This electric motor-driven cooling pump assembly has two motor pumps for either redundancy or dual flow operation.
Parker Aerospace pressure-compensated, axial piston engine-driven pumps provide hydraulic power to a variety of aerospace systems. They range in size from 0.03 to 5.5 in³/rev and capable of operation at system pressures between 1,000 and 8,000 psi.
Spar-mounted or cartridge/canister pumps supplying fuel to the APU during ground and flight operations. This type of pump provides less flow and pressure than a typical engine feed pump and may or may not be required to re-prime at altitude.
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.
Cartridge/canister or in-tank mounted pumps, transferring fuel between tanks. 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.
Parker Aerospace's wing tank pump is a spar-mounted pump designed to supply fuel to the aircraft engine. The maximum discharge pressure is limited by an internal valve, and reverse flow through the pump is prevented by check valves.
Parker Aerospace's engine feed ejector pumps are hydro-mechanical jet pumps, with no moving parts. The pumps independently supply fuel to their respective engines using the motive flow supplied by the engine
Electric motor-driven pumps can be used as primary, supplemental, or emergency backup hydraulic power in a variety of aerospace applications. Both DC and AC motors with full control are available and can be adapted to the application's individual need.
Parker Aerospace in-line potable water pump is designed to supply up to six GPM flow at 18 psi. Equipped with EMI filtering, sensor-less locked rotor protection software, and discrete output signals for high-current, high-temperature, rotor rotation
The electric motor-driven pump (EMP) is liquid cooled to increase the efficiency of the motor cooling for aircraft-specific applications, where the flow can be easily adjusted to meet the needs of your application.
This electric motor-driven gear pump assembly meters fuel directly to a gas turbine engine fuel manifold and nozzles.