Oil system: pressure spray at 40 psi (275.8 kPa) dry sump, 60 S.U.XJ30-WE-7 1,600 lbf (7.1 kN) for Northrop X-4 XJ30-WE-8 originally designated J43 XJ30-WE-9 1,600 lbf (7.1 kN) for Northrop X-4 J30-WE-20 production engines delivering 1,600 lbf (7.1 kN) thrust, Internal model 19XB-2B Applications
Westinghouse j34 oil pump driver#
Variants 19A Prototypes and initial production, boost engines 19B Increased mass flow version delivering 1,400 lbf (6.23 kN) at 18,000 rpm at sea level, added gearbox to allow engine to be a prime driver 19XB-2B Company designation for WE-20. It was developed into the smaller J32, and the successful Westinghouse J34, an enlarged version which produced 3,000 pounds of thrust. Its first flight was under a FG Corsair in January 1944. ContentsĪ simple and robust unit with six-stage compressor, annular combustor, and single-stage turbine, it initially gave 1,200 pounds of thrust but improved to 1,600 in production versions. It was the first American-designed turbojet to run, and only the second axial-flow turbojet to run outside Germany (after the British Metropolitan-Vickers F.2). The Westinghouse J30, initially known as the Westinghouse 19XB, was a turbojet engine developed by Westinghouse Electric Corporation. Westinghouse Aviation Gas Turbine Division WikiMili Westinghouse J30 Last updated AugJ30
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