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91. 发明授权

EP2803584B1 Actuation system for flight control surface 有权
标题翻译：用于飞行控制面操作系统
公开(公告)号：EP2803584B1
公开(公告)日：2015-09-16
申请号：EP13168196.7
申请日：2013-05-17
申请人： Airbus Operations GmbH
发明人： Brady, Michael , Winkelmann, Christoph
IPC分类号： B64D45/00 , B64C9/16 , B64C13/34
CPC分类号： B64F5/60 , B64C9/16 , B64C13/28 , B64D45/0005 , B64D2045/001

92. 发明授权

EP2544947B1 SLAT MONITORING SYSTEM AND METHOD 有权
标题翻译：系统和监测方法LATTE
公开(公告)号：EP2544947B1
公开(公告)日：2015-05-06
申请号：EP11710546.0
申请日：2011-03-04
申请人： Airbus Operations Limited
发明人： PARKER, Simon John
IPC分类号： B64C9/22 , G01D5/347 , B64D45/00
CPC分类号： B64C9/22 , B64D45/0005 , B64D2045/001

93. 发明公开

EP2666716A2 Integrated torque limiter/no-back device 有权
标题翻译： Integrierter Drehmomentbegrenzer /Rückstellverhinderer
公开(公告)号：EP2666716A2
公开(公告)日：2013-11-27
申请号：EP13168099.3
申请日：2013-05-16
申请人： Hamilton Sundstrand Corporation
发明人： Finney, Adam M.
IPC分类号： B64C9/16 , B64C9/22 , B64D45/00
CPC分类号： F16D67/02 , B64C13/24 , B64C13/28 , B64D2045/001 , F16D7/005 , F16D43/215 , F16D43/218 , F16D55/02 , F16D55/16 , F16D55/48 , F16D2125/38 , F16H35/10 , Y02T50/44
摘要： An integrated torque limiter/no-back device (36) for use in an actuator (20) with an input shaft (30), an output (34) and gear reduction (32). The device includes an input ramp (38) to receive torque from the input shaft (30); a combined ramp (40) to transfer torque; an output ramp (42) to transfer torque to the gear reduction (32); one or more balls (46; 48) between the input ramp (38) and the combined ramp (40) and between the combined ramp (40) and the output ramp (42) to transfer torque; and a brake (44; 45) for causing torque to be grounded and for preventing backdriving of the input shaft by preventing movement of one or more of the input ramp (38), the combined ramp (40) and the output ramp (42) when a torque threshold has been met. The input ramp and the output ramp are one of a no-back ramp (42) and a torque limiter ramp (38), respectively, and the device (36) also includes a pin (50) between the combined ramp (40) and one or more of the no-back ramp (42) and the gear reduction (32) for transferring torque.
摘要翻译：一种用于具有输入轴（30），输出（34）和齿轮减速（32）的致动器（20）中的集成扭矩限制器/无返回装置（36）。该装置包括从输入轴（30）接收扭矩的输入斜坡（38）; 传递扭矩的组合斜坡（40）; 输出斜坡（42）以将扭矩传递到齿轮减速（32）; 在输入斜坡（38）和组合斜坡（40）之间以及组合斜坡（40）和输出斜坡（42）之间的一个或多个球（46; 48）以传递扭矩; 以及用于使扭矩接地的制动器（44; 45），并且用于通过防止输入斜坡（38），组合斜坡（40）和输出斜坡（42）中的一个或多个的移动来防止输入轴的反向驱动，当满足扭矩阈值时。输入斜坡和输出斜坡分别是无背斜面（42）和扭矩限制器斜坡（38）之一，并且装置（36）还包括在组合斜坡（40）和一个或多个无背斜面（42）和用于传递扭矩的齿轮减速（32）。

94. 发明授权

EP2419332B1 HOCHAUFTRIEBSSYSTEM FÜR EIN FLUGZEUG UND VERFAHREN ZUM DETEKTIEREN VON FEHLERN IN EINEM HOCHAUFTRIEBSSYSTEM FÜR EIN FLUGZEUG 有权
标题翻译：高升力系统，用于检测误差的高升力系统用于飞行器的飞机和方法
公开(公告)号：EP2419332B1
公开(公告)日：2013-09-11
申请号：EP10713649.1
申请日：2010-04-14
申请人： Airbus Operations GmbH
发明人： SPILLER, Olaf
IPC分类号： B64D45/00 , B64C9/16
CPC分类号： B64D45/0005 , B64C9/16 , B64D2045/001 , Y02T50/44

