Patent · US Active

Rear mount for an aircraft engine

US10464686B2 · kind B2 · utility

0Cited by
2References
5Claims
0Family size

Assignee

Inventor

Key dates

Filing dateAug 23, 2017
Grant dateNov 5, 2019
Priority date—
Expiry dateJul 26, 2038

Classification

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

Abstract

A rear engine mount for a turbomachine of an aircraft comprising a pylon. The rear engine mount comprises a beam attached to the pylon, a first and a second lateral connecting rod having an abutment and attached between the beam and the turbomachine, a three-point, V-shaped central connecting rod, of which the vertex is attached to the turbomachine, and of which the ends of the arms are attached to the beam. The rear engine mount has a plane of symmetry passing through the center of the ball joint of the vertex. The beam has, for each abutment, a buffer, wherein each abutment comes to bear against the buffer in the event of failure of the central connecting rod.

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