公开(公告)号：US20160214703A1

公开(公告)日：2016-07-28

申请号：US15089909

申请日：2016-04-04

申请人： AIRBUS OPERATIONS GMBH

发明人： Markus ESSER ,  Ali LOHMANN ,  Jörg PUMP ,  Sönke HAGER ,  Johannes VÖLKER

IPC分类号： B64C1/20 ,  B64G1/22

CPC分类号： B64C1/20 ,  B60R11/00 ,  B64D9/00 ,  B64D9/003 ,  B64D2009/006 ,  B64G1/22 ,  B65G13/00 ,  B65G13/11 ,  B65G21/02 ,  B65G21/06 ,  B65G39/12 ,  F16B21/02

摘要： A fastening device is disclosed for releasably fastening a mechanism in the region of a floor of an aircraft or spacecraft and includes a base component and a latch component. The latch component includes at least one holding portion including a latch-component-side holding face and is movably coupled to the base component between an unlocked and a locked position. When positioned in a predefined mounting position on the floor component and/or on the base component, the holding portion of the latch component engages a fastening portion, and the latch-component-side holding face faces the mechanism-side holding face. During passage of the latch component from locked position into unlocked position a gap between the latch-component-side holding face and the mechanism-side holding face continuously widens. The invention further relates to an arrangement for a cargo loading system.

摘要翻译： 公开了一种紧固装置，用于将机构可释放地紧固在飞行器或航天器的地板区域中并且包括基座部件和闩锁部件。 闩锁部件包括至少一个包括闩锁部件侧保持面的保持部分，并且在解锁和锁定位置之间可移动地联接到基部部件。 当位于地板部件和/或基部部件上的预定安装位置时，闩锁部件的保持部分接合紧固部分，并且闩锁部件侧保持面面向机构侧保持面。 在闩锁部件从锁定位置通过到解锁位置时，闩锁部件侧保持面和机构侧保持面之间的间隙持续变宽。 本发明还涉及一种用于货物装载系统的装置。

公开(公告)号：US20140202824A1

公开(公告)日：2014-07-24

申请号：US14163343

申请日：2014-01-24

申请人： AIRBUS OPERATIONS GMBH

发明人： Markus ESSER ,  Ali Lohmann ,  Jörg Pump ,  Sönke Hager ,  Johannes Völker

IPC分类号： B60R11/00 ,  B64C1/20 ,  B65G13/00 ,  B64D9/00

CPC分类号： B64C1/20 ,  B60R11/00 ,  B64D9/00 ,  B64D9/003 ,  B64D2009/006 ,  B64G1/22 ,  B65G13/00 ,  B65G13/11 ,  B65G21/02 ,  B65G21/06 ,  B65G39/12 ,  F16B21/02

摘要： A fastening device is disclosed for releasably fastening a mechanism in the region of a floor of an aircraft or spacecraft and includes a base component and a latch component. The latch component includes at least one holding portion including a latch-component-side holding face and is movably coupled to the base component between an unlocked and a locked position. When positioned in a predefined mounting position on the floor component and/or on the base component, the holding portion of the latch component engages a fastening portion, and the latch-component-side holding face faces the mechanism-side holding face. During passage of the latch component from locked position into unlocked position a gap between the latch-component-side holding face and the mechanism-side holding face continuously widens. The invention further relates to an arrangement for a cargo loading system.

摘要翻译： 公开了一种紧固装置，用于将机构可释放地紧固在飞行器或航天器的地板区域中并且包括基座部件和闩锁部件。 闩锁部件包括至少一个包括闩锁部件侧保持面的保持部分，并且在解锁和锁定位置之间可移动地联接到基部部件。 当位于地板部件和/或基部部件上的预定安装位置时，闩锁部件的保持部分接合紧固部分，并且闩锁部件侧保持面面向机构侧保持面。 在闩锁部件从锁定位置通过到解锁位置时，闩锁部件侧保持面和机构侧保持面之间的间隙持续变宽。 本发明还涉及一种用于货物装载系统的装置。