发明名称 MULTISTAGE TURBO COMPRESSOR
摘要 PROBLEM TO BE SOLVED: To improve the efficiency of a multistage turbo compressor, by widening the range of stable operation without causing complication of the configuration, upsizing of the device configuration, and weight increase. SOLUTION: In the multi-stage turbo compressor in which a plurality of impellers 1, 2, 3 of multistage are connected in series, torque is input to the impeller 2 of intermediate stage, torque is transmitted to the impeller 1 of pre-stage and the rear impeller 3 of post-stage from the impeller 2 of intermediate stage through an differential mechanism 4 for distributing power, and the impeller 1 of pre-stage and the impeller 3 of post-stage are coupled together so that revolving speeds of them are increased or decreased oppositely. COPYRIGHT: (C)2010,JPO&INPIT
申请公布号 JP2010180859(A) 申请公布日期 2010.08.19
申请号 JP20090027443 申请日期 2009.02.09
申请人 IHI CORP 发明人 HAGAWA YUKIHAYA
分类号 F04D29/053;F04D17/12 主分类号 F04D29/053
代理机构 代理人
主权项
地址