FIELD: aeronautical engineering.
SUBSTANCE: proposed method includes continuous prevention of reduction of volume of working fluid through untight sections of system. Volume of working fluid is made up by continuous delivery of fuel to suction line of hydraulic system from fuel system of flying vehicle. Fuel at preset parameters of consumption and pressure is fed from active fuel line of flying vehicle fuel system. Delivery of fuel to suction main of hydraulic system is under constant control.
EFFECT: enhanced survivability of flying vehicle; avoidance of leakage of working fluid through untight sections.
3 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
A FLYING VEHICLE'S CONTROL SYSTEM | 2003 |
|
RU2251514C1 |
METHOD OF ENHANCING SURVIVABILITY OF FLYING VEHICLE HYDRAULIC SYSTEM, DEVICE FOR REALIZATION OF THIS METHOD AND MULTIPLEXING UNIT | 2004 |
|
RU2279995C1 |
AIRCRAFT HYDRAULIC SYSTEM | 2013 |
|
RU2544053C1 |
SPACE VEHICLE ENGINE PLANT FUEL-FEED SYSTEM | 1999 |
|
RU2170839C1 |
REFUELING TRUCK | 2003 |
|
RU2234441C1 |
SPACE VEHICLE ENGINE PLANT FUEL-FEED SYSTEM | 1999 |
|
RU2170840C1 |
REFUELLER WITH VACUUM OPERATION | 2008 |
|
RU2380293C1 |
FUEL TANKER WITH WATER SEPARATOR | 2008 |
|
RU2378165C1 |
DEVICE FOR FEEDING PROPELLANT TO SPACECRAFT POWER PLANT | 1999 |
|
RU2168050C1 |
DEVICE TO SUPPLY FUEL TO SPACE CRAFT ENGINE PLANT | 1999 |
|
RU2160845C1 |
Authors
Dates
2005-07-20—Published
2003-11-12—Filed