Water pump AP series

hydraulic motorself-primingaxial piston

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. BY CHOOSING A SPECIFIC MAXIMUM OUTPUT FLOW VALUE ABOVE, SPECIFIC PERFORMANCE CHARACTERISTICS CAN BE VIEWED ON - THE TECH SPECIFICATIONS TAB. - The engine-driven pump (EDP) product line, designed and manufactured by the Parker Aerospace Hydraulic Systems Division (HSD), provides - the primary hydraulic power for many of today's leading military and commercial aircraft including: - • Airbus A220, A320, and A350XWB - • Boeing 737,747, 757, 767, 777X, and 787 - • Boeing F-1 5, F-18, and 8-52 - • Bombardier Global 5500, 6500, 7500, Challenger 350 - • Cessna Latitude, Longitude, Sovereign and Citation X - • COMAC ARJ21, cgu - • Dassault Falcon 7X / 8X - • Embraer 170/1 go - • Gulfstream G400, G500, G600, G550, G650, G700 - • Lockheed Martin F-16 Falcon and C130 Hercules - • Mitsubishi CRJ 700/900/1 OOO and space,let - • Northrop Grumman 8-2 Spirit - • Sukhoi Superjet - Ranging in size from 0.03 to 5.5 in3/rev and capable of operation at system pressures between 1 ,OOO and 8,000 psi, Parker Aerospace EDPS - provide unmatched efficiency and reliability in a compact, lightweight package, with a superior power-to-weight ratio. - OPERATION: - EDPS serve as the primary supply of hydraulic flow and pressure for the hydraulic users within the aircraft system. The typical EDP -