发明名称 MULTI-STAGE LIQUID-RING COMPRESSOR
摘要 FIELD: engines and pumps. ^ SUBSTANCE: multi-stage liquid-ring compressor includes external rotor 1 and internal rotor 31, which can be rotated from external drives 2 and 18 respectively. Rotor 1 forms liquid ring 6 with free surface 8 in ambient gas medium during rotation with working liquid. Rotor 31 is arranged with eccentricity in liquid ring 6 and has discs 7, 10, 12, and 14 which do not go beyond limits of liquid ring 6 and form hydraulic locks in pairs with discs 5, 16 of rotor 1. Closed suction cavity filled with gas and impeller put on rotor 31 shaft is located between locks in each section of liquid ring 6. In flow part of impeller there located is suction chamber 9 cyclically going beyond volume limits of liquid ring 6 during rotor 31 rotation. Delivery channel 24 with delivery valve 25 enters suction cavity of impeller of the next stage. Ratio of rotation frequencies of rotors 1 and 31 is permanent. ^ EFFECT: enlarging the range of gas pressures required for the consumer.
申请公布号 RU2414625(C1) 申请公布日期 2011.03.20
申请号 RU20090131951 申请日期 2009.08.25
申请人 MAKOVETSKIJ ANATOLIJ FEDOROVICH 发明人 MAKOVETSKIJ ANATOLIJ FEDOROVICH
分类号 F04C19/00 主分类号 F04C19/00
代理机构 代理人
主权项
地址