The model number assigned was X24C10, even though the J46 differed in many design features from the smaller J34.
#Westinghouse j34 combustor series#
Normal thrust, flight: 570 lbf (2.54 kN) at 16,260 rpm at altitude, 19B 465 lbf (2. The Westinghouse model number was a continuation of the 'X24C' series of the J34. The Westinghouse J34 was a turbojet engine developed by Westinghouse Electric Corporation's Aviation Gas Turbine Division in the late 1940s. First run on 11 January 1947, the 24C was essentially an enlarged version of the earlier Westinghouse J30, the J34 produced 3,000 pounds of thrust, twice as much as the J30. Among others were the following civil and military aircraft equipped with the. The Westinghouse J34, company designation Westinghouse 24C, was a turbojet engine developed by Westinghouse Aviation Gas Turbine Division in the late 1940s. Rolls- Royce Avon are under the name RT48/RT56 as stationary drive eg used on oil rigs. Maximum thrust: 1,360 lbf (6.05 kN) at 18,000 rpm at sea level, 19B 1,400 lbf (6.23 kN) at 18,000 rpm at sea level The highest thrust generated version RA.29 Mk.301 / 2 ( RB.146 ) for the English Electric Lightning, the 56.5 kN, with additional afterburner even delivered almost 73 kN thrust. Oil system: pressure spray at 40 psi (275.8 kPa) dry sump, 60 S.U. Length: 100 in (2,540.0 mm), 19B 104.5 in (2,654.3 mm) Gas Turbine Combustion: Alternative Fuels and Emissions Arthur H. ISBN 0-7509-4479-X.Variants 19A Prototypes and initial production 19B Increased mass flow version delivering 1,400 lbf (6.23 kN) at 18,000 rpm at sea level J30-WE-20 production engines delivering 1,600 lbf (7.1 kN) thrust Applications 500 VELOCITY P - 30742 - D Accessories Cutaway drawing of Westinghouse J34 engine. Inlet manifold 1.6 VTEC 1.6 Internal combustion engine 1.5 Compression ratio 1.5 Engine swap 1.4. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. Westinghouse J34 - Wikipedia O M KThe Westinghouse J34. World Encyclopedia of Aero Engines, 5th Edition. Specific fuel consumption: 1.04 lb/hr-lb. 
Compressor: Single-Spool, 11-stage Axial.C-119 Flying Boxcar (civilian variant modification).peratures, the better its performance (as is the case with gas turbine combustion and. ĭeveloped during the transition from piston-engined aircraft to jets, the J34 was sometimes fitted to aircraft as a supplement to other powerplants, as with the P-2 Neptune and Douglas Skyrocket (fitted with radial piston engines and a rocket engine, respectively). Navy) and the engine builders (GE, Pratt & Whitney, Westinghouse. However, equipped with the J34 instead of its intended engines, it was seriously underpowered and could not exceed Mach 1 in level flight. By 1944, Westinghouse was working on three derivatives of its first axial engine, the 19A. The Stiletto was developed to investigate the design of an aircraft at sustained supersonic speeds. centrifugal compressor and a can-annular, reverse-flow combustor arrangement with 14 cans. For instance, the Douglas X-3 "Stiletto" was equipped with two J34 engines when the intended Westinghouse J46 engine proved to be unsuitable. Westinghouse J34 was also deployed in the Douglas Skyrocket. Built in an era of rapidly advancing gas turbine engine technology, the J34 was largely obsolete before it saw service, and often served as an interim engine.
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