Patent · US Active

Assembly between an aircraft pylon and a turbine engine

US10836500B2 · kind B2 · utility

0Cited by

2References

16Claims

0Family size

Assignee

SAFRAN AIRCRAFT ENGINES · FR

Inventors

Antoine Elie Hellegouarch · Moissy-Cramayel, FR
Marc Patrick Tesniere · Mennecy, FR

Key dates

Filing date	Oct 26, 2017
Grant date	Nov 17, 2020
Priority date	—
Expiry date	Oct 16, 2038

Classification

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

Abstract

An assembly between an aircraft structural pylon and an aircraft turbine engine is disclosed, with the assembly comprising a beam intended to be attached to the turbine engine and wherein a knuckle intended for the installation of a pad integral with the pylon is mounted, with the beam comprising suspension lugs each including a bore for the passage of a shaft intended to further go through a bore formed in the pylon to connect the beam with the pylon.

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