COMPOSITE MATERIAL STRUCTURE, AND AIRCRAFT WING AND FUSELAGE PROVIDED THEREWITH
COMPOSITE MATERIAL STRUCTURE, AND AIRCRAFT WING AND FUSELAGE PROVIDED THEREWITH
- New search for: TANAKA YUYA
- New search for: SUZUKI HIDEYUKI
- New search for: KANAYAMA YUTAKA
- New search for: SATO KAZUKI
- New search for: HATANO MASATAKE
- New search for: SAITO SATORU
- New search for: WATANABE AKIHISA
- New search for: ABE RYO
- New search for: TANAKA YUYA
- New search for: SUZUKI HIDEYUKI
- New search for: KANAYAMA YUTAKA
- New search for: SATO KAZUKI
- New search for: HATANO MASATAKE
- New search for: SAITO SATORU
- New search for: WATANABE AKIHISA
- New search for: ABE RYO
Provided is a composite material structure that reinforces areas around holes against stress concentrations, and also enables weight reduction. A wing (1) has a box structure. A lower outer plate (3) on the wing (1) is provided with: a center section (3b), made of metal, which extends in one direction and in which access holes (5) are formed; and a forward section (3a) and an aft section (3c), both made of fiber reinforced plastic, which extend in the one direction and are respectively connected to both sides of the center section (3b). The metal used for the center section (3b) is preferably a titanium alloy or an aluminum alloy.
Document information
COMPOSITE MATERIAL STRUCTURE, AND AIRCRAFT WING AND FUSELAGE PROVIDED THEREWITH
VERBUNDWERKSTOFFSTRUKTUR SOWIE FLUGZEUGFLÜGEL UND -RUMPF DAMIT
STRUCTURE EN MATÉRIAU COMPOSITE, ET AILE ET FUSELAGE D'AÉRONEF LA COMPORTANT
2019-07-03
Patent
Electronic Resource
English
| IPC: | B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B62D MOTOR VEHICLES , Motorfahrzeuge / B64C AEROPLANES , Flugzeuge |
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