Patent · US Active

Aircraft joint

US10730605B2 · kind B2 · utility

1Cited by
1References
17Claims
0Family size

Assignee

Inventor

Key dates

Filing dateMay 11, 2017
Grant dateAug 4, 2020
Priority date
Expiry dateMay 8, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16B11/006
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft joint includes a first component having an outer aerodynamic surface and an inner surface, a second component having an outer aerodynamic surface and an inner surface, and a strap assembly bridging between the inner surfaces of the first and second components. The strap assembly has a first strap part attached to the inner surface of the first component, a second strap part attached to the inner surface of the second component, and a third strap part received in the first and second strap parts in a sliding manner. The third strap part when received in the first and second strap parts constrains movement of the first component relative to the second component in a direction normal to the outer aerodynamic surfaces of the first and second components in the vicinity of the strap assembly.

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