FIELD: aircraft instrumentation engineering; measurement of mass of fuel on board maneuverable aircraft. SUBSTANCE: proposed system includes sensors and indicators showing parameters of fuel contained in aircraft fuel tanks: indicators of suspension and dropping of first usage tanks auxiliary tanks, sensors of flow rate of fuel being used and meters of fuel characteristic parameters; sensors of flow rate of fuel being received and meters of said fuel characteristic parameters, as well as fuel level sensors and meters of said fuel characteristic parameters. System includes also fuel data processing units. For effective compensation of error of measurement of fuel mass, especially when aircraft works on foreign fuels, system is provided with two different meters of fuel characteristic parameters: fuel temperature meter and fuel static dielectric permeability meter for measurements at DC or low-frequency AC. EFFECT: enhanced accuracy of measurement of mass of fuel carried on board aircraft. 4 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
ON BOAR FUEL GAUGING SYSTEM WITH STATIC DIELECTRIC FUEL PERMEABILITY COMPENSATION | 2001 |
|
RU2186345C1 |
ON-BOARD FUEL GAUGING SYSTEM WITH COMPENSATION IN FUEL CHARACTERISTIC PARAMETERS | 2001 |
|
RU2191142C1 |
ON-BOARD FUEL GAUGING SYSTEM WITH COMPENSATION IN DYNAMIC DIELECTRIC FUEL PERMEABILITY | 2001 |
|
RU2191356C1 |
ON-BOARD FUEL GAUGING SYSTEM WITH COMPENSATION FOR STATIC AND DYNAMIC DIELECTRIC FUEL PERMEABILITY | 2001 |
|
RU2191355C1 |
ON-BOARD FUEL GAUGING SYSTEM WITH TEMPERATURE AND STATIC DIELECTRIC FUEL PERMEABILITY COMPENSATION | 2001 |
|
RU2186346C1 |
AIRBORNE FUEL GAGGING SYSTEM WITH TEMPERATURE COMPENSATION | 2001 |
|
RU2189926C1 |
PROCEDURE ESTABLISHING MASS FUEL RESERVE ABOARD MANEUVERING AIRCRAFT | 2001 |
|
RU2220403C2 |
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 |
Authors
Dates
2002-10-20—Published
2001-10-10—Filed