95. 发明公开

EP2625104A1 HIGH LIFT SYSTEM FOR AN AIRCRAFT WITH A SEPARATE DRIVE UNIT FOR EACH WING HALF 有权
标题翻译： HOCHAUFTRIEBSSYSTEMFÜREIN FLUGZEUG MIT SEPARATER ANTRIEBSEINHEITFÜRJEDETRAGFLÄCHENHÄLFTE
公开(公告)号：EP2625104A1
公开(公告)日：2013-08-14
申请号：EP11764226.4
申请日：2011-10-05
申请人： Airbus Operations GmbH
发明人： RICHTER, Martin
IPC分类号： B64D45/00 , B64C13/30
CPC分类号： B64C13/28 , B64C13/30 , B64D45/0005 , B64D2045/001 , Y02T50/44
摘要： A high-lift system on a wing of an aircraft is provided. The wing includes a right-hand and a left-hand wing half with movably held high-lift flaps and the right-hand and left-hand wing half are attached to an aircraft fuselage, thus forming a wing root. Each wing half in a region in close proximity to the wing root, includes a drive unit. In each case this drive unit is joined to a transmission shaft mechanically connected to the respective drive unit, which transmission shaft extends from the drive unit in the direction of the end of the respective wing half and is designed to mechanically move the high-lift flaps arranged in the respective wing half. By means of such an arrangement it is possible to do without deflection gear arrangements from a central drive unit to the individual wing halves.
摘要翻译：提供飞机机翼上的高升程系统。机翼包括右手和左手翼半部，其具有可移动地保持的高提升襟翼，右侧和左侧翼半部附接到飞行器机身，从而形成翼根。在靠近翼根的区域中的每个翼半部包括驱动单元。在每种情况下，该驱动单元连接到机械地连接到相应驱动单元的传动轴，该传动轴从驱动单元沿着相应的翼半部的端部的方向延伸，并被设计成机械地移动高升降翼布置在相应的翼半部。通过这种布置，可以在没有偏转齿轮装置的情况下从中心驱动单元到单独的翼片半部进行。

96. 发明公开

EP2555979A2 CONTROL SURFACE ELEMENT SKEW AND / OR LOSS DETECTION SYSTEM 有权
标题翻译：测量系统的扭转和/或损失TAX区域元件
公开(公告)号：EP2555979A2
公开(公告)日：2013-02-13
申请号：EP11713025.2
申请日：2011-03-23
申请人： Moog Wolverhampton Limited
发明人： THOMAS, Glynn
IPC分类号： B64D45/00
CPC分类号： B64D45/0005 , B64C13/28 , B64D2045/001
摘要： A control surface element skew and/or loss detection system (100) is provided which combines a cable (168, 178) system linked to movement transducers (120) via mechanical links (114, 116) connecting the fixed wing structure (102) to the control surface elements (106, 112).

97. 发明公开

EP2530019A1 Resolver type skew sensor with gimbal attachment 审中-公开
标题翻译： DrehsensorfürKlappenasymmetrie mit kardanischerAufhängung
公开(公告)号：EP2530019A1
公开(公告)日：2012-12-05
申请号：EP12169998.7
申请日：2012-05-30
申请人： Hamilton Sundstrand Corporation
发明人： Wallen, Gregory T. , Regan, James M. , Lang, David J. , Crandall-Seibert, Cory M. , Miller, Mark D. , Leden, William E. , Baines, Andrew N. , Jacobs, Jeffrey Paul
IPC分类号： B64D45/00
CPC分类号： B64D45/0005 , B64D2045/001
摘要： A disclosed sensor assembly 16 for detecting movement and a position of a wing flap 14 includes a sensing device 18 that generates a signal corresponding to a position of the flap. The sensor assembly includes a linkage 20 that is attached to the movable flap for mechanically communicating movement of the flap to the sensing device. The linkage includes a first pivot shaft 36 mounted to the flap that is disposed about a first axis and a second pivot shaft 34 attached to the first pivot shaft for movement about a second axis transverse to the first axis.
摘要翻译：用于检测机翼翼片14的运动和位置的公开的传感器组件16包括感测装置18，该感测装置18产生对应于翼片的位置的信号。传感器组件包括连接到活动翼片的连杆20，用于将翼片的运动机械地连接到传感装置。联动装置包括安装在围绕第一轴线设置的翼片的第一枢转轴36和连接到第一枢转轴的第二枢转轴34，用于绕横向于第一轴线的第二轴线移动。

