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:
Jul. 10, 2012

Filed:

Sep. 12, 2008
Applicants:

Helene Cazeneuve, Plaisance du Touch, FR;

Bruno Cacciaguerra, Les Nolles, FR;

Jean-claude Lacombe, Blagnac, FR;

David Andissac, Toulouse, FR;

Inventors:

Helene Cazeneuve, Plaisance du Touch, FR;

Bruno Cacciaguerra, Les Nolles, FR;

Jean-Claude Lacombe, Blagnac, FR;

David Andissac, Toulouse, FR;

Assignee:

Airbus Operations SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 1/06 (2006.01);
U.S. Cl.
CPC ...
Abstract

An aircraft structure including stiffened panels assembled at the junction, without continuity of the stiffeners. Multiple panels are used to form the fuselage, tail units and wings of an aircraft. These panels include stiffeners which are interrupted at each panel junction. However, the stresses experienced by the stiffeners must be transmitted despite these interruptions. Known solutions require the use of at least one additional part per stiffener and per interruption. In order to solve this problem, the disclosed embodiments include a doubler necessitating at most one additional part per panel junction area for all of the interrupted stiffeners in this area.


Find Patent Forward Citations

Loading…