FIELD: aviation.
SUBSTANCE: fuel tank comprises a structural element using carbon fibre reinforced plastic (CFRP) (15) including reinforcing material containing carbon fibre and matrix that contains plastic. The structural element is formed by rolling conducting sheets (17) between prepreg sheets from reinforced carbon fibre reinforced plastic (CFRP) (15) and formed with a fastening hole (22), in which the bolt is fixed.
EFFECT: necessity for application of sealant is eliminated, reduced labour input and reduced costs associated with quality control, prevention of weight gain.
6 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FUEL TANK, MAIN WINGS, AIR FRAME, AIRCRAFT AND VEHICLE | 2014 |
|
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| AIRBORNE VEHICLE WING AND AIRBORNE VEHICLE'S FLIGHT METHOD | 2017 |
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| AIRCRAFT FUEL TANK | 2010 |
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| CAP, FASTENING STRUCTURE USING THIS CAP, AND AIRCRAFT COMPRISING FASTENING STRUCTURE | 2011 |
|
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| STRUCTURE MADE OF COMPOSITE MATERIALS, AIRCRAFT MAIN WING AND BODY CONTAINING SAID STRUCTURE | 2010 |
|
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| CONSTRUCTION FROM PLASTIC, REINFORCED WITH CARBON FIBRE, AND METHOD OF THEREOF PRODUCTION | 2012 |
|
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| STRUCTURE OF COMPOSITE AND AIRCRAFT WING AND FUSELAGE EQUIPPED WITH SAID STRUCTURE | 2012 |
|
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