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147 条记录 (耗时 0.03 秒)

    Fluid passages for power generation equipment
    32.
    发明授权
    Fluid passages for power generation equipment 有权

    公开(公告)号：US07022429B2

    公开(公告)日：2006-04-04

    申请号：US10063467

    申请日：2002-04-25

    申请人： Ronald Scott Bunker

    发明人： Ronald Scott Bunker

    IPC分类号： H01M8/00

    CPC分类号： H01M8/0267 ,  H01M8/0254 ,  H01M8/026 ,  H01M8/04007 ,  H01M2008/1293

    摘要： A solid oxide fuel cell is provided wherein the solid oxide fuel cell comprises a thermal management section and an electrolytic section disposed adjacent the thermal management section wherein a plurality of concavities are disposed on at least one of the thermal management and electrolytic sections so as to cause hydrodynamic interactions and affect the heat transfer rate between a fluid and the concavities when the fluid is disposed over the concavities.

    Fluid passages for power generation equipment
    33.
    发明授权
    Fluid passages for power generation equipment 有权
    用于发电设备的流体通道

    公开(公告)号：US07011904B2

    公开(公告)日：2006-03-14

    申请号：US10064605

    申请日：2002-07-30

    申请人： Ronald Scott Bunker

    发明人： Ronald Scott Bunker

    IPC分类号： H01M8/12

    CPC分类号： H01M8/04074 ,  H01M8/0269 ,  H01M8/04007

    摘要： A cooling apparatus for fuel cell components is provided wherein the cooling apparatus comprises a base plate having a first end and a second end and a first side plate coupled to the first end and a second side plate coupled to the second end. A plurality of bottom ribs are coupled to the base plate and a plurality of upper ribs are coupled to the bottom ribs. In addition, a top channel and a bottom channel are formed between each of the plurality of upper ribs and each of the plurality of bottom ribs, respectively, wherein the top channel and the bottom channel are disposed to allow a flow of a fluid therethrough and disposed to allow a portion of the fluid to alternate between the top channel and the bottom channel at a flow redirection area so as to enhance the heat transfer rate between the fluid and the fuel cell components.

    摘要翻译： 提供了一种用于燃料电池部件的冷却装置，其中冷却装置包括具有第一端和第二端的基板，以及联接到第一端的第一侧板和联接到第二端的第二侧板。 多个底肋连接到基板，并且多个上肋连接到底肋。 另外，顶部通道和底部通道分别形成在多个上部肋条中的每一个和多个底部肋条中的每一个之间，其中顶部通道和底部通道设置成允许流体流过其中， 设置成允许流体的一部分在流动重定向区域在顶部通道和底部通道之间交替，以便增强流体和燃料电池部件之间的传热速率。

    Turbine blade wall cooling apparatus and method of fabrication
    34.
    发明授权
    Turbine blade wall cooling apparatus and method of fabrication 失效
    涡轮叶片壁冷却装置及其制造方法

    公开(公告)号：US06695582B2

    公开(公告)日：2004-02-24

    申请号：US10162739

    申请日：2002-06-06

    申请人： Ronald Scott Bunker ,  Frederic Joseph Klug ,  Shyh-Chin Huang

    发明人： Ronald Scott Bunker ,  Frederic Joseph Klug ,  Shyh-Chin Huang

    IPC分类号： F01D518

    CPC分类号： F01D5/187 ,  F05D2240/126 ,  F05D2250/241 ,  F05D2250/314 ,  F05D2260/22141 ,  Y02T50/672 ,  Y02T50/673 ,  Y02T50/676

    摘要： A turbine blade comprises an external pressure side plate comprising a plurality of external pressure ribs, an internal pressure side plate comprising a plurality of internal pressure ribs, and a plurality of pressure flow redirection areas. The external pressure side plate is disposed over the internal pressure side plate to form a pressure side double wall. The external pressure ribs are disposed at a first angle with respect to a blade span reference line and the internal pressure ribs are disposed at a second angle with respect to the blade span reference line to form the pressure flow redirection areas. The pressure side double wall is configured to pass a coolant through the pressure side double wall. A fabrication method aligns the external pressure side plate and the internal pressure side plate to form the pressure flow redirection areas between the external pressure side plate and the internal pressure side plate.

    摘要翻译： 涡轮叶片包括包括多个外部压力肋的外部压力侧板，包括多个内部压力肋的内部压力侧板和多个压力流动重定向区域。 外压侧板设置在内压侧板上，形成压力侧双壁。 外部压力肋相对于叶片跨度基准线以第一角度设置，并且内部压力肋相对于叶片跨距基准线设置成第二角度以形成压力流动重定向区域。 压力侧双壁构造成使冷却剂通过压力侧双壁。 制造方法使外压侧板和内压侧板对准，以形成外压侧板和内压侧板之间的压力重定向区域。

    Turbine blade having a cooled tip shroud
    35.
    发明授权
    Turbine blade having a cooled tip shroud 有权

    公开(公告)号：US06506022B2

    公开(公告)日：2003-01-14

    申请号：US09681553

    申请日：2001-04-27

    申请人： Ronald Scott Bunker

    发明人： Ronald Scott Bunker

    IPC分类号： F01D518

    CPC分类号： F01D5/187 ,  F01D5/225 ,  F05D2230/21 ,  F05D2240/81 ,  F05D2260/22141 ,  Y02T50/673 ,  Y02T50/676

    摘要： A turbine blade having a cooled shroud comprises a blade attachment portion and a radially extended turbine airfoil integral with the blade attachment portion. The turbine airfoil has a plurality of cooling passages. A tip shroud is affixed to a top portion of the airfoil, the tip shroud having a plurality of circumferential cooling channels disposed substantially parallel to the rotation of the airfoil. Each circumferential cooling channel is in communication with a respective cooling passage and at least one exit port is in communication with at least one of the circumferential cooling channels.

