Patent · US Active

Engine attachment system for an aircraft engine

US10934009B2 · kind B2 · utility

0Cited by
1References
6Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 5, 2018
Grant dateMar 2, 2021
Priority date
Expiry dateSep 17, 2039

Classification

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

Abstract

An engine attachment system comprising an engine pylon with a top wall, a bottom wall and two lateral walls, and a front engine attachment with a beam which bears two connecting rods for fixing the engine. The engine attachment system also comprises an intermediate piece with a bottom wall and four lateral walls, wherein the beam is fixed against an outer face of the bottom wall, wherein the intermediate piece is fitted at a front-end face of the engine pylon in such a way that an inner face of the bottom wall comes against the front-end face of the engine pylon, and in such a way that the lateral walls of the intermediate piece are superposed with the walls of the engine pylon. In such an engine attachment system, the front engine attachment is thus located on the front-end face of the engine pylon, allowing a space saving.

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