Patent · US Active

Aircraft conduit harness retention system

US8888053B2 · kind B2 · utility

6Cited by
14References
3Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 14, 2011
Grant dateNov 18, 2014
Priority date
Expiry dateSep 18, 2031

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16L3/237
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A conduit harness retention system has a base, a first spacer, a second spacer and a cap which snap-fit together to retain P-clip harnesses in position spaced from an aircraft fuselage.

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