发明名称 排気ガス再循環系を備えたガスタービンパワープラント
摘要 What is described is a method for operating a gas turbine power plant, in which fresh air is delivered to a compressor inlet and is accelerated in the compressor inlet and a recirculated first exhaust gas substream is delivered into a region of the compressor inlet in which the fresh air is accelerated to an extent such that the difference between total pressure and static pressure in the fresh air is greater than or equal to a pressure difference which is required in order to suck a target mass flow of the recirculated first exhaust gas substream into the compressor inlet. What is described, further, is a gas turbine power plant with a gas turbine, the compressor inlet of which is divided into two sectors which the flow duct of the compressor adjoins, a feeder for fresh air being connected to the first sector and a recirculation line for recirculating the first exhaust gas substream being connected to the second sector, and the second sector reaching so close to the compressor that, when the gas turbine is in operation, the static pressure at the outlet of the second sector is so low that the difference between total pressure and static pressure is greater than or equal to a pressure difference which is required in order to suck a target mass flow of the recirculated first exhaust gas substream into the compressor inlet.
申请公布号 JP5933767(B2) 申请公布日期 2016.06.15
申请号 JP20140559207 申请日期 2013.02.28
申请人 ゼネラル エレクトリック テクノロジー ゲゼルシャフト ミット ベシュレンクテル ハフツングGeneral Electric Technology GmbH 发明人 エリベアト ベンツ;ヤーン ヘラート;ハンス ヴェットシュタイン;ロビン パイン
分类号 F02C3/30;F01K23/10;F02C6/18;F23R3/00;F23R3/34 主分类号 F02C3/30
代理机构 代理人
主权项
地址