公开(公告)号：US20140064827A1

公开(公告)日：2014-03-06

申请号：US14015057

申请日：2013-08-30

Applicant: Driessen Aerospace Group N.V.

Inventor： Maarten Michiel Korenromp ,  Remko Schiphorst

IPC: B64D11/00 ,  F16B2/06

CPC classification number: B64D11/00 ,  F16B2/06 ,  Y10T403/32091

Abstract: The invention relates to a locking assembly for locking an aircraft interior structure (13) to an internal mounting frame (2) comprising: a sliding element (1) which is suitable for insertion in the internal mounting frame (2), a height adjustment assembly, comprising a lower and an upper height adjustment part (4, 5). The assembly further comprises a fitting (6) attachable to the aircraft interior structure, having a recess wherein a projection (19) of the upper height adjustment part (5) is received, wherein the fitting (6) can be moved with respect to the projection (19) in a plane defined by Xr- and Yr-directions. Further provided is a locking bolt (11) received in the upper height adjustment part (5) for locking the fixation element (9), the fitting (6), and the height adjustment parts (4, 5) to the sliding element (1).

Abstract translation: 本发明涉及一种用于将飞行器内部结构（13）锁定到内部安装框架（2）的锁定组件，包括：适于插入内部安装框架（2）中的滑动元件（1），高度调节组件 ，包括下部和上部高度调节部分（4,5）。 组件还包括可附接到飞行器内部结构的配件（6），具有凹部，其中容纳上部高度调节部分（5）的突起（19），其中，所述配件（6）能够相对于 突起（19）在由Xr和Yr方向限定的平面内。 还提供了一种容纳在上部高度调节部分（5）中的锁定螺栓（11），用于将固定元件（9），配件（6）和高度调节部件（4,5）锁定到滑动元件（1） ）。