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    • 33. 发明专利
    • TWO-SHAFT GAS TURBINE ENGINE
    • JPH0441935A
    • 1992-02-12
    • JP14730190
    • 1990-06-07
    • TOYOTA MOTOR CORP
    • WATANABE ATSUSHI
    • F02C3/10B60W10/06F01D19/00F02B1/04F02C7/32F02C7/36F02C9/54F02C9/56F16H61/66F16H61/662
    • PURPOSE:To improve acceleration responsiveness immediately after starting of a vehicle by providing an automatic transmission mechanism which can change reduction ratio corresponding to driving state of an engine between an output shaft of an output turbine and an input shaft of a transmission in a two-shaft gas turbine engine. CONSTITUTION:This two-shaft gas turbine engine mounted on a vehicle is provided with a front gear F/G to which a fuel pump, an oil pump, a starter motor and so on are connected, a compressor C, a heat exchanger HE, a combustor CC, a compressor turbine CT directly connected to the compressor C by a rotation shaft, a variable nozzle VN, and a gas turbine GT having a power turbine (output turbine) PT and a reduction gear R/G and so on, and an automatic transmission A/T is connected to the reduction gear R/G through a continuously variable transmission CVT. And a revolution speed is converted to the speed corresponding to a shift state by a torque converter T/C of the automatic transmission A/T provided with a lock-up clutch L/C and a transmission mechanism TM, an output of this automatic transmission A/T is transmitted to a wheel W through a differential gear D so as to drive the vehicle.
    • 36. 发明专利
    • CONTROLLER OF DOBLE AXIS GAS-TURBINE ENGINE
    • JPH03141830A
    • 1991-06-17
    • JP27722589
    • 1989-10-26
    • TOYOTA MOTOR CORP
    • AMANO KENJI
    • F02C9/28F02C9/54
    • PURPOSE:To improve responsiveness of opening control of a variable nozzle by converting the temperature at inlet of a target compressor turbine to a target pressure ratio, and controlling the opening of the variable nozzle so that a value of the pressure ratio becomes equal to the target pressure ratio. CONSTITUTION:Outlet pressure P3 of a compressor C, outlet pressure P5 of a compressor turbine CT and the number of revolutions N1 of a gas generator GG are detected by respective sensors SP3, SP5, SN1. Temperature T4 is calculated by using the relation between the number of revolutions N1 and the inlet temperature T4 of the compressor turbine CT. When the temperature T4 is not at the target value, and an engine PT is under a normal condition, a pressure ratio P3/P5 is compared with a target value of a memory means 1 and a comparison means 2. The opening of a variation nozzle VN is adjusted by a control means 3 through stably maintaining the number of revolutions N1 of the compressor C so that the temperature T4 becomes the target value. Thereafter the calculation of temperature T4 is not performed, but adjusted only by the pressure P3/P5. In this way, the responsiveness of control can be improved.