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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.
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 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
APPLICATIONS:
• Commercial and military transports
• Business and general aviation
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FLUID SYSTEMS DIVISION
16666 VON KARMAN AVE
IRVINE
CA
UNITED STATES
92606
Teléfono
9498333000
Fax
9498513788
Cree una cuenta para gestionar todo lo que haga con Parker, desde sus preferencias de compra hasta su acceso a la aplicación.