Composite-material aircraft part and method of manufacturing same
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United States of America
Stats
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Dec 24, 2024
Grant Date -
Jul 29, 2021
app pub date -
Mar 31, 2021
filing date -
Mar 31, 2021
priority date (Note) -
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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.

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- 15 United States
- 10 France
- 8 Japan
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- 5 Korea
- 2 Other
Patent Owner(s)
Patent Owner | Address | |
---|---|---|
KAWASAKI JUKOGYO KABUSHIKI KAISHA | KOBE-SHI HYOGO 650-8670 |
International Classification(s)
- B29C:SHAPING OR JOINING OF PLASTICS; SHAPING OF SUBSTAN....
- B64F:GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS
- B29K:INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, ....
- B29L:INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RE....
- B64C:AEROPLANES; HELICOPTERS
- B32B:LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA....

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- [Patents Count]
Inventor(s)
Inventor Name | Address | # of filed Patents | Total Citations |
---|---|---|---|
Kanazawa, Shouhei | Kakamigahara, JP | 4 | 1 |
Nakayama, Yoshihiro | Konan, JP | 33 | 178 |
Ochi, Sayaka | Kakamigahara, JP | 5 | 1 |
Okumura, Kenshirou | Kani, JP | 7 | 1 |
Shimada, Naoki | Nagoya, JP | 84 | 1187 |
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