首页> 外国专利> TURBINE WITH A SHROUD RING AROUND ROTOR BLADES AND METHOD OF LIMITING LEAKAGE OF WORKING FLUID IN A TURBINE

TURBINE WITH A SHROUD RING AROUND ROTOR BLADES AND METHOD OF LIMITING LEAKAGE OF WORKING FLUID IN A TURBINE

机译:涡轮机与转子叶片周围的护罩环和限制涡轮机中的工作流体泄漏的方法

摘要

A gas (or steam) turbine (200) is disclosed including: a rotor with at least one array of rotor blades (213-1), a stator with a casing (261) and a shroud ring (250); the shroud ring (250) extends around the array of blades rotor (213-1) and the casing (261) extends around the shroud ring (250). The shroud ring (250) has radial size independent from temperature thanks to its material, and is movably coupled with the casing (261) so to allow the casing (261) of the stator to thermally expand and contract during operation of the turbine while maintaining the shroud ring radial size. Also the rotor thermally expands and contracts during operation of the turbine, and, at working temperature, tip regions of the rotor blades (213-1) are in close proximity to an inner region of the shroud ring (250) so that clearance is small or even zero at working condition.
机译:公开了一种气体(或蒸汽)涡轮机(200),包括:带有至少一个转子叶片(213-1)的转子,具有壳体(261)的定子和护罩环(250); 护罩环(250)围绕叶片转子(213-1)阵列延伸,并且壳体(261)围绕护罩环(250)延伸。 由于其材料,护罩环(250)具有独立于温度的径向尺寸,并且可与壳体(261)可移动地连接,以允许定子的壳体(261)在保持时在涡轮机的操作期间热膨胀和收缩 护罩环径向尺寸。 此外,转子在涡轮机的操作期间热膨胀和收缩,并且在工作温度下,转子叶片(213-1)的尖端区域靠近护罩环(250)的内部区域,使得间隙很小 在工作条件下甚至零。

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