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1. 发明公开

EP2490934A2 AIRCRAFT HORIZONTAL STABILISER FITTED WITH LEADING-EDGE STRAKE 有权
标题翻译：配备前缘水平面STABILISATOR
公开(公告)号：EP2490934A2
公开(公告)日：2012-08-29
申请号：EP10773273.7
申请日：2010-10-18
申请人： Airbus Operations Limited , Airbus Operations GmbH , Airbus Opérations SAS
发明人： WHITEHOUSE, Ian , WEBER, Carsten , FISCHER, Markus , TANGUY, Alain
IPC分类号： B64C5/02 , B64C23/06
CPC分类号： B64C5/02 , B64C23/06 , Y02T50/162
摘要： An adjustable, or all -moving, horizontal stabiliser (4) for an aircraft, the stabiliser having a leading edge, a trailing edge, a root and a tip, and a strake (7) fixed with respect to the stabiliser (4) and attached to, or integrally formed with, the stabiliser leading edge adjacent the root.

2. 发明授权

EP2490934B1 AIRCRAFT HORIZONTAL STABILISER FITTED WITH LEADING-EDGE STRAKE 有权
标题翻译：配备前缘水平面STABILISATOR
公开(公告)号：EP2490934B1
公开(公告)日：2016-08-03
申请号：EP10773273.7
申请日：2010-10-18
申请人： Airbus Operations Limited , Airbus Operations GmbH , Airbus Opérations SAS
发明人： WHITEHOUSE, Ian , WEBER, Carsten , FISCHER, Markus , TANGUY, Alain
IPC分类号： B64C5/02 , B64C23/06
CPC分类号： B64C5/02 , B64C23/06 , Y02T50/162

3. 发明公开

EP2408667A2 AN AIRCRAFT COMPRISING A DEVICE FOR INFLUENCING THE DIRECTIONAL STABILITY OF THE AIRCRAFT, AND A METHOD FOR INFLUENCING THE DIRECTIONAL STABILITY OF THE AIRCRAFT 有权
标题翻译：与设备平面影响稳飞机和方法的方向影响飞机的方向稳定性
公开(公告)号：EP2408667A2
公开(公告)日：2012-01-25
申请号：EP10710221.2
申请日：2010-03-17
申请人： Airbus Operations GmbH , Airbus Opérations SAS
发明人： WEBER, Carsten , FISCHER, Markus , NAMER, Arnaud
IPC分类号： B64C9/04
CPC分类号： B64C5/06 , B64C9/32 , Y02T50/32
摘要： An aircraft including a device for influencing the directional stability of the aircraft is provided. The device includes a control-input device; a flight control device; a sensor device for acquiring the rotation rates, including the yaw rates, of the aircraft; and at least one actuator, which is coupled with ailerons, spoilers, an elevator and a rudder. The flight control device includes a control function generating adjusting commands for the actuators for controlling the aircraft according to control commands. The aircraft includes two tail-mounted flaps, each including an actuator connected with the flight control device, situated symmetrically to each other and on opposite sides of the fuselage, and movable between retracted and extended positions. The control function is designed such that the adjusting commands that are generated on the basis of the control commands depending on the acquired rotation rates include adjusting commands to the actuators of the tail-mounted flaps.
摘要翻译：提供一种飞机，包括用于影响飞机的方向稳定性的装置。该装置包括一个控制输入装置; 一个飞行控制装置; 的传感器装置，用于获取所述旋转率，包括偏航率，飞行器的; 和至少一个致动器，所有这一切都耦合于副翼，扰流板，电梯和舵。飞行控制装置包括控制函数生成调节用于致动器的命令，用于控制飞行器gemäß控制命令。飞行器包括两个尾装式襟翼，每一个包括在与飞行控制装置致动器相连，对称位于海誓山盟和机身的相对侧上，以及缩回和伸出位置之间移动。控制功能被设计检查做了调整指令所做的控制命令根据所获取的旋转率的基础上产生包括调整命令到尾装式襟翼的致动器。

4. 发明授权

EP2408667B1 AN AIRCRAFT COMPRISING A DEVICE FOR INFLUENCING THE DIRECTIONAL STABILITY OF THE AIRCRAFT, AND A METHOD FOR INFLUENCING THE DIRECTIONAL STABILITY OF THE AIRCRAFT 有权
标题翻译：包含影响飞机方向稳定性的装置的飞机以及影响飞机方向稳定性的方法
公开(公告)号：EP2408667B1
公开(公告)日：2018-05-02
申请号：EP10710221.2
申请日：2010-03-17
申请人： Airbus Operations GmbH , Airbus Opérations SAS
发明人： WEBER, Carsten , FISCHER, Markus , NAMER, Arnaud
IPC分类号： B64C9/04
CPC分类号： B64C5/06 , B64C9/32 , Y02T50/32
摘要： An aircraft including a device for influencing the directional stability of the aircraft is provided. The device includes a control-input device; a flight control device; a sensor device for acquiring the rotation rates, including the yaw rates, of the aircraft; and at least one actuator, which is coupled with ailerons, spoilers, an elevator and a rudder. The flight control device includes a control function generating adjusting commands for the actuators for controlling the aircraft according to control commands. The aircraft includes two tail-mounted flaps, each including an actuator connected with the flight control device, situated symmetrically to each other and on opposite sides of the fuselage, and movable between retracted and extended positions. The control function is designed such that the adjusting commands that are generated on the basis of the control commands depending on the acquired rotation rates include adjusting commands to the actuators of the tail-mounted flaps.

