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 fuel transfer pumps main pumping element use a centrifugal impeller driven by a three phase constant frequency or -
variable frequency induction motor. Input frequency varies between 360 and 800 Hz The canister is installed on the wet side of the spar with -
the pump element installed into the canister from the dry side. This allows the element that contains the motor and bearings to be replaced -
without draining the fuel tank.
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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 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: -
• Constant- or variable-frequency three-phase induction motor -
• The motor is fuel cooled -
• The fuel-wetted carbon bearings allow for long-life fluid film design with no rotating shaft seals -
• Optional pressure switch for fuel outlet pressure signal
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APPLICATIONS -
• Commercial and military transports -
• Business and general aviation