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    • 13. 发明专利
    • GAS TURBINE DEVICE
    • JP2003206754A
    • 2003-07-25
    • JP2002003313
    • 2002-01-10
    • EBARA CORP
    • MARUI HIDEFUMIMCKELVEY TERENCEMIYAMOTO MASAHIROKATAOKA TADASHIFURUYA YASUSHI
    • F02C9/28F02C9/00G05B11/36
    • PROBLEM TO BE SOLVED: To provide a gas turbine device equipped with a control unit capable of controlling a gas turbine in a good condition even when controlling any condition of the acceleration or deceleration of the gas turbine. SOLUTION: The control unit 11 is equipped with an operation part 13a for acceleration, and operation part 13b for deceleration and an output switching part 13c. The operation part 13a for acceleration calculates the optimal control signal for promptly bringing the number of rotations of the turbine close to the target number of rotations by accelerating the turbine when the present number of rotations of the turbine is lower than the target number of rotations. The operation part 13b for deceleration calculates the optimal control signal for promptly bringing the number of rotations of the turbine close to the target number of rotations by decelerating the turbine when the present number of rotations of the turbine is higher than the target number of rotations. The output switching part 13c inputs a control signal from the operation part 13a for acceleration and the control signal from the operation part 13b for deceleration, adopts the control signal from the operation part 13a for acceleration and outputs it when the turbine is accelerated, and adopts the control signal from the operation part 13b for deceleration and output it when the turbine is decelerated. COPYRIGHT: (C)2003,JPO
    • 17. 发明专利
    • Centrifugal compressor
    • 离心式压缩机
    • JPS59599A
    • 1984-01-05
    • JP10670882
    • 1982-06-23
    • Ebara Corp
    • FURUYA YASUSHI
    • F04D17/08F04D29/44
    • F04D29/444
    • PURPOSE:To raise the efficiency of a compressor, by reducing the expansion loss and the frictional loss of a fluid by connecting a return channel having a return valve to the outlet of a U-turn section formed at the outlet of a diffuser, and connecting an annular chamber having a discharge opening to the outlet of said return channel. CONSTITUTION:Since the velocity energy of a fluid is recovered considerably while passing through a diffuser 4, the speed of fluid flow is decreased and the pressure is increased. The fluid enters into a U-turn section 12, where the speed of fluid flow is further decreased and the pressure is further increased, and then the fluid enters into an inlet end 16 of a return vane 13 at the minimum speed. Thereafter, the fluid is introduced into an annular chamber 18 via a return channel 14 at a speed decreased to a level lower than the discharge speed at a discharge opening 6, and then discharged to the outside from the discharge opening 6. Thus, since the pressure of fluid is raised continuously by decreasing the speed of fluid flow from that at the outlet of the diffuser 4 to that at the outlet of the return channel 14 and residual energy at the outlet of the diffuser 4 can be recovered efficiently, it is enabled to raise the efficiency of a compressor as a whole.
    • 目的:为了提高压缩机的效率,通过将具有回流阀的返回通道连接到形成在扩散器的出口处的U形转弯部分的出口,通过减小膨胀损失和流体的摩擦损失,并连接 环形室具有通向所述返回通道出口的排放口。 构成:由于在通过扩散器4时流体的速度能量被大大地恢复,所以流体流动的速度降低并且压力增加。 流体进入U形转弯部分12,其中流体流动的速度进一步降低并且压力进一步增加,然后流体以最小速度进入回流叶片13的入口端部16。 此后,流体通过返回通道14以降低到排出口6处的排出速度的水平的速度被引入到环形室18中,然后从排出口6排出到外部。因此,由于 流体的压力通过降低从扩散器4的出口处的流体流速到返回通道14的出口处的流动速度而连续升高,并且能够有效地恢复扩散器4的出口处的剩余能量, 提高整体压缩机的效率。