发明名称 TERMINATION COVER FOR A COMPRESSOR IMPELLER OF AN EXHAUST GAS TURBOCHARGER AND EXHAUST GAS TURBOCHARGER
摘要 <p>The present invention is to provide a termination cover (13) for a compressor impeller of an exhaust gas turbocharger, which includes a main body (16) having a passage aperture (17) for a shaft, wherein the air-return compressor impeller can be separated from an oil supply assembly of the exhaust gas turbocharger through the termination cover. At least one annular protrusion (22) is formed in the main body (16).</p>
申请公布号 KR20150018438(A) 申请公布日期 2015.02.23
申请号 KR20140101054 申请日期 2014.08.06
申请人 发明人
分类号 F01D11/00;F01D25/24;F01D25/28;F02B39/00;F02B39/14 主分类号 F01D11/00
代理机构 代理人
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