Fuel Transfer Pump

产品概况：

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


性能特点：

额定电流（gpm)		Up to 250 gpm
燃料类型		JET A, JP-5, JP-8
最高燃料温度（F)		130°F
最小流体温度（F)		-45°F
温度系数(F)		-65F to 160F
电压值（VAC)		115VAC three phase
频率（赫兹）		360 - 800 Hz