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The story of Westinghouse gas turbine experience lists the many "firsts" achieved during the more than 50 years prior to the sale of the Power Generation Business Unit to Siemens, AG in 1998. [4] As indicated below, the history actually begins with the successful development of the first fully US-designed jet engine during World War II.
The Westinghouse Aviation Gas Turbine Division (AGT) was established by Westinghouse Electric Corporation in 1945 to continue the development and production of its gas turbine engines for aircraft propulsion under contract to the US Navy Bureau of Aeronautics. The AGT Division was headquartered in Kansas City, Missouri, where it remained in ...
The propelling nozzle converts a gas turbine or gas generator into a jet engine. Power available in the gas turbine exhaust is converted into a high speed propelling jet by the nozzle. The power is defined by typical gauge pressure and temperature values for a turbojet of 20 psi (140 kPa) and 1,000 °F (538 °C). [18]
The Westinghouse J30, initially known as the Westinghouse 19XB, was a turbojet engine developed by Westinghouse Electric Corporation. 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 ).
An inlet air cooling system installed in a desert-dry area to increase turbine power output. Turbine inlet air cooling is a group of technologies and techniques consisting of cooling down the intake air of the gas turbine. The direct consequence of cooling the turbine inlet air is power output augmentation.
J40 powered XF3H-1 prototype on the USS Coral Sea in 1953. Westinghouse Electric Corporation established the Westinghouse Aviation Gas Turbine Division (AGT) in 1945. Along with General Electric, Westinghouse had extensive experience in turbine design that put them in the lead over established aviation engine manufacturers, who had little experience with these entirely new design concepts.
The Westinghouse J34, company designation Westinghouse 24C, was a turbojet engine developed by Westinghouse Aviation Gas Turbine Division in the late 1940s. Essentially an enlarged version of the earlier Westinghouse J30 , the J34 produced 3,000 pounds of thrust, twice as much as the J30.
The J46 engine was developed as a larger, more powerful version of Westinghouse's J34 engine, about 50% larger. The Westinghouse model number was a continuation of the "X24C" series of the J34. The model number assigned was X24C10, even though the J46 differed in many design features from the smaller J34.
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