ONBOARD SYSTEM FOR FUEL CONTROL AND MEASUREMENT WITH COMPENSATION FOR FUEL TEMPERATURE Russian patent published in 2014 - IPC B64D37/00 B64C17/10 G01F9/00 G01F23/22 

FIELD: aircraft engineering.

SUBSTANCE: this system comprises fuel parameter transducers fitted in aircraft fuel tanks: Fuel level and dielectric constant, fuel upper and lower level indicators, onboard computer with left and right control modules, control channels and memory cells on fuel tank geometry, left and right fuel age modules, comparator and balance adjuster. System onboard computer is provided with input to receive extra data from aircraft undercarriage indicator.

EFFECT: higher accuracy, validity and efficiency of measurement fuel mass store, fuel reserve supply and control over aircraft balance at standard and emergent conditions of system operation.

1 dwg