Patent · US Active

Front structure of an aircraft fuselage comprising landing gear

US8840063B2 · kind B2 · utility

4Cited by

7References

14Claims

0Family size

Assignee

AIRBUS OPERATIONS SAS · FR

Inventors

Patrick Lieven · Fronton, FR
Pascal Chaumel · Plaisance-du-Touch, FR

Key dates

Filing date	Nov 29, 2012
Grant date	Sep 23, 2014
Priority date	—
Expiry date	Dec 11, 2032

Classification

Technology area (CPC B)Performing Operations; Transporting
CPC primaryB64C25/14
WIPO fieldTransport
WIPO sectorMechanical engineering

Abstract

A front structure of an aircraft fuselage comprising landing gear pivoting about a main shaft and a stay shaft. The front structure also comprises a first reinforcing frame and a second reinforcing frame, the main shaft and the stay shaft being respectively connected to the first and second frames, and a device for the mechanical connection and transfer of forces connecting the stay shaft and the main shaft and transferring to the main shaft a portion of the forces induced by the wheels of the landing gear onto the stay shaft, the second frame and said device being perpendicular to one another.

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