FIELD: aircraft instrumentation engineering; measurement of fuel capacity and consumption on board maneuverable aircraft.
SUBSTANCE: proposed system is provided with fuel mass flow meter mounted in fuel line, fuel flow sensors mounted in filling and service lines of fuel tanks and in trimming lines, unit cooling lines, return line and in fuel replenishing line, fuel level sensors and detectors mounted in fuel tanks and fuel temperature sensors mounted in fuel lines and fuel 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 |
|---|---|---|---|
| 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 |
| FUEL FLOW METER SYSTEM WITH FUEL TEMPERATURE COMPENSATION | 2006 |
|
RU2327611C1 |
| MANEUVERABLE AIRCRAFT ONBOARD FUEL GAGING AND FLOW-METERING SYSTEM AT TEMPERATURE COMPENSATION | 2006 |
|
RU2317230C1 |
| 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 |
| FUEL GAGING AND FLOW-METERING SYSTEM OF MANEUVERABLE AIRCRAFT AT FUEL TEMPERATURE AND DIELECTRIC PERMEABILITY COMPENSATION | 2006 |
|
RU2317231C1 |
| 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 |
