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.

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.