发明名称 ガスタービン発電プラントにおける改良されたインテーク配列
摘要 An improved intake arrangement 100, for a compressor 12 having a compressor blading 14, includes a manifold 110 divided by a barrier 116 into two sections 118, 120, to convey, from one section 118, a flue gas stream, and, from other section 120, an air stream. Further, the intake arrangement 100 includes a converging section 130 configured to the manifold 110 and extends convergingly to the compressor 12 defining an inlet 16 to the compressor blading 14. The converging section 130 includes inner and outer ring members 132, 134 disposed coaxially to each other, between which there extends, coaxially and convergingly, the barrier 116 to at least up to a certain distance within the converging section 130, defining a converging nozzle 140 therebetween. The converging nozzle 140 includes a mixing feature 144 adapted to enhance mixing of the flue gas and air streams.
申请公布号 JP5865970(B2) 申请公布日期 2016.02.17
申请号 JP20140164794 申请日期 2014.08.13
申请人 アルストム テクノロジー リミテッドALSTOM Technology Ltd 发明人 ロビン パイン;エリベアト ベンツ
分类号 F02C7/04;F02C3/34;F23R3/00 主分类号 F02C7/04
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