FIELD: air transport.
SUBSTANCE: hull includes outer skin which is flexible material containing composite material and metal material. Composite material is made from carbon fibres and/or glass fibres, and/or ceramic fibres, or from carbon fibres coated with the material with nitride or carbon connection, and/or metal or ceramic material in which there built are carbon fibres, and represents fireproof material. Metal material consists of aluminium or titanium, aluminium and titanium alloy. Composite material and metal material are covered with resin layer or submerged into resin in order to obtain hybrid material. Outer skin has sandwich design in which composite material and metal material are adhesively connected.
EFFECT: increasing fire safety.
11 cl, 2 dwg
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|
RU2413651C2 |
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| METHOD OF JOINTING, AT LEAST, TWO METAL SHEETS TOGETHER AND ITS APPLICATION FOR MAKING LIGHT-WEIGHT STRUCTURE | 2006 |
|
RU2418665C2 |
| CIRCUMFERENTIAL BUTT JOINT FOR SKIN STRUCTURES | 2013 |
|
RU2658211C2 |
| STRUCTURE MADE OF COMPOSITE MATERIALS, AIRCRAFT MAIN WING AND BODY CONTAINING SAID STRUCTURE | 2010 |
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RU2518927C2 |
