发明名称 |
Rotor balancing device for loading device i.e. exhaust turbo charger, has nozzle ring comprising nozzles directed towards turbine/compressor wheel, where nozzles generate gas flow flowing on turbine/compressor wheel |
摘要 |
<p>The device (1) has a pressure source for generating a guest current driving a rotor (2). A nozzle ring (3) surrounds a turbine/compressor wheel (4) and comprises two nozzles (5) directed towards the turbine/compressor wheel. The nozzles are formed such that the nozzles generate gas flow flowing on the turbine/compressor wheel. The nozzles are directed on a radial outer region of rotating blade of the turbine/compressor wheel. The pressure source generates a gas pressure of 6 bars. An annular groove (6) is provided in the nozzle ring and connected with the pressure source and the nozzles.</p> |
申请公布号 |
DE102008049144(A1) |
申请公布日期 |
2010.04.01 |
申请号 |
DE20081049144 |
申请日期 |
2008.09.26 |
申请人 |
BOSCH MAHLE TURBO SYSTEMS GMBH & CO. KG |
发明人 |
NGUYEN-SCHAEFER, THANH-HUNG;GOETZ, KLAUS;KRETH, JENS |
分类号 |
G01M1/06;F02B29/00 |
主分类号 |
G01M1/06 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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