发明名称 Multistage turbofan for a carbon dioxide laser
摘要 The turbofan (10), with input and output sides, has an electrical drive unit with rotor (22) and drive shaft (20). The impellers (12,14,16,18) on both sides of the electrical drive unit rotor are aligned the same way behind each other in the direction of the drive shaft axis. The impeller nearest the input side of the rotor has a flow connection to the impeller nearest the output side of the rotor. The drive shaft has at least three bearing points.
申请公布号 DE19814485(A1) 申请公布日期 1999.10.07
申请号 DE19981014485 申请日期 1998.04.01
申请人 GWJ ENGINEERING GBR DIPL.-ING. GUNTHER WESER DIPL.-ING JOERG WESER 发明人 WESER, GUNTHER;WESER, JOERG
分类号 F04D25/16;F04D29/04;F04D29/58;(IPC1-7):F04D17/12 主分类号 F04D25/16
代理机构 代理人
主权项
地址