Patent · US Active

Suspension assembly for an aircraft turbojet engine

US8985508B2 · kind B2 · utility

1Cited by

6References

9Claims

0Family size

Assignee

AIRCELLE · FR

Inventors

Pierre Caruel · Moissy-Cramayel, FR
Guy Bernard Vauchel · Le Havre, FR

Key dates

Filing date	Jan 21, 2010
Grant date	Mar 24, 2015
Priority date	—
Expiry date	Feb 21, 2032

Classification

Technology area (CPC Y)Emerging Cross-Sectional Technologies
CPC primaryY02T50/40
WIPO fieldTransport
WIPO sectorMechanical engineering

Abstract

A suspension assembly for an aircraft turbojet engine includes a pylon and connecting rods for taking up the thrust of the turbojet engine which is connected to the pylon. In particular, the suspension assembly includes an insulator which is separate from the pylon and thermally insulates the connecting rods from the turbojet engine.

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