发明名称 Integrated turbocharger fan intercooler with partial isothermal compression
摘要 An integrated cooling system for a turbocharger, suitable for an internal combustion engine. A cooling air shroud surrounds a portion of an interstage duct in a two-stage turbocharger, and may also surround a part of the outlet from the turbocharger. A fan on a turbocharger shaft is driven by the turbocharger turbine to draw air into the cooling air shroud, and pass the cooling air in heat exchange relationship with compressed air flowing through the turbocharger. The fan may also be used to precompress air compressed in the turbocharger.
申请公布号 US6557345(B1) 申请公布日期 2003.05.06
申请号 US20010022642 申请日期 2001.12.17
申请人 CATERPILLAR INC 发明人 MOECKEL MARK D.
分类号 F02B29/04;(IPC1-7):F02B29/04 主分类号 F02B29/04
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