发明名称 TURBO COMPRESSION SYSTEM
摘要 Disclosed turbo compression system comprises a first impeller having a first inlet and a first outlet, compressing fluid flowing in through the first inlet by rotation motion and then discharging out through the first outlet; a second impeller having a second inlet and a second outlet, compressing fluid flowing in through the second inlet by rotation motion and then discharging out through the second outlet; a second discharge flow path connected with the second outlet; a first discharge flow path communicating the second discharge flow path with the first outlet; a first valve provided at the first discharge flow path and controlling flowing of the fluid; a second intake flow path connected with the second inlet and selectively making the fluid flow into the second impeller; a second valve provided at one end of the second intake flow path; and a compression flow path connected with the first valve at one end of the compression flow path and connecting with the second intake flow path at the other end of the compression flow path, and has plural design points; the characteristics of two-stage turbo compression system and single-stage dual-intake turbo compression system to be selectively converted.
申请公布号 EP2857692(A4) 申请公布日期 2016.03.02
申请号 EP20130796768 申请日期 2013.05.31
申请人 KTURBO INC. 发明人 LEE, HEON SEOK
分类号 F04D19/04;F04D17/10;F04D17/12;F04D25/16;F04D27/02;F04D29/28 主分类号 F04D19/04
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