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Expired
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GB20220/39A
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Individual
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Individual
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Publication of GB531905ApublicationCriticalpatent/GB531905A/en
531,905. Gas turbines. JENDRASSIK, G. July 11, 1939, No. 20220. Convention date, July 14, 1938. [Class 110 (iii)] In a gas turbine plant of the continuous combustion type, comprising a compressor 3 driven by the turbine 1, with or without a heat exchanger 7, the load is regulated by byepassing part of the working fluid supplied by the compressor, either in the compressor, or at one or more interstage points 31 ... 31<111> controlled by a slide valve 35. The fluid normally passes from the compressor through pipes 6, 8 to the heat exchanger 47 and through the combustion chamber 10 and pipe 12 to the turbine. Part of the fluid may be byepassed through pipe 17 controlled by a throttle valve 18. Specifications 492,831 and 516,438 are referred to.
GB20220/39A1938-07-141939-07-11Improvements in or relating to gas turbine plant
ExpiredGB531905A
(en)