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CN106089443A 用于涡轮机的热管冷却系统 无效 - 撤回

用于涡轮机的热管冷却系统
摘要：
一种涡轮机(100)包括压缩机(110)，压缩机(110)构造成压缩在进口部分(202)接收的空气以形成离开到出口部分(204)中的压缩空气流。压缩机具有多个转子叶片(112)和多个定子导叶(113)、和形成压缩机外壳的压缩机壳体(111)；燃烧器(120)与压缩机可操作地连接且燃烧器接收压缩空气流。涡轮(130)与燃烧器可操作地连接且涡轮从燃烧器接收燃烧气体流。涡轮具有涡轮壳体。冷却系统操作地连接到压缩机壳体。冷却系统包括位于多个定子导叶(113)的至少一部分中的多个热管(250)。热管(250)构造成与压缩机壳体(111)热连通。由多个热管(250)吸收的热量被传递至压缩机壳体(111)。
摘要（英）：

A turbomachine includes a compressor configured to compress air received at an intake portion to form a compressed airflow that exits into an outlet portion. The compressor has a plurality of rotor blades and a plurality of stator vanes, and a compressor casing forming an outer shell of the compressor. A combustor is operably connected with the compressor, and the combustor receives the compressed airflow. A turbine is operably connected with the combustor, and the turbine receives combustion gas flow from the combustor. The turbine has a turbine casing. A cooling system is operatively connected to the compressor casing. The cooling system includes a plurality of heat pipes located in at least a portion of the plurality of stator vanes. The heat pipes are configured to be in thermal communication with the compressor casing. The heat absorbed by the plurality of heat pipes is transferred to the compressor casing.

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