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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 11939038 B1

PDFFull Text
Date of Patent:
Mar. 26, 2024

Filed:

Jun. 25, 2020

Fuselage structure of an aircraft and method for manufacturing the same

Applicant:

Kok & Van Engelen Composite Structures B.v., The Hague, NL;

Inventor:

Maarten Labordus, Delft, NL;

Assignee:

KOK & VAN ENGELEN COMPOSITE STRUCTURES B.V., The Hague, NL;

Attorney:

KDW Firm PLLC

Primary Examiner:

Joseph W Sanderson

Int. Cl.
CPC ...
B64C 1/12 (2006.01); B29C 65/36 (2006.01); B29D 99/00 (2010.01); B29L 31/30 (2006.01); B64C 1/06 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/12 (2013.01); B29C 65/3636 (2013.01); B29C 65/3684 (2013.01); B29D 99/0014 (2013.01); B64C 1/061 (2013.01); B64C 1/064 (2013.01); B64C 1/069 (2013.01); B29L 2031/3082 (2013.01); B64C 2001/0072 (2013.01);
Abstract

A fuselage structure of an aircraft includes a fuselage skin, and a plurality of frame elements spaced apart from one another in a direction parallel to the aircraft longitudinal axis for supporting the fuselage skin. The fuselage skin includes a plurality of interconnected fiber-reinforced composite skin panels that extend between each pair of frame elements and are connected thereto. The composite skin panels further comprise a stiffener integrally formed in each composite skin panel. A method for manufacturing the fuselage skin. The composite skin panels may be interconnected and/or connected to a frame element through an induction welded connection.

Find Patent Forward Citations

Quick Actions:

Labordus, Maarten. (2024). Fuselage structure of an aircraft and method for manufacturing the same (U.S. Patent No. 11939038). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11939038

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

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