发明名称 Vortex inlet vanes
摘要 <p>The compressor assembly, for a turbocharger at an internal combustion motor, has an inserted spin unit (7) fitted into the housing (3) and/or the air intake (6) and in front of the running wheel (5), to generate a spiral flow towards the wheel. The spin unit is inserted at the junction between the housing and the air intake, with a mounting flange (12) to secure it radially within the housing or the air intake, and fix it axially between the air intake and the housing. An elastic seal (8) is between the air intake and/or the spin unit and the housing.</p>
申请公布号 EP1416123(A3) 申请公布日期 2008.02.06
申请号 EP20030022991 申请日期 2003.10.10
申请人 BAYERISCHE MOTOREN WERKE AKTIENGESELLSCHAFT 发明人 WIMMER, RUDOLF;STEINDL, WERNER;JURSITZKY, CHRISTIAN;KROISS, ROSWITHA
分类号 F01D9/04;F01D9/06;F01D25/24;F02C6/12;F02C7/00;F02C7/04;F04D29/42;F04D29/44;F04D29/46;F04D29/62 主分类号 F01D9/04
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