Patent · US Active

Engine mount for an aircraft, to be placed between an engine and an engine mounting structure

US8740136B2 · kind B2 · utility

13Cited by
9References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 27, 2006
Grant dateJun 3, 2014
Priority date
Expiry dateDec 1, 2030

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16C2326/43
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

An aircraft engine attachment configured to be inserted between an engine and an EMS, the attachment including a plate assembly connected to a first fixing device including an end fitting with two arms and a pin passing through the plate assembly and the two arms, in each of which an orifice is formed including a first ring and a second ring respectively holding the pin. The first ring includes a bottom acting as a stop for a first end of the pin, and the first attachment device includes a mechanism to stop the pin in translation cooperating with a second end of the pin.

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