FIELD: aircraft engineering.
SUBSTANCE: fuel tank comprises the plastic structural element reinforced with the carbon fibre. Said reinforcing material contains the carbon fibres while the matrix comprises the plastic. Said matrix features electric conductivity. Structural element surface cut thereat is exposed to the fuel tank inner part of fuel tank. The main wing, aircraft fuselage, aircraft and moving body include the fuel tank of aforesaid design.
EFFECT: decreased weight, labour input and production costs.
6 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| STRUCTURAL MATERIAL FOR MAKING STRUCTURAL ELEMENTS, FUEL TANK, MAIN WING AND AIRCRAFT | 2013 |
|
RU2605716C2 |
| FUEL TANK, MAIN WINGS, AIR FRAME, AIRCRAFT AND VEHICLE | 2014 |
|
RU2628291C2 |
| FUEL TANK, MAIN WINGS, AIRCRAFT BODY, FLYING VEHICLE AND VEHICLE | 2014 |
|
RU2641404C2 |
| AIRCRAFT FUEL TANK | 2010 |
|
RU2492108C2 |
| STRUCTURE OF COMPOSITE AND AIRCRAFT WING AND FUSELAGE EQUIPPED WITH SAID STRUCTURE | 2012 |
|
RU2553608C2 |
| TANK OF COMPOSITE, WING AND METHOD OF MAKING SAID TANK | 2010 |
|
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| STRUCTURE MADE OF COMPOSITE MATERIALS, AIRCRAFT MAIN WING AND BODY CONTAINING SAID STRUCTURE | 2010 |
|
RU2518927C2 |
| AIRCRAFT ASSEMBLY | 2009 |
|
RU2448875C2 |
| AIRBORNE VEHICLE WING AND AIRBORNE VEHICLE'S FLIGHT METHOD | 2017 |
|
RU2745876C2 |
| AIRCRAFT JUNCTION AND STRUCTURE | 2014 |
|
RU2636373C2 |
