Patent · US Active

Rod connection system, structural aircraft component and connector stud

US10465378B2 · kind B2 · utility

1Cited by
5References
8Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 29, 2016
Grant dateNov 5, 2019
Priority date
Expiry dateDec 13, 2037

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/40
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A rod connection system includes a first structural member having an angled pin connector integrally formed at an end portion of the first structural member with angled pins being spaced apart from and protruding parallel to an end face of the first structural member. The rod connection system further includes a second structural member having an angled socket connector integrally formed at an end portion of the second structural member with angled tubes as sockets for the angled pins of the first structural member. The angled tubes are spaced apart from and protruding parallel to an end face of the second structural member.

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