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1. 发明授权

US08783615B2 Loads interface, particularly loads interface of an aircraft structure and application of said loads interface 有权
标题翻译：负载接口，特别是负载接口的飞机结构和所述负载接口的应用
公开(公告)号：US08783615B2
公开(公告)日：2014-07-22
申请号：US13553167
申请日：2012-07-19
申请人： Christian Wolf , Hanno Niemann , Matthias Hopf , Patrik Schmiedel
发明人： Christian Wolf , Hanno Niemann , Matthias Hopf , Patrik Schmiedel
IPC分类号： B64C1/14
CPC分类号： B64C1/1407 , E05D5/0207
摘要： A loads interface (1) of an aircraft structure with an edge member (6) and a background structure both preferably made from fiber reinforced plastics. A loads transferring flange (2) is adapted and mounted to said edge member (6) to transmit bending moments into the background structure. Said loads transferring flange (2) is provided with two angled upper and lower planes (8, 9). Said edge member (6) is provided with two angled edge member's upper and lower transfer planes (10, 11). The two angled upper and lower planes (8, 9) and the two angled edge member's upper and lower transfer planes (10, 11) are paired essentially parallel and respectively oriented to each other with an angle of approximately 90°. The invention relates as well to applications of such a loads interface (1).
摘要翻译：具有边缘构件（6）和背景结构的飞行器结构的负载接口（1），其优选地由纤维增强塑料制成。负载传递凸缘（2）适于并安装到所述边缘构件（6）上以将弯矩传递到背景结构中。所述载荷传递凸缘（2）设置有两个成角度的上下平面（8,9）。所述边缘构件（6）设置有两个成角度的边缘构件的上部和下部转移平面（10,11）。两个倾斜的上下平面（8,9）和两个成角度的边缘构件的上下传输平面（10,11）基本上平行配对并且分别以大约90°的角度相互取向。本发明还涉及这种负载接口（1）的应用。

2. 发明申请

US20130032660A1 LOADS INTERFACE, PARTICULARLY LOADS INTERFACE OF AN AIRCRAFT STRUCTURE AND APPLICATION OF SAID LOADS INTERFACE 有权
标题翻译：负载接口，特殊载荷飞机结构接口和适用载荷接口
公开(公告)号：US20130032660A1
公开(公告)日：2013-02-07
申请号：US13553167
申请日：2012-07-19
申请人： Christian Wolf , Hanno Niemann , Matthias Hopf , Patrik Schmiedel
发明人： Christian Wolf , Hanno Niemann , Matthias Hopf , Patrik Schmiedel
IPC分类号： B64C1/06 , B64C1/18 , B64C1/14
CPC分类号： B64C1/1407 , E05D5/0207
摘要： A loads interface (1) of an aircraft structure with an edge member (6) and a background structure both preferably made from fiber reinforced plastics. A loads transferring flange (2) is adapted and mounted to said edge member (6) to transmit bending moments into the background structure. Said loads transferring flange (2) is provided with two angled upper and lower planes (8, 9). Said edge member (6) is provided with two angled edge member's upper and lower transfer planes (10, 11). The two angled upper and lower planes (8, 9) and the two angled edge member's upper and lower transfer planes (10, 11) are paired essentially parallel and respectively oriented to each other with an angle of approximately 90° . The invention relates as well to applications of such a loads interface (1).
摘要翻译：具有边缘构件（6）和背景结构的飞行器结构的负载接口（1），其优选地由纤维增强塑料制成。负载传递凸缘（2）适于并安装到所述边缘构件（6）上以将弯矩传递到背景结构中。所述载荷传递凸缘（2）设置有两个成角度的上下平面（8,9）。所述边缘构件（6）设置有两个成角度的边缘构件的上部和下部转移平面（10,11）。两个成角度的上下平面（8,9）和两个成角度的边缘部件的上下传输平面（10,11）基本上平行配对并且分别以大约90°的角度相互取向。本发明还涉及这种负载接口（1）的应用。

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