FUEL FLOW METER SYSTEM WITH TEMPERATURE COMPENSATION OF MANEUVERABLE AIRCRAFT Russian patent published in 2008 - IPC B64D37/00 B64D37/14 G01F23/00 

FIELD: aircraft instrument.

SUBSTANCE: system may be used to meter fuel stock and flow in a maneuverable aircraft. The system contains fuel mass flow rate pickups (12) mounted in the fuel line, fuel flow rate pickups (4) arranged in priming and operating lines of fuel tanks as well as in balancing lines (17), return line (6) and fuel pumping up line (9), fuel level pickups (1) and fuel level signalling devices (19) arranged in fuel tanks and fuel temperature pickups (2) mounted in the aircraft lines power plant tanks. The system incorporates, also, airborne computer (22), comparator (28), indicator (29) and the following electronic units, i.e. overflow unit (23), return unit (26), fuelling unit (24), refuelling unit (25) and balancing unit (27). Proceeding from the data on fuel coming from the aforesaid system pickups, signalling devices and the counter, and in compliance with data received from the aircraft outer systems on types of fuelling, refueling and returning kept in the airborne computer, comparator and counter memory, the system defines the amount of fuel fed into the tanks on ground, current stock of fuel in flight, the amount of fuel fed from the aircraft and aerodynamic amount of fuel required for aircraft return.

EFFECT: higher accuracy and efficiency of control over fuel flow rates and distribution.

1 dwg