FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to system and method of water removal from aircraft fuel tanks. Fuel system comprises fuel line, fuel pump with its inlet communicated with fuel tank and outlet communicated with fuel line. Fuel system comprises also water removal system provided with water discharge opening to remove water from fuel tank and outlet opening communicated with fuel line, parallel with fuel pup. In water removal from fuel tank, water is forced into fuel line downstream of fuel pump and fed from fuel line into engine.
EFFECT: higher efficiency.
12 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| WATER REMOVAL SYSTEM | 2007 |
|
RU2446995C2 |
| WATER REMOVAL SYSTEM | 2008 |
|
RU2494930C2 |
| WATER REMOVAL SYSTEM | 2008 |
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RU2475422C2 |
| PROPORTIONER | 1980 |
|
SU900540A1 |
| AIRCRAFT EQUIPPED WITH FUEL SUPPLY ASSEMBLY FOR SYSTEM OF FUEL ELEMENTS | 2007 |
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| FLYING VEHICLE FUEL SYSTEM WITH FLIGHT REFUELLING | 1991 |
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SU1798986A1 |
| FUEL SUPPLY SYSTEM FOR INTERNAL COMBUSTION ENGINE | 1992 |
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| METHOD OF FUEL RESERVE BALANCING IN AIRPLANE WING TANKS DURING GROUND OPERATIONS (VERSIONS) | 2009 |
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| METHOD OF PRODUCING FUEL-AIR MIX AND DEVICE TO THIS END (VERSIONS) | 2008 |
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| REFUELLER WITH VACUUM OPERATION | 2008 |
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RU2380293C1 |
