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    • 8. 发明申请
    • TURBOMACHINE
    • 涡轮机
    • US20120301280A1
    • 2012-11-29
    • US13479315
    • 2012-05-24
    • Jaroslaw Leszek SzwedowiczAlexey MozharovStefan Irmisch
    • Jaroslaw Leszek SzwedowiczAlexey MozharovStefan Irmisch
    • F01D11/14
    • F01D11/18F01D11/24F05D2300/505
    • A turbomachine which operates at enhanced operating temperatures includes a stationary component. A rotating component includes a clearance to avoid a rubbing contact between the stationary component and the rotating component, the clearance including a first value in a stationary state of the turbomachine and a second value in a steady-state operation of the machine, wherein during a transient operating phase between the stationary state and the steady-state operation, the clearance includes a value which traverses a curve having an extreme value on account of a different time variation of a rotational speed and a thermal expansion of different components. A compensating device includes a non-linear compensation mechanism configured to reduce or compensate the extreme value during the transient operating phase.
    • 在增强的工作温度下操作的涡轮机包括固定部件。 旋转部件包括间隙,以避免固定部件和旋转部件之间的摩擦接触,间隙包括在涡轮机的静止状态下的第一值和机器的稳态操作中的第二值,其中在 在静止状态和稳态操作之间的瞬时动作相位,间隙包括由于不同部件的转速和热膨胀的不同时间变化而横过具有极值的曲线的值。 补偿装置包括被配置为在过渡操作阶段期间减少或补偿极值的非线性补偿机构。