Fuel Boost Pump 13C1-1

Cartridge/canister or in-tank mounted pumps supply fuel to the aircraft engine. Reverse flow through the pump is prevented by check valves. The cartridge/canister design allows removal of the pump cartridge without draining the fuel tank.

Our fuel boost pumps use 28 V direct current (DC) to drive a high efficiency, brushless DC (BLDC) motor or 115.5 V alternating current (AC) three-phase induction motors. The BLDC motor-driven pumps incorporate integral electronic controllers using Hall Effect sensor rotor-position feedback. The hardware-only controller does not use any software or programmable logic devices.

Ranging from fuel boost and transfer pumps to hydraulic brake and actuation pumps, potable water pumps, recirculation pumps, and APU fuel feed pumps, Parker Aerospace’s fuel pumps add real power to both military and commercial aircraft. Our brushless, electric DC motor-driven pumps with sensorless or sensor-based electronic controls offer powerful advantages.

FEATURES AND ATTRIBUTES:
• The motor and electronics are fuel cooled
• The fuel-wetted carbon bearings allow for long-life fluid film design with no rotating shaft seals
• The pumps use a high efficiency brushless DC motor or a three-phase induction motor
• The pumps are qualified for high levels of lightning and electromagnetic interference (EMI)

APPLICATIONS:
• Commercial and regional transports
• Military transports

Характеристики