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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.

Patent No.:

US 12162600 B1

PDFFull Text
Date of Patent:
Dec. 10, 2024

Filed:

May. 13, 2020

Aircraft panel assembly

Applicants:

Airbus Operations Limited, Bristol, GB;

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Chris Heaysman, Bristol, GB;

John Martin Gaitonde, Bristol, GB;

Hauke Seegel, Hamburg, DE;

Assignees:

AIRBUS OPERATIONS LIMITED, Bristol, GB;

AIRBUS OPERATIONS GmbH, Hamburg, DE;

Attorney:

Nixon & Vanderhye P.C.

Primary Examiner:

Michael H Wang

Int. Cl.
CPC ...
B64C 3/18 (2006.01); B64C 1/00 (2006.01); B64C 1/06 (2006.01); B64C 3/20 (2006.01); B64C 3/26 (2006.01); B64C 3/34 (2006.01); B64F 5/10 (2017.01); B29C 70/42 (2006.01); B29C 70/84 (2006.01); B29D 99/00 (2010.01);
U.S. Cl.
CPC ...
B64C 3/182 (2013.01); B64C 1/00 (2013.01); B64C 1/06 (2013.01); B64C 1/061 (2013.01); B64C 1/064 (2013.01); B64C 1/065 (2013.01); B64C 3/187 (2013.01); B64C 3/20 (2013.01); B64C 3/26 (2013.01); B64C 3/34 (2013.01); B64F 5/10 (2017.01); B29C 70/42 (2013.01); B29C 70/84 (2013.01); B29D 99/0014 (2013.01);
Abstract

An aircraft panel assembly with a panel and a plurality of stiffeners on the panel is disclosed. Each stiffener has an attachment part attached to the panel and a structural part spaced apart from the panel. A rib foot beam crosses the stiffeners at a series of intersections. At each intersection the rib foot beam is located between the panel and the structural part of a respective one of the stiffeners.

Find Patent Forward Citations

Heaysman, Chris. (2024). Aircraft panel assembly (U.S. Patent No. 12162600). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12162600

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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