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1. 发明授权

EP2497944B1 System and method of manipulating a boundary layer across a rotor blade of a wind turbine 有权
标题翻译：的系统和方法的边界层的处理上的风力涡轮机的叶片
公开(公告)号：EP2497944B1
公开(公告)日：2014-08-13
申请号：EP11194546.5
申请日：2011-12-20
申请人： General Electric Company
发明人： Bhaisora, Shailesh Singh , Shastri, Narasimha , Gupta, Anurag
IPC分类号： F03D7/04 , F03D1/06 , F03D7/02 , F15D1/12
CPC分类号： F03D1/065 , F03D1/0633 , F03D7/022 , F03D7/04 , F05B2240/122 , F05B2260/60 , F05B2270/32 , F15D1/12 , Y02E10/721 , Y02E10/723

2. 发明公开

EP2497944A1 System and method of manipulating a boundary layer across a rotor blade of a wind turbine 有权
标题翻译：的系统和方法的边界层的处理上的风力涡轮机的叶片
公开(公告)号：EP2497944A1
公开(公告)日：2012-09-12
申请号：EP11194546.5
申请日：2011-12-20
申请人： General Electric Company
发明人： Bhaisora, Shailesh Singh , Shastri, Narasimha , Gupta, Anurag
IPC分类号： F03D1/06 , F03D7/04 , F03D7/02
CPC分类号： F03D1/065 , F03D1/0633 , F03D7/022 , F03D7/04 , F05B2240/122 , F05B2260/60 , F05B2270/32 , F15D1/12 , Y02E10/721 , Y02E10/723
摘要： An air distribution system (30) for manipulating a boundary layer (76) of air across a wind turbine rotor blade (28), the wind turbine rotor blade having at least one sidewall (54) defining a cavity (60) therein, the sidewall extending between a leading edge (66) and an axially spaced trailing edge (68) and defining a chordwise axis (44) between the leading edge and the trailing edge is provided. The air distribution system includes a plurality of bleed flow assemblies (84) positioned within the rotor blade and configured to discharge air into the boundary layer to reduce a separation of the boundary layer from the rotor blade. Each bleed flow assembly of the plurality of bleed flow assemblies include a bleed flow conduit (90) coupled to an inner surface (92) of the sidewall and oriented with respect to the chordwise axis between the leading edge and the trailing edge, the bleed flow conduit configured to channel air through the rotor blade, an inlet aperture (86) defined through the bleed flow conduit and through the sidewall to channel air into the bleed flow conduit, and an outlet aperture (88) defined through the bleed flow conduit and through the sidewall to discharge air from the bleed flow conduit and into the boundary layer.
摘要翻译：用于跨越风力涡轮机转子叶片（28）操纵的空气的边界层（76）的空气分配系统（30），具有至少一个侧壁（54）的风力涡轮机转子叶片。其中 - 定义一个腔（60），所述侧壁在轴向间隔开的后缘（68）和定义所述前缘和后缘之间的弦向轴线（44）的前缘（66）之间并延伸设置。该空气分配系统包括在转子叶片内定位和配置将空气排出到所述边界层，以减少从转子叶片的边界层的分离泄流组件（84）的复数。泄流组件的多个各泄流组件包括耦合到所述侧壁的内表面（92）和取向为相对于所述前缘和后缘，所述泄放流之间的弦向轴线的泄流管道（90）导管被配置为通过在通过泄流管道并穿过侧壁限定成引导空气进入泄流管道入口孔（86）的转子叶片成引导空气，并且在出口孔（88）通过该泄流管道，并通过定义侧壁从泄流管道并进入边界层排出空气。

3. 发明公开

EP1643116A2 System and method for reducing emission from a combustion engine 审中-公开
标题翻译：系统和Verfahren zur Verminderung von Emissionen einer Brennkraftmaschine
公开(公告)号：EP1643116A2
公开(公告)日：2006-04-05
申请号：EP05256090.1
申请日：2005-09-29
申请人： GENERAL ELECTRIC COMPANY
发明人： Bhaisora, Shailesh Singh , Gudlavalleti, Sauri , Bowman, Michael John
IPC分类号： F02M25/10 , F02D19/08
CPC分类号： F02M25/10 , C01B3/366 , C01B2203/0255 , F02D19/0644 , F02D19/0671 , F02D19/081 , Y02T10/121 , Y02T10/36
摘要： A combustion engine system (10) comprises a plurality of cylinders (30) configured to combust a mixed fuel (16) to produce an exhaust gas (34) and at least one reforming cylinder (24) configured to receive a first portion of a fuel (22) and deliver a reformed hydrogen-containing gas (26). The hydrogen-containing gas (26) is introduced into a second portion of the fuel (14) to form the mixed fuel (16) to reduce emission from the combustion engine system (10).
摘要翻译：内燃机系统（10）包括多个气缸（30），其构造成燃烧混合燃料（16）以产生废气（34）和至少一个重整气缸（24），其被构造成容纳燃料的第一部分（22）并输送重整的含氢气体（26）。含氢气体（26）被引入到燃料（14）的第二部分中以形成混合燃料（16）以减少来自内燃机系统（10）的排放。

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