    Cooling for double-wall structures
    36.
    发明授权
    Cooling for double-wall structures 失效
    双壁结构冷却

    公开(公告)号：US06000908A

    公开(公告)日：1999-12-14

    申请号：US744135

    申请日：1996-11-05

    申请人： Ronald Scott Bunker

    发明人： Ronald Scott Bunker

    IPC分类号： F01D5/18 ,  F01D9/06 ,  F01D25/12 ,  F01D25/14

    CPC分类号： F01D5/189 ,  F05D2250/241 ,  F05D2260/201 ,  Y02T50/676 ,  Y10S165/908

    摘要： A coolable double walled structure, for use and exposure in a hot gas flow environment, includes a jet issuing wall, a target wall spaced from the jet issuing wall defining at least one cavity therebetween. The jet issuing wall includes at least one impingement rail having a greater thickness than the jet issuing wall such that a bottom portion of the impingement rail extends within the cavity formed between the jet issuing wall and the target wall. A number of impingement ports are disposed within each impingement rail to provide flow communication through the jet issuing wall to the target wall. Due to the relatively thick dimensions of the impingement rail, the impingement ports disposed within respective impingement rails can be directionalized so as to provide for local cooling needs. In one embodiment, the entry areas of the impingement ports are bell shaped so as to lower inlet pressure loss. In another embodiment, the exit area immediately surrounding the impingement ports is rounded for lower post-impingement pressure drop.

    摘要翻译： 用于在热气流环境中使用和暴露的可冷却双壁结构包括喷射发射壁，与喷射发射壁间隔开的靶壁，其在其间限定至少一个腔。 喷射出口壁包括至少一个具有比喷射出口壁更大的厚度的冲击轨道，使得冲击轨道的底部在形成在喷射发射壁和目标壁之间的空腔内延伸。 多个冲击口设置在每个冲击轨道内以提供通过射流发射壁到目标壁的流动连通。 由于冲击轨道的尺寸相对较厚，所以设置在相应冲击轨道内的冲击口可被定向化，以便提供局部冷却需求。 在一个实施例中，冲击口的进入区域是钟形的，以便降低入口压力损失。 在另一个实施例中，紧邻冲击端口的出口区域是圆形的，用于较低的冲击后压降。

    Articles which include chevron film cooling holes, and related processes
    39.
    发明授权
    Articles which include chevron film cooling holes, and related processes 有权
    包括人字形薄膜冷却孔的文章及相关工艺

    公开(公告)号：US08905713B2

    公开(公告)日：2014-12-09

    申请号：US12790675

    申请日：2010-05-28

    申请人： Ronald Scott Bunker ,  Benjamin Paul Lacy

    发明人： Ronald Scott Bunker ,  Benjamin Paul Lacy

    IPC分类号： F01D5/18

    CPC分类号： F01D5/186 ,  F05D2230/10 ,  Y02T50/67 ,  Y02T50/672 ,  Y02T50/676 ,  Y10T29/49316

    摘要： An article is described, including an inner surface which can be exposed to a first fluid; an inlet; and an outer surface spaced from the inner surface, which can be exposed to a hotter second fluid. The article further includes at least one row or other pattern of passage holes. Each passage hole includes an inlet bore extending through the substrate from the inlet at the inner surface to a passage hole-exit proximate to the outer surface, with the inlet bore terminating in a chevron outlet adjacent the hole-exit. The chevron outlet includes a pair of wing troughs having a common surface region between them. The common surface region includes a valley which is adjacent the hole-exit; and a plateau adjacent the valley. The article can be an airfoil. Related methods for preparing the passage holes are also described.

    摘要翻译： 描述了一种制品，包括可暴露于第一流体的内表面; 一个入口 以及与内表面间隔开的外表面，其可以暴露于较热的第二流体。 该制品还包括至少一行或其它图案的通道孔。 每个通孔包括从内表面的入口延伸穿过基底的入口孔，靠近外表面的通道孔出口，入口孔终止于邻近孔出口的人字形出口。 人字形出口包括一对翼槽，它们之间具有共同的表面区域。 公共表面区域包括与孔出口相邻的谷部; 和毗邻山谷的高原。 文章可以是一个翼型。 还描述了制备通道孔的相关方法。

    Components with cooling channels and methods of manufacture
    40.
    发明授权
    Components with cooling channels and methods of manufacture 有权
    具有冷却通道和制造方法的部件

    公开(公告)号：US08727727B2

    公开(公告)日：2014-05-20

    申请号：US12965083

    申请日：2010-12-10

    申请人： Ronald Scott Bunker ,  Todd Garrett Wetzel

    发明人： Ronald Scott Bunker ,  Todd Garrett Wetzel

    IPC分类号： F01D5/18

    CPC分类号： F01D5/18 ,  F01D5/147 ,  F01D5/28 ,  F01D5/288 ,  F05D2260/202 ,  Y02T50/67 ,  Y02T50/672 ,  Y02T50/676

    摘要： A component is disclosed. The component includes a substrate comprising an outer surface and an inner surface. The inner surface defines at least one hollow, interior space, and the outer surface defines one or more grooves that extend at least partially along the outer substrate surface and have a respective base. One or more access holes are formed through the base of a respective groove, to connect the groove in fluid communication with the respective hollow interior space. The component further includes a coating comprising one or more layers disposed over at least a portion of the outer substrate surface. The groove(