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1. 发明授权

US08884456B2 Turbine unit and assembly 有权
标题翻译：涡轮机组和组装
公开(公告)号：US08884456B2
公开(公告)日：2014-11-11
申请号：US12445456
申请日：2007-10-05
申请人： Stephen Mark West , Steele West
发明人： Stephen Mark West , Steele West
IPC分类号： F03B13/00 , F03B13/10 , F03D1/02 , F03D1/04
CPC分类号： F03B13/10 , F03B13/105 , F03D1/025 , F03D1/04 , F03D9/25 , F03D9/28 , F05B2240/133 , F05B2240/97 , Y02E10/22 , Y02E10/72
摘要： A turbine unit (11) adapted to be placed in a flowing fluid. The turbine unit (11) comprises a first turbine set (13) and a second turbine set (15) mounted within a passage (21) of a housing (19). The first turbine blade set (13) and a second turbine blade set (15) are set in opposed relation such that in operation a region between the two turbine blade sets (13, 15) has a lower pressure than the fluid pressure at an opening of the passage (21). The turbine unit (11) being used to generate power. The turbine units (FIGS. 8 to 11) can be abutted with each other such that they define a passage and each turbine unit comprises a driving turbine blade set before fluid passes to a pumping turbine blade set.
摘要翻译：适于放置在流动流体中的涡轮单元（11）。涡轮单元（11）包括安装在壳体（19）的通道（21）内的第一涡轮机组（13）和第二涡轮机组（15）。第一涡轮叶片组（13）和第二涡轮叶片组（15）被设置成相对关系，使得在操作中，两个涡轮叶片组（13,15）之间的区域的压力低于开口处的流体压力通道（21）。涡轮单元（11）用于发电。涡轮机单元（图8至11）可以彼此邻接，使得它们限定通道，并且每个涡轮机单元包括在流体到泵送涡轮机叶片组之前设置的驱动涡轮机叶片。

2. 发明授权

US08358023B2 Driving turbine blade assembly comprising a passage through which a fluid may pass 有权
标题翻译：驱动涡轮叶片组件，其包括流体可以通过的通道
公开(公告)号：US08358023B2
公开(公告)日：2013-01-22
申请号：US12681363
申请日：2008-10-06
申请人： Stephen Mark West
发明人： Stephen Mark West
IPC分类号： F03B13/10
CPC分类号： F01D1/26 , F03B3/04 , F03D1/025 , F03D1/04 , F03D9/28 , F03D15/10 , F05B2240/133 , Y02E10/223 , Y02E10/72
摘要： A turbine unit (11) comprising a passage (23) through which a fluid may pass. Located within the passage (23) is a driving turbine blade set (25) upstream from a pumping turbine blade set (27) wherein the diameter of the pumping turbine blade is larger than the diameter of the driving turbine blade set. The driving turbine blade set and pumping turbine blade set are mounted in opposed relation whereby the turbine blade sets are in reversed orientation with respect to each other such that in simultaneous operation a region between the two turbine blade sets has a lower pressure than the fluid pressure at an opening of the passage. This induces a greater mass flow rate through the turbine unit than would otherwise be created by a pumping turbine blade set equal to or smaller in diameter than the driving turbine blade set.
摘要翻译：涡轮单元（11）包括流体可以通过的通道（23）。位于通道（23）内的是泵送涡轮叶片组（27）上游的驱动涡轮叶片组（25），其中泵送涡轮叶片的直径大于驱动涡轮叶片组的直径。驱动涡轮叶片组和泵送涡轮叶片组以相对的关系安装，由此涡轮叶片组相对于彼此处于相反的方向，使得在同时操作中，两个涡轮叶片组之间的区域具有比流体压力更低的压力在通道的开口。这导致通过涡轮机单元的质量流量比通过等于或小于驱动涡轮机叶片组的直径的泵送涡轮叶片组产生的质量流量更大。

3. 发明申请

US20100237620A1 TURBINE ASSEMBLY 有权
标题翻译：涡轮总成
公开(公告)号：US20100237620A1
公开(公告)日：2010-09-23
申请号：US12681363
申请日：2008-10-06
申请人： Stephen Mark West
发明人： Stephen Mark West
IPC分类号： H02K7/18 , F04B25/00 , F03B17/04
CPC分类号： F01D1/26 , F03B3/04 , F03D1/025 , F03D1/04 , F03D9/28 , F03D15/10 , F05B2240/133 , Y02E10/223 , Y02E10/72
摘要： A turbine unit (11) comprising a passage (23) through which a fluid may pass. Located within the passage (23) is a driving turbine blade set (25) upstream from a pumping turbine blade set (27) wherein the diameter of the pumping turbine blade is larger than the diameter of the driving turbine blade set. The driving turbine blade set and pumping turbine blade set are mounted in opposed relation whereby the turbine blade sets are in reversed orientation with respect to each other such that in simultaneous operation a region between the two turbine blade sets has a lower pressure than the fluid pressure at an opening of the passage. This induces a greater mass flow rate through the turbine unit than would otherwise be created by a pumping turbine blade set equal to or smaller in diameter than the driving turbine blade set.
摘要翻译：涡轮单元（11）包括流体可以通过的通道（23）。位于通道（23）内的是泵送涡轮叶片组（27）上游的驱动涡轮叶片组（25），其中泵送涡轮叶片的直径大于驱动涡轮叶片组的直径。驱动涡轮叶片组和泵送涡轮叶片组以相对的关系安装，由此涡轮叶片组相对于彼此处于相反的方向，使得在同时操作中，两个涡轮叶片组之间的区域具有比流体压力更低的压力在通道的开口。这导致通过涡轮机单元的质量流量比通过等于或小于驱动涡轮机叶片组的直径的泵送涡轮叶片组产生的质量流量更大。

4. 发明申请

US20100102566A1 TURBINE UNIT AND ASSEMBLY 有权
标题翻译：涡轮机组和组件
公开(公告)号：US20100102566A1
公开(公告)日：2010-04-29
申请号：US12445456
申请日：2007-10-05
申请人： Stephen Mark West , Steele West
发明人： Stephen Mark West , Steele West
IPC分类号： F03B13/00
CPC分类号： F03B13/10 , F03B13/105 , F03D1/025 , F03D1/04 , F03D9/25 , F03D9/28 , F05B2240/133 , F05B2240/97 , Y02E10/22 , Y02E10/72
摘要： A turbine unit (11) adapted to be placed in a flowing fluid. The turbine unit (11) comprises a first turbine set (13) and a second turbine set (15) mounted within a passage (21) of a housing (19). The first turbine blade set (13) and a second turbine blade set (15) are set in opposed relation such that in operation a region between the two turbine blade sets (13, 15) has a lower pressure than the fluid pressure at an opening of the passage (21). The turbine unit (11) being used to generate power. The turbine units (FIGS. 8 to 11) can be abutted with each other such that they define a passage and each turbine unit comprises a driving turbine blade set before fluid passes to a pumping turbine blade set.
摘要翻译：适于放置在流动流体中的涡轮单元（11）。涡轮单元（11）包括安装在壳体（19）的通道（21）内的第一涡轮机组（13）和第二涡轮机组（15）。第一涡轮叶片组（13）和第二涡轮叶片组（15）被设置成相对关系，使得在操作中，两个涡轮叶片组（13,15）之间的区域的压力低于开口处的流体压力通道（21）。涡轮单元（11）用于发电。涡轮机单元（图8至11）可以彼此邻接，使得它们限定通道，并且每个涡轮机单元包括在流体到泵送涡轮机叶片组之前设置的驱动涡轮机叶片。

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