Patent · US Active

Aircraft engine assembly comprising rear engine attachments in the form of shackles

US10189575B2 · kind B2 · utility

1Cited by
1References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 21, 2016
Grant dateJan 29, 2019
Priority date
Expiry dateSep 16, 2037

Classification

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

Abstract

An aircraft engine assembly including a set of rear engine attachments comprising a first shackle hinged on a bracket secured to the engine and on a bracket made as one piece with one of the two side panels, the shackle being oriented along a vertical direction, a second shackle hinged on a bracket secured to the engine and on a bracket made as one piece with the other one of the two side panels, the second shackle being oriented along the vertical direction, and a third shackle for transversally transmitting loads, inclined relative to the vertical direction and hinged on a bracket secured to the engine and on a bracket secured to the primary structure.

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