公开(公告)号：US07546984B2

公开(公告)日：2009-06-16

申请号：US11187334

申请日：2005-07-22

申请人： Bernd Poppe ,  Kurt Auhagen

发明人： Bernd Poppe ,  Kurt Auhagen

IPC分类号： B64C9/02

CPC分类号： B64C9/04 ,  B64C9/16 ,  B64C13/24

摘要： Described is an interconnection system, in particular for flaps which are located side-by-side, on an aircraft wing, for example landing flaps or high-lift flaps. The interconnection system is in particular characterised in that it comprises a correspondingly guided compensating profile for a gap between the flaps, which gap changes when the flaps are moved. Preferably, the interconnection system is combined with a failsafe device for adjacent flaps in the form of a longitudinally adjustable interconnection strut which is connected to the adjacent flaps by way of corresponding load introduction fittings. The interconnection system is in particular suitable for large aircraft in which the gap between adjacent flaps, due to the relatively large lateral movement of the flaps during retraction and extension, becomes relatively wide, and the forces acting on the flaps are relatively great.

摘要翻译： 描述了一种互连系统，特别是在飞机机翼上并排设置的襟翼，例如落地襟翼或高升襟翼。 互连系统的特征特征在于，其包括用于襟翼之间的间隙的相应引导的补偿轮廓，当襟翼移动时，该间隙变化。 优选地，互连系统与用于相邻翼片的故障保护装置组合，其形式为纵向可调节的互连支柱，其通过相应的负载引入配件连接到相邻的翼片。 互连系统特别适用于大型飞行器，其中相邻翼片之间的间隙由于在缩回和延伸期间襟翼的相对大的横向运动变得相对较宽，并且作用在翼片上的力相对较大。

公开(公告)号：US20060022093A1

公开(公告)日：2006-02-02

申请号：US11187334

申请日：2005-07-22

申请人： Bernd Poppe ,  Kurt Auhagen

发明人： Bernd Poppe ,  Kurt Auhagen

IPC分类号： B64C3/50

CPC分类号： B64C9/04 ,  B64C9/16 ,  B64C13/24

摘要： Described is an interconnection system, in particular for flaps which are located side-by-side, on an aircraft wing, for example landing flaps or high-lift flaps. The interconnection system is in particular characterised in that it comprises a correspondingly guided compensating profile for a gap between the flaps, which gap changes when the flaps are moved. Preferably, the interconnection system is combined with a failsafe device for adjacent flaps in the form of a longitudinally adjustable interconnection strut which is connected to the adjacent flaps by way of corresponding load introduction fittings. The interconnection system is in particular suitable for large aircraft in which the gap between adjacent flaps, due to the relatively large lateral movement of the flaps during retraction and extension, becomes relatively wide, and the forces acting on the flaps are relatively great.