发明名称 GAS TURBINE ENGINE
摘要 PURPOSE:To aim at effectively using energy, by providing two turbines the front one of which is coupled to both compressor and a load, and the rear one of which is coupled to only the compressor. CONSTITUTION:There are provided two of front and rear turbines 2, 3. One of the output shaft 6 of the front turbine 2 is coupled to a compressor 1 via. a speed change unit 4, and the other one of the output shafts 6 is coupled to a load. Further, the output shaft of the rear turbine 3 is coupled to the compressor 1 alone. When the load increases, the rotational speed lowers so that the efficiency of the front turbine 2 lowers. However, lost energy by the front turbine 2 is recovered by the rear turbine, and as well the rotational speed of the compressor 1 is increased upto a steady-state rotational speed by means of the drive force of the output shaft 6. With this arrangement, energy may be effectively used.
申请公布号 JPS60150438(A) 申请公布日期 1985.08.08
申请号 JP19840006243 申请日期 1984.01.19
申请人 SUGIMORI TOSHIO 发明人 SUGIMORI TOSHIO
分类号 F02C3/045;F02C7/36 主分类号 F02C3/045
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