Invention Grant
US09302851B2 Fastening device for releasably fastening a mechanism in the region of a floor of an aircraft or space craft and arrangement for a cargo loading system
有权
紧固装置,用于可释放地将机构紧固在飞机的地板区域或用于货物装载系统的航天器和装置的区域中
- Patent Title: Fastening device for releasably fastening a mechanism in the region of a floor of an aircraft or space craft and arrangement for a cargo loading system
- Patent Title (中): 紧固装置,用于可释放地将机构紧固在飞机的地板区域或用于货物装载系统的航天器和装置的区域中
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Application No.: US14163343Application Date: 2014-01-24
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Publication No.: US09302851B2Publication Date: 2016-04-05
- Inventor: Markus Esser , Ali Lohmann , Jörg Pump , Sönke Hager , Johannes Völker
- Applicant: AIRBUS OPERATIONS GMBH
- Applicant Address: DE Hamburg
- Assignee: Airbus Operations GmbH
- Current Assignee: Airbus Operations GmbH
- Current Assignee Address: DE Hamburg
- Agency: Jenkins, Wilson, Taylor & Hunt, P.A.
- Priority: DE102013201120 20130124
- Main IPC: B65G13/11
- IPC: B65G13/11 ; B65G39/12 ; B65G21/02 ; B65G21/06 ; B60R11/00 ; B64C1/20 ; B65G13/00 ; F16B21/02 ; B64D9/00

Abstract:
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.
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