The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 07, 2023

Filed:

Jul. 14, 2021
Applicant:

Airbus Operations Sas, Toulouse, FR;

Inventors:

Germain Gueneau, Toulouse, FR;

Michael Berjot, Toulouse, FR;

Olivier Pautis, Toulouse, FR;

Assignee:

AIRBUS OPERATIONS SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); B64C 3/32 (2006.01); B64D 27/16 (2006.01); B64C 3/18 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64C 3/185 (2013.01); B64C 3/187 (2013.01); B64C 3/32 (2013.01); B64D 27/16 (2013.01); B64D 2027/264 (2013.01);
Abstract

An assembly for an aircraft that has a wing and an engine pylon having a primary structure with right-side and left-side panels, an upper and a lower spar and a rear rib, two sets of upper or lower shackles, one set fastening the right-side panel to the wing, and a second set fastening the left-side panel to the wing, a fastening element secured to the rear rib or to the lower spar, a rear rod connecting the fastening element to the wing, a transverse shackle connecting the upper spar to the wing, a line connecting two centers of the transverse shackle being oriented transversely relative to a longitudinal axis of the engine pylon, and a reinforcing panel, at each joint between a right-side or left-side panel and an upper or lower shackle, which is fastened along a height against the panel and to which the shackle is also fastened.


Find Patent Forward Citations

Loading…