发明公开
EP1805412A1 TURBINE AND COMPRESSOR EMPLOYING TUBERCLE LEADING EDGE ROTOR DESIGN
有权
涡轮机和压缩机OR 与HÖCKER前缘采用了一个转子VERSION
- 专利标题： TURBINE AND COMPRESSOR EMPLOYING TUBERCLE LEADING EDGE ROTOR DESIGN
- 专利标题（中）： 涡轮机和压缩机OR 与HÖCKER前缘采用了一个转子VERSION
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申请号： EP05797075.8申请日： 2005-10-18
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公开(公告)号： EP1805412A1公开(公告)日： 2007-07-11
- 发明人: DEWAR, Stephen W. , WATTS, Philip , FISH, Frank Eliot
- 申请人： Whalepower Corporation
- 申请人地址： 27 Tyrrel Avenue Toronto, Ontario M6G 2G1 CA
- 专利权人： Whalepower Corporation
- 当前专利权人： Whalepower Corporation
- 当前专利权人地址： 27 Tyrrel Avenue Toronto, Ontario M6G 2G1 CA
- 代理机构： Naismith, Robert Stewart
- 优先权： US619002P 20041018
- 国际公布： WO2006042401 20060427
- 主分类号： F03B3/12
- IPC分类号： F03B3/12 ; F03D3/06 ; F03D11/00 ; H02K7/18
摘要：
A turbine/compressor comprises at least one magneto-electric device and a drive train coupled to the magneto-electric device. At least one rotor blade is coupled to the drive train. The rotor blade has a shaped leading edge with a series of spaced tubercles formed therealong.
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