枢转运动，由此当相对于飞行器结构缩回时起落架门覆盖飞机起落架， 以及打开状态，由此当相对于飞机结构延伸时，起落架门相对于飞行器起落架横向和向上移动。 齿轮门致动组件（40）可操作地连接到门支撑支架（22），用于在其关闭和打开的状态之间移动门支撑支架和由其支撑的齿轮门。 齿轮门致动组件将包括一个中心以上的弹簧组件（50），其帮助门支撑托架（22）和由其支撑的齿轮门（12-1）从关闭状态转动到打开状态 它们。
-
公开(公告)号：EP2855261A4
公开(公告)日：2017-03-08
申请号：EP13800839
申请日：2013-06-04
CPC分类号： F15B15/14 , B64C25/30 , F15B15/088 , F15B15/19 , F15B2211/8752 , F15B2211/8757 , F16H25/20 , F16H25/2015 , F16H2025/2071 , F16H2025/2081
摘要： An actuator assembly includes an actuation member, a release member, and a source of pressurized gas, wherein during a normal mode of operation, the actuation member and the release member are engaged to move in unison, and wherein during an emergency mode of operation, pressurized gas automatically decouples the actuation member from the release member to move separately. In accordance with yet other aspects of the present disclosure, an electro-mechanical actuator includes an electro-mechanical drive system and an integrated backup system operated by a gas generator, wherein when the backup system is activated, the electro-mechanical drive system is decoupled and the actuator moves to a predetermined position and mechanically locks in place.
摘要翻译： 致动器组件包括致动构件，释放构件和加压气体源，其中在正常操作模式期间，致动构件和释放构件接合以一致地移动，并且其中在紧急操作模式期间， 加压气体将致动构件与释放构件自动分离以单独移动。 根据本公开的其他方面，一种机电致动器包括机电驱动系统和由气体发生器操作的集成备用系统，其中当备用系统被激活时，机电驱动系统被解耦 并且致动器移动到预定位置并且机械锁定就位。
-
-
-
-
-
-
-
-
-
搜索结果
37 条记录 (耗时 0.012 秒)
