FIELD: motors and pumps.
SUBSTANCE: invention can be used in fuel systems of internal combustion engines (ICE). Proposed fuel feed device comprises housing 14 of fuel tank, including several fuel compartments, device to feed fuel from fuel tank housing 14 including feed pipe 44 extending outward from the main fuel compartment 38M and fuel pump 42. There is also return pipe 64, discharge part of the fuel passing through fuel pump 42 into auxiliary fuel compartment 38S and channel 52 for fuel transfer supplying fuel from compartment 38S into compartment 38M. There is a connecting part, connecting channel 52 with return pipe 64 so that portion of fluid from channel 52 can move in return pipe 64.
EFFECT: technical result consists in reduction of dimensions of fuel pump and reduction of power consumption.
6 cl, 19 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF EQUALISING FUEL CAPACITY IN AIRCRAFT WING TANKS IN OPERATION ON SURFACE | 2009 |
|
RU2435705C2 |
METHOD FOR BALANCING FUEL RESERVE IN AIRCRAFT WING TANKS DURING GROUND OPERATION (VERSIONS) | 2009 |
|
RU2403179C1 |
METHOD OF EQUALISING FUEL CAPACITY IN AIRCRAFT WING TANKS IN OPERATION ON SURFACE | 2009 |
|
RU2438928C2 |
METHOD OF FUEL RESERVE BALANCING IN AIRPLANE WING TANKS DURING GROUND OPERATIONS (VERSIONS) | 2009 |
|
RU2435706C2 |
REFUELLING TRUCK | 1997 |
|
RU2113367C1 |
0 |
|
SU312784A1 | |
PLANE FUEL SYSTEM | 2006 |
|
RU2323857C1 |
AIRPLANE FUEL SYSTEM | 2007 |
|
RU2356800C1 |
SYSTEM AND PROCESS FOR RUNNING ON EMULSIFIED FUEL | 2010 |
|
RU2559091C2 |
FUEL STORAGE DEVICE | 1998 |
|
RU2181326C2 |
Authors
Dates
2016-04-27—Published
2012-02-02—Filed