Patent · US Active

Coupling for joining two frame segments

US8356771B2 · kind B2 · utility

2Cited by
2References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 8, 2009
Grant dateJan 22, 2013
Priority date
Expiry dateOct 5, 2030

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C1/12
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

The invention relates to a coupling for joining two frame segments within a fuselage cabin structure of an aircraft. The frame segments may comprise a Z-shaped or I-shaped cross-sectional geometry, optionally including a recess. Towards the top and the bottom, respectively, the frame segments are equipped with a header flange and a footer flange. According to the invention, at least one side plate is arranged in the area of one side of the web, and at least one counter plate is fitted in the area of an opposing side of the web. Because of the side plates and counter plates butted and riveted symmetrically on both sides against the webs of the frame segments to be joined, the coupling is moment-free and can be configured in a weight-optimized way. For further increase of rigidity, the header flanges may additionally be riveted with the side plates and/or counter plates.

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