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Brayton cycle gas turbine - has combustion chamber and turbine with hot-cool operating cycle

机译:布雷顿循环燃气轮机-具有燃烧室和具有热冷运行循环的涡轮机

摘要

The constant pressure, Brayton cycle gas turbine includes a combustion chamber and a turbine uses a hot- cool operating cycle with a hot phase alternating with cool phase. Gas is continuously fed to the combustion chamber and from the combustion chamber to the turbine. During the hot phase all of the gas fed to the turbine is hot. The gas temperature during the hot phase is higher than the turbine could withstand in a continuous burn mode. The time of the hot phase is less than the time it would take for the turbine blades to "soak" to the high temperature of the hot gas.
机译:恒定压力的布雷顿循环燃气涡轮机包括燃烧室,并且涡轮机使用热相与冷相交替的热冷操作循环。气体被连续地输送到燃烧室,并且从燃烧室被输送到涡轮。在热阶段,送入涡轮的所有气体都是热的。热阶段的气体温度高于涡轮在连续燃烧模式下的承受温度。热阶段的时间少于涡轮叶片“吸收”到热气体的高温所花费的时间。

著录项

  • 公开/公告号IT1114474B

    专利类型

  • 公开/公告日1986-01-27

    原文格式PDF

  • 申请/专利号IT19790048309

  • 发明设计人

    申请日1979-03-12

  • 分类号F02C;

  • 国家 IT

  • 入库时间 2022-08-22 07:39:26

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