FIELD: manufacture of aircraft; devices feeding fuel to power plant, namely to helicopter fuel systems. SUBSTANCE: transfer system is provided with additional overflow main whose pipe lines connect top points of additional tanks with above-fuel cavity of main tank whose top point is connected with vent pipe line. Part of pipe lines of overflow main which are used for interconnecting the additional tanks are located above pipe line of overflow main connecting the additional tanks of second sequence of fuel usage with main tank. EFFECT: enhanced efficiency. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
FLYING VEHICLE FUEL SYSTEM | 1992 |
|
RU2028969C1 |
HELICOPTER FUEL SYSTEM | 1992 |
|
RU2027641C1 |
HELICOPTER | 1993 |
|
RU2102285C1 |
NECK FOR TOP FILLING OF TANK WITH FUEL | 1992 |
|
RU2039681C1 |
FUEL TRANSFER SYSTEM | 0 |
|
SU593405A1 |
FLEXIBLE PIPE LINE | 1995 |
|
RU2097643C1 |
SYSTEM FOR CONTROL OF FUEL CONSUMPTION IN AIRCRAFT | 0 |
|
SU927645A2 |
FUEL FEED SYSTEM | 0 |
|
SU854807A1 |
AIRCRAFT FUEL SYSTEM | 1996 |
|
RU2134216C1 |
FLYING VEHICLE FUEL-FEED SYSTEM | 0 |
|
SU626535A1 |
Authors
Dates
1997-06-20—Published
1994-07-01—Filed