Aerospace Axial, Cooling and Fluid Pumps

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.

This electric motor-driven cooling pump assembly has two motor pumps for either redundancy or dual flow operation.

This electric motor-driven gear pump assembly meters fuel directly to a gas turbine engine fuel manifold and nozzles.

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.

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 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 are capable of operation at system pressures between 1,000 and 8,000 psi.

Parker Aerospace in-line potable water pump supplies up to six GPM flow at 18 psi. Equipped with EMI filtering, sensor-less control and locked rotor protection software, and discrete output signals for high-current, high-temperature, and 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.

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

Power transfer units (PTUs) are used to transfer hydraulic power from one hydraulic system to another without mixing fluid. PTUs are generally used for a contingency purpose or as a ground service source of hydraulic power.

This electric motor-driven scavenge pump assembly is for UAV platforms and ideal for medium and continuous duty; suitable for propulsion or power generation gas turbine engines.

The scavenge ejector pumps are hydro-mechanical venturi pumps, with no moving parts, that transfer fuel from the wing tanks to the collector bays, using the engine’s motive flow.

Gearbox-driven lubrication and scavenge pumps use gerotor technology to provide the customized, smallest, most compact, lightweight, reliable solution to distribute lubricating oil into main gas turbine engine and scavenge the oil back to the reservoir.

Gearbox-driven lubrication pumps use gerotor technology to provide customized smallest, most compact, lightweight, reliable solution to distribute lubricating oil into main gas turbine engine.

Electric motor-driven (EMD) lubrication and scavenge pumps use brushless DC motors combined with gerotor technology to provide a custom and reliable solution. The EMD pump sends high-pressure lubricating oil to the gas turbine engine while simultaneously

Gearbox-driven scavenge pumps use gerotor technology to provide customized, smallest, most compact, lightweight, reliable solution to scavenge lubricating oil from the main gas turbine engine back to the reservoir.

aerospace-pumps

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