98. 发明公开

EP2447161A2 Cantilevered differential motion sensor and associated frame 有权转让
标题翻译： Freischwebender Differenzialbewegungssensor undzugehörigerRahmen
公开(公告)号：EP2447161A2
公开(公告)日：2012-05-02
申请号：EP11181885.2
申请日：2011-09-19
申请人： Hamilton Sundstrand Corporation
发明人： Carbone, Michael
IPC分类号： B64D45/00
CPC分类号： B64D45/0005 , B64D2045/001 , Y10T29/49826
摘要： The disclosed sensor (50;150) includes a frame having a base (26;126) and a plurality of arms (22,24;122,124) integral with the base. The arms are biased to a relaxed position, which may be an extended position. A fuse (40;140) is fastened between the arms to hold the arms in a non-relaxed position. When incorporated into an aircraft, for example, the disclosed sensor may be connected to a first panel (72), and a pin (60) connected to a second panel (74) may be positioned between the arms.
摘要翻译：所公开的传感器（50; 150）包括具有底座（26; 126）和与基座成一体的多个臂（22,24; 122,124）的框架。臂被偏置到松弛位置，其可以是延伸位置。保险丝（40; 140）被紧固在臂之间以将臂保持在非放松位置。例如，当结合到飞行器中时，所公开的传感器可以连接到第一面板（72），并且连接到第二面板（74）的销（60）可以定位在臂之间。

99. 发明公开

EP2368794A2 Aircraft slat disconnect sensor 审中-公开
标题翻译： Flugzeugvorflügel-Trennungssensor
公开(公告)号：EP2368794A2
公开(公告)日：2011-09-28
申请号：EP11250338.8
申请日：2011-03-18
申请人： Hamilton Sundstrand Corporation
发明人： Mayer, Timothy Michael , Hastings, Paul F. , Massolle Jr, Dale, W.
IPC分类号： B64C9/18 , B64D45/00
CPC分类号： B64C9/18 , B64D45/0005 , B64D2045/001
摘要： A slat disconnect sensor (32;32;232) includes a base (68). First and second arms (60,62;260,262) are spaced apart from one another and are operatively supported by the base. (68) At least one of the first and second arms have an end (64) mounted to the base and is rotatable relative thereto at a pivot (72) between connect and disconnect conditions. A mechanical link (82;246) includes first and second link portions (84,86) respectively secured to the first and second arms. The link interconnects the first and second arms and includes a weakened area (88) providing a frangible connection in the connect condition and is configured to break at the frangible connection in the disconnect condition. A fuse (82;182;226) includes first and second fuse portions (84,86;228,230) operatively mounted to the first and second arms. The fuse is interconnected between the first and second arms providing continuity in the connected condition, and continuity is broken between the first and second portions in the disconnect condition.
摘要翻译：板条断开传感器（32; 32; 232）包括基座（68）。第一和第二臂（60,62; 260,262）彼此间隔开并由底座可操作地支撑。（68）第一和第二臂中的至少一个具有安装到基座的端部（64）并且可以在连接和断开状态之间的枢轴（72）处相对于其旋转。机械连杆（82; 246）包括分别固定到第一和第二臂的第一和第二连杆部分（84,86）。所述连杆将所述第一臂和所述第二臂互连，并且包括在所述连接状态下提供易碎连接的弱化区域（88），并且构造成在所述断开状态下在所述易碎连接处断裂。保险丝（82; 182; 226）包括可操作地安装到第一和第二臂的第一和第二保险丝部分（84,86; 228,230）。保险丝在第一和第二臂之间互连，在连接状态下提供连续性，并且断开状态下的第一和第二部分之间的连续性断裂。

100. 发明授权

EP1966043B1 AIRFOIL FOR AN AIRCRAFT AND AIRCRAFT 有权
标题翻译： WING用于飞机和飞机
公开(公告)号：EP1966043B1
公开(公告)日：2011-08-03
申请号：EP06830855.0
申请日：2006-12-29
申请人： Airbus Operations GmbH
发明人： POHL, Ulrich
IPC分类号： B64C9/00 , B64C13/24
CPC分类号： B64C9/16 , B64C13/24 , B64D45/0005 , B64D2045/001
摘要： The invention relates to the monitoring of the landing flaps on an airfoil (2) for an aircraft (1), and to an aircraft (1) having such an airfoil (2). The airfoil (2) has a wingbox (3), a support (5) which is mounted relative to the wingbox (3) such that it can rotate with respect to a flap rotation axis (7), a flap (4) which is attached to the support (5) and rotates with respect to the flap rotation axis (7) during rotation of the support (5) relative to the wingbox (3), a movement mechanism (8) which is coupled to the support (5) in order to set an angle position of the flap (4) with respect to the wingbox (3) and a measurement apparatus (18) for detection of the angle position of the flap (4). The measurement apparatus (18) has a rotation sensor (19), which is arranged on the support (5), and a four-element coupling transmission (22, 24, 26, 27) which couples the rotation sensor (19) to the movement mechanism (8).

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