Patent · US Active

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

US10071796B2 · kind B2 · utility

2Cited by
12References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 4, 2016
Grant dateSep 11, 2018
Priority date
Expiry dateAug 23, 2036

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D2009/006
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.