Feature• The motor is fuel cooled,• Optional pressure switch for fuel outlet pressure signal
Supply TypeManufacturer, Exporter, Supplier
Preferred Buyer Location
All over the world
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.