FIELD: aircraft instrumentation engineering; measurement of fuel capacity and consumption on board aircraft.
SUBSTANCE: proposed system is provided with fuel flow sensors mounted in operating lines and in replenishing lines of aircraft and in return lines of power plant, fuel mass flow meter mounted in fuel supply line, fuel level sensors and detectors mounted in fuel tanks, fuel temperature sensors and fuel dielectric permeability sensors mounted in lines and in tanks of aircraft power plant. System is also provided with onboard computer, comparison unit, indicator and the following electronic units: bypass unit, return unit, filling unit, replenishing unit and trimming unit.
EFFECT: enhanced efficiency and reliability.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FUEL FLOW METER SYSTEM WITH FUEL TEMPERATURE COMPENSATION | 2006 |
|
RU2327611C1 |
| FUEL FLOW METER SYSTEM WITH FUEL TEMPERATURE AND DIELECTRIC PERMEABILITY COMPENSATION | 2006 |
|
RU2327612C1 |
| AIRBORNE AIRCRAFT FUEL FLOW METER SYSTEM WITH FUEL TEMPERATURE AND DIELECTRIC PERMEABILITY COMPENSATION | 2006 |
|
RU2327613C1 |
| AIRBORNE AIRCRAFT FUEL FLOW METER SYSTEM WITH FUEL DIELECTRIC PERMEABILITY COMPENSATION | 2006 |
|
RU2327614C1 |
| AIRCRAFT FUEL GAGING AND FLOW-METERING SYSTEM AT COMPENSATION OF FUEL DIELECTRIC PERMEABILITY | 2006 |
|
RU2317232C1 |
| AIRBORNE MANEUVERABLE AIRCRAFT FUEL FLOW METER SYSTEM WITH FUEL DIELECTRIC PERMEABILITY COMPENSATION | 2006 |
|
RU2327615C1 |
| AIRBORNE MANEUVERABLE AIRCRAFT FUEL FLOW METER SYSTEM WITH FUEL DIELECTRIC PERMEABILITY COMPENSATION | 2006 |
|
RU2327609C1 |
| MANEUVERABLE AIRCRAFT ONBOARD FUEL GAGING AND FLOW-METERING SYSTEM AT FUEL TEMPERATURE AND DIELECTRIC PERMEABILITY COMPENSATION | 2006 |
|
RU2317228C1 |
| FUEL FLOW METER SYSTEM WITH TEMPERATURE COMPENSATION OF MANEUVERABLE AIRCRAFT | 2006 |
|
RU2327610C1 |
| AIRCRAFT ONBOARD FUEL GAGING AND FLOW-METERING SYSTEM AT TEMPERATURE COMPENSATION | 2006 |
|
RU2317229C1 |
