Original document(19 pages) Authorized document(19 pages) 中文版
    The centrifugal compressor has several groups of blades installed and each blade group includes several blades in impeller circumference and concentrical with the rotating center of the impeller rotating axle. The single blades of blade group near the impeller can rotate. It case that the air inlet vaolume is changed, the diffuser efficiency will reduce and the air flow can not flow easily from one blade to the other. Therefore, the blades will rotate to change their front wing central line angle to conform the direction of the air flow the impeller exhausts. So, even if the inlet air volume is changed, the efficiency of the diffuser may be maintained at relatively higher level.
Application Number
申请号
01124348 Application Date
申请日
2001.07.27
Title 名称 Centrifugal compressor
Publication Number
公开号
1399077 Publication Date
公开日
2003.02.26
Approval Pub. Date Granted Pub. Date 2005.03.09
International Classification 分类号 F04D29/46
Applicant(s) Name
申请人
Mitsubishi Jukogyo K.K.
Address 地址
Inventor(s) Name 发明人
Attorney & Agent 代理人 zheng xiuzhe
More information 更  多  信  息


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