Patent · US Active

Assembly of a pylon with a wing of an aircraft

US11618579B2 · kind B2 · utility

0Cited by
2References
4Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 29, 2021
Grant dateApr 4, 2023
Priority date
Expiry dateOct 29, 2041

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D27/406
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An assembly of a pylon and of a wing of an aircraft, the pylon including a primary structure with a rear face and an upper spar. The assembly includes a rear fastening system including a pair of vertical shackles articulated between the rear face of the primary structure and a first shoe fastened to the wing, wherein the shackles are fastened to the primary structure by a clevis-type connection, and a pair of transverse shackles articulated between the rear face of the primary structure and a second shoe fastened to the wing, wherein the shackles are fastened to the primary structure by a clevis-type connection. With such an assembly, the bulk of the rear fastening system is reduced.

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