Patent · US Active

Aircraft fuel pipe coupling

US8172272B2 · kind B2 · utility

15Cited by
12References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 6, 2006
Grant dateMay 8, 2012
Priority date
Expiry dateOct 3, 2027

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16L2201/30
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A coupling for fuel pipe includes a pipe end fitting, which includes a male outer surface including a groove and a female inner surface including a groove. The coupling includes a double-walled socket including a female outer socket and a male inner shaft. The pipe end fitting is accommodated in the region between the female outer socket and the male inner shaft. A first seal ring seals between the female inner surface and the male inner shaft. A second seal ring, which may be substantially coplanar with the first, seals between the male outer surface and the female outer socket of the double-walled socket. The coupling may be so arranged that the pipe end fitting and the double-walled socket are able to pivot relative to each other by up to at least ±2 degrees and are able to slide both towards and apart from each other.

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