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:
Dec. 24, 2024

Filed:

Mar. 31, 2021
Applicant:

Kawasaki Jukogyo Kabushiki Kaisha, Kobe, JP;

Inventors:

Naoki Shimada, Nagoya, JP;

Yoshihiro Nakayama, Konan, JP;

Sayaka Ochi, Kakamigahara, JP;

Kenshirou Okumura, Kani, JP;

Shouhei Kanazawa, Kakamigahara, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B32B 3/30 (2006.01); B29C 70/44 (2006.01); B29C 70/46 (2006.01); B29C 70/54 (2006.01); B29K 101/10 (2006.01); B29K 307/04 (2006.01); B29L 31/30 (2006.01); B32B 3/26 (2006.01); B32B 5/02 (2006.01); B32B 5/26 (2006.01); B64C 1/00 (2006.01); B64C 1/06 (2006.01); B64F 5/10 (2017.01);
U.S. Cl.
CPC ...
B29C 70/44 (2013.01); B29C 70/46 (2013.01); B29C 70/465 (2013.01); B29C 70/54 (2013.01); B32B 3/26 (2013.01); B32B 3/263 (2013.01); B32B 3/266 (2013.01); B32B 3/30 (2013.01); B32B 5/02 (2013.01); B32B 5/26 (2013.01); B64C 1/064 (2013.01); B64F 5/10 (2017.01); B29K 2101/10 (2013.01); B29K 2307/04 (2013.01); B29L 2031/3076 (2013.01); B32B 2260/023 (2013.01); B32B 2260/046 (2013.01); B32B 2262/106 (2013.01); B32B 2605/18 (2013.01); B64C 2001/0072 (2013.01);
Abstract

An aircraft structure (such as a T-shaped structure, a convex structure, a curved structure, or the like) includes: a laminated structure including composite-material layers that are laminated; and wherein the composite material aircraft structure is a three-dimensional structure that includes at least one of a standing structure, a convex structure, or a curved structure. The composite-material layers include at least a composite-material layer in which a reinforced fiber is a single continuous fiber, wherein the single continuous fiber includes a partial slit region. When a thickness of a flat-plate formed body including a same laminated structure as the aircraft structure but not including the three-dimensional structure, is defined as a reference thickness, the aircraft structure includes a thin plate region which has a thickness that is smaller than the reference thickness while maintaining the laminated structure.


Find Patent Forward Citations

Loading…