公开(公告)号：US20200070951A1

公开(公告)日：2020-03-05

申请号：US16552373

申请日：2019-08-27

申请人： Airbus Defence and Space GmbH

发明人： Wolfgang MACHUNZE ,  Heiko FIETZEK

IPC分类号： B64C3/18

摘要： An end rib assembly for a high-lift device of an aircraft to reduce the noise caused by the transition between the wing and a high-lift device as well as the noise caused by the lateral side edge of the end rib assembly. An end rib assembly includes a noise-reducing portion configured to reduce noise caused by an airflow around the end rib assembly, and a guiding portion configured for guiding the end rib assembly along a pre-determined path when the high-lift device is moved between a retracted position and an extended position, wherein the guiding portion is formed such that an airflow impinging on the guiding portion is partly guided towards the noise-reducing portion.

公开(公告)号：US20160318239A1

公开(公告)日：2016-11-03

申请号：US15140693

申请日：2016-04-28

申请人： AIRBUS DEFENCE AND SPACE GMBH

发明人： Juergen SILVANUS ,  Heiko FIETZEK

IPC分类号： B29C65/06 ,  B64F5/00 ,  B29C65/00 ,  B29C65/34 ,  B23K20/12 ,  B23K20/22

CPC分类号： B29C65/069 ,  B23K20/122 ,  B23K20/1245 ,  B23K20/22 ,  B23K2103/172 ,  B23K2103/42 ,  B29C65/0681 ,  B29C65/3476 ,  B29C66/0042 ,  B29C66/005 ,  B29C66/1122 ,  B29C66/1142 ,  B29C66/43 ,  B29C66/54 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72321 ,  B29C66/73113 ,  B29C66/73921 ,  B29C66/8122 ,  B29C66/81429 ,  B29C66/836 ,  B29K2105/20 ,  B29K2701/12 ,  B29K2705/00 ,  B29K2705/02 ,  B29L2031/3082 ,  B64C2001/0054 ,  B64F5/10 ,  B29K2905/00 ,  B29K2909/02 ,  B29K2309/08

摘要： A method for manufacturing components includes joining a first edge of a thermoplastic-containing first component part and a second edge of a thermoplastic-containing second component part to one another without any overlap. The first and the second edge are interconnected by friction stir welding. Friction stir welding involves rubbing a rotating friction stir welding pin against at least one metal object.

摘要翻译： 制造部件的方法包括将含热塑性塑料的第一部件的第一边缘和含热塑性塑料的第二部件的第二边缘彼此接合而没有任何重叠。 第一和第二边缘通过摩擦搅拌焊接相互连接。 摩擦搅拌焊接包括将旋转的摩擦搅拌焊接销摩擦至少一个金属物体。

公开(公告)号：US20160144947A1

公开(公告)日：2016-05-26

申请号：US14948765

申请日：2015-11-23

申请人： Airbus Defence and Space GmbH

发明人： Tamas HAVAR ,  Meinhard MEYER ,  Heiko FIETZEK

IPC分类号： B64C9/14

CPC分类号： B64C9/14 ,  B64C9/16 ,  F16C29/02 ,  F16C33/26 ,  F16C2326/43

摘要： A high-lift system for an aircraft includes a high-lift flap which is arranged on the wing of the aircraft and is mounted on a carriage coupled to the wing, the carriage being displaceably mounted on a track by means of a high-lift bearing. The high-lift bearing includes a plain bearing.

摘要翻译： 用于飞行器的高升力系统包括布置在飞行器机翼上的高升降翼，并安装在联接到机翼的滑架上，滑架通过高升力轴承可移动地安装在轨道上 。 高升力轴承包括滑动轴承。