| 摘要 |
<p>The present invention relates to: a gas turbine having a rotor shaft, which is movable in the direction of a rotation shaft, for adjusting a turbine blade front end gap, and having a blade vane carrier, which is movable in the direction of the rotation shaft, for adjusting a compressor blade front end gap when the rotor shaft moves, thereby enabling the active adjustment of the compressor blade front end gap; and a control method therefor.</p> |
