Patent · US Active

Rear engine attachment for an aircraft engine

US10647441B2 · kind B2 · utility

0Cited by
8References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 16, 2018
Grant dateMay 12, 2020
Priority date
Expiry dateNov 16, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2240/90
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A rear engine attachment for an engine of an aircraft which comprises a pylon having a bottom face, the rear engine attachment comprising a first fitting configured to be fixed against the bottom face and having a wall, a second fitting configured to be secured to a structural casing of the engine, two front links and two rear links, which are fixed by one and the same main link point to the wall and by two link points on either side of the second fitting. Such a motorization assembly allows for a reduction of the bulk, in particular at the rear engine attachment, which helps in improving the overall performance of the motorization assembly.

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