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公开(公告)号:US20140060058A1
公开(公告)日:2014-03-06
申请号:US14075213
申请日:2013-11-08
申请人: Jens Birkner , Walter David , Rudolf Gensler , Arne Graßmann , Knut Halberstadt , Beate Heimberg , Bora Kocdemir , Rainer Nies , Jörg Schürhoff , Werner Stamm
发明人: Jens Birkner , Walter David , Rudolf Gensler , Arne Graßmann , Knut Halberstadt , Beate Heimberg , Bora Kocdemir , Rainer Nies , Jörg Schürhoff , Werner Stamm
IPC分类号: F02C7/143
CPC分类号: F02C7/143 , C09D1/00 , C23C18/1254 , C25D11/02 , F01D25/305 , F02C7/1435 , F28C3/08 , F28F13/18 , F28F2245/02
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.
摘要翻译: 燃气轮机系统包括压缩机; 燃烧室; 燃气轮机; 和蒸发冷却器。 蒸发冷却器包括多个冷却元件,流动通道和进给装置。 多个冷却元件布置在流动通道中。 进料装置向多个冷却元件供应液体。 液体被蒸发或汽化。 多个冷却元件中的每一个都是平坦的冷却片,冷却片的至少在形成液膜所规定的次级区域具有亲水性。 蒸发冷却器在进气侧连接在压缩机前方。