发明名称 TURBOCHARGER OF VARIABLE TURBINE GEOMETRY
摘要 <p><P>PROBLEM TO BE SOLVED: To provide a turbocharger capable of forming a welded coupled part to connect a disk with a vane support ring without generating any distortion if possible and forming a constant uniform clearance like screw connection as a result. <P>SOLUTION: This turbocharger of variable turbine geometry comprises a vane support ring assembly 1 including the vane support ring 2 and the disk 3 which can be fixed to the vane support ring 2 for creating a flow channel 4, and at least one support pin 5 of which first end part 6 is connected with the vane support ring 2 and second end part 7 is welded to the disk 3. The disk 3 has a recessed part to which a support pin end 7 is welded, and the recessed part is surrounded by a heat throttle part 14. <P>COPYRIGHT: (C)2006,JPO&NCIPI</p>
申请公布号 JP2006189041(A) 申请公布日期 2006.07.20
申请号 JP20050348934 申请日期 2005.12.02
申请人 BORGWARNER INC 发明人 BOENING RALF;METZ DIETMAR;FRANKENSTEIN DIRK
分类号 F02B37/24 主分类号 F02B37/24
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