Fuel pump 13C1-1

with electric motorself-primingimpeller

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 1 15.5 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 Aerospac€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. - • 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