发明申请
- 专利标题： GAS TURBINE SYSTEM HAVING AN EVAPORATIVE COOLER
- 专利标题（中）： 具有蒸发冷却器的气体涡轮机系统
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申请号： US14075213申请日： 2013-11-08
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公开(公告)号： US20140060058A1公开(公告)日： 2014-03-06
- 发明人: Jens Birkner , Walter David , Rudolf Gensler , Arne Graßmann , Knut Halberstadt , Beate Heimberg , Bora Kocdemir , Rainer Nies , Jörg Schürhoff , Werner Stamm
- 申请人： Jens Birkner , Walter David , Rudolf Gensler , Arne Graßmann , Knut Halberstadt , Beate Heimberg , Bora Kocdemir , Rainer Nies , Jörg Schürhoff , Werner Stamm
- 优先权： EP07002345.2 20070202
- 主分类号： F02C7/143
- IPC分类号： F02C7/143
摘要：
A gas turbine system includes a compressor; a combustion chamber; a gas turbine; and an evaporative cooler. The evaporative cooler includes a plurality of cooling elements, a flow channel, and a feed device. The plurality of cooling elements are arranged in the flow channel. The feed device supplies a liquid to the plurality of cooling elements. The liquid is evaporated or vaporized. Each of the plurality of cooling elements is a flat cooling sheet, a surface of the cooling sheet having hydrophilic properties at least in a subregion which is specified for forming a liquid film. The evaporative cooler is connected ahead of the compressor on an intake side.
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