5. 发明公开

EP2625096A1 DEVICE AND METHOD FOR INCREASING THE AERODYNAMIC LIFT OF AN AIRCRAFT 有权
标题翻译： VORRICHTUNG UND VERFAHREN ZURERHÖHUNGDES AERODYNAMISCHEN HUBS EINES FLUGZEUGES
公开(公告)号：EP2625096A1
公开(公告)日：2013-08-14
申请号：EP11767986.0
申请日：2011-10-05
申请人： Airbus Operations GmbH
发明人： WEBER, Carsten , FISCHER, Markus , GROTE, Arne , RADESPIEL, Rolf , DREYER, Martin
IPC分类号： B64C5/12 , B64C9/34 , B64C23/06
CPC分类号： B64C23/06 , B64C5/12 , B64C9/34 , Y02T50/162 , Y02T50/44
摘要： A lift arrangement for an aircraft (2) comprises an aircraft fuselage section with an outside (3), an aerodynamic lift body (6, 8)attached to the aircraft fuselage section and extending from the aircraft fuselage section outwardly, and a pair of movably held add-on bodies (12)arranged upstream of a leading edge (14) of the aerodynamic lift body (6, 8). The add-on bodies(12) comprise an aerodynamically effective surface and are equipped with incoming airflow to generate vortices (18) that impinge on the aerodynamic lift body (6, 8), thus leading to an increase inlift on the aerodynamic lift body (6, 8). Consequently it becomes possible with simple means to effectively influence lift generation on a lift body (6, 8), in particular to compensate for loss of lift as a result of icing. Preferably, the add-on bodies are moveable, and, when operational conditions do not require the use of said add-on bodies, can be moved to a neutral position in which they do not project into the flow around the aircraft, and are thus not effective from the point of view of fluid dynamics.
摘要翻译：飞机的电梯装置包括具有外部的飞机机身部分，附接到飞行器机身部分并从飞行器机身部分向外延伸的空气动力升降体，以及一对可移动地固定的附加物体，其布置在前缘的气动提升体。附加物体包括空气动力学有效的表面，并且配备有进入的气流以产生冲击空气动力升力体的涡流，从而导致空气动力升降体的升力增加。因此，电梯主体上的电梯产生有效地受到影响，特别是为了补偿结冰导致的电梯损失。附加物体是可移动的，并且可以移动到中性位置，在该位置中它们不会投射到飞机周围的流中，并且因此从流体动力学的角度来看是没有效果的。

6. 发明授权

EP2625096B1 DEVICE AND METHOD FOR INCREASING THE AERODYNAMIC LIFT OF AN AIRCRAFT 有权
标题翻译：用于增加飞行器的气动升降装置和方法
公开(公告)号：EP2625096B1
公开(公告)日：2017-07-19
申请号：EP11767986.0
申请日：2011-10-05
申请人： Airbus Operations GmbH
发明人： WEBER, Carsten , FISCHER, Markus , GROTE, Arne , RADESPIEL, Rolf , DREYER, Martin
IPC分类号： B64C5/12 , B64C9/34 , B64C23/06
CPC分类号： B64C23/06 , B64C5/12 , B64C9/34 , Y02T50/162 , Y02T50/44

7. 发明授权

EP3334650B1 AIRCRAFT DOOR ARRANGEMENT WITH A NOISE REDUCED HOLLOW SPACE WHICH CAN BE COVERED BY AN AIRCRAFT DOOR 有权
公开(公告)号：EP3334650B1
公开(公告)日：2019-07-17
申请号：EP16750178.2
申请日：2016-08-11
申请人： Airbus Operations GmbH
发明人： FISCHER, Markus , HANKE, Jean-Marc , DITTMANN, Uwe , SIERCKE, Matthias , KAGEL, Sebastian , HOUTROUW, Enno , FRENZEL, Peter-Philipp
IPC分类号： B64C1/14 , B64C1/40

8. 发明公开

EP3334650A1 AIRCRAFT DOOR ARRANGEMENT WITH A NOISE REDUCED HOLLOW SPACE WHICH CAN BE COVERED BY AN AIRCRAFT DOOR 有权
公开(公告)号：EP3334650A1
公开(公告)日：2018-06-20
申请号：EP16750178.2
申请日：2016-08-11
申请人： Airbus Operations GmbH
发明人： FISCHER, Markus , HANKE, Jean-Marc , DITTMANN, Uwe , SIERCKE, Matthias , KAGEL, Sebastian , HOUTROUW, Enno , FRENZEL, Peter-Philipp
IPC分类号： B64C1/14 , B64C1/40
CPC分类号： B64C1/1461 , B64C1/14 , B64C1/1407 , B64C1/40 , Y02T50/46
摘要： An aircraft door arrangement includes a door, a door seal, and a door opening. The door opening has an opening edge adjoining the door opening and extending into the aircraft fuselage, at which a seal seat is arranged, which can be brought into flush contact with the door seal. A hollow space, partially covered by the edge region of the door, is formed by the door seal, the seal seat, and the opening edge. A gap (located between the door and the door opening when the aircraft door is closed) is connected with the hollow space. A sound reducing profile is arranged at the opening edge in the hollow space, and it includes a sound reflecting surface oriented oblique with respect to a surface of the door, which is adjacent to the gap. The sound reflecting surface at least partially follows the course of the gap.

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