FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft fuel tank. Proposed fuel tank suppresses electrostatic charge originating due to electrisation by fuel flow. Fuel comprises electrically conducting top lining 5 and bottom lining 7 that make fuel container, metallic inner structures 19 and inner surface layer 15 having the semiconductor or insulator properties and made integral with inner surfaces of said top and bottom linings 5, 7 at their joint with inner structure 19 and nearby sections wherein inner surface layer is made of semiconductor material on least adjacent section.
EFFECT: ruled out electrochemical corrosion.
2 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
TANK OF COMPOSITE, WING AND METHOD OF MAKING SAID TANK | 2010 |
|
RU2493085C2 |
CAPACITANCE-TYPE LEVEL GAUGE | 2011 |
|
RU2539739C2 |
STRUCTURAL MATERIAL FOR MAKING STRUCTURAL ELEMENTS, FUEL TANK, MAIN WING AND AIRCRAFT | 2013 |
|
RU2605716C2 |
FUEL TANK, MAIN WING, AIRCRAFT FUSELAGE, AIRCRAFT AND MOVING BODY | 2013 |
|
RU2581104C1 |
CAP, FASTENING STRUCTURE USING THIS CAP, AND AIRCRAFT COMPRISING FASTENING STRUCTURE | 2011 |
|
RU2531113C2 |
FUEL TANK, MAIN WINGS, AIR FRAME, AIRCRAFT AND VEHICLE | 2014 |
|
RU2628291C2 |
AIRCRAFT WIRING CONNECTOR ASSEMBLY | 2007 |
|
RU2424951C2 |
FUEL TANK, MAIN WINGS, AIRCRAFT BODY, FLYING VEHICLE AND VEHICLE | 2014 |
|
RU2641404C2 |
WING WITH SUPERSONIC FREE LAMINAR FLOW (VERSIONS) AND WING SURFACE LAMINAR FLOW CONTROL SYSTEM | 1994 |
|
RU2133692C1 |
AIRFOIL, AIRCRAFT AND METHOD FOR MANUFACTURE THEREOF | 2014 |
|
RU2667657C2 |
Authors
Dates
2013-09-10—Published
2010-03-26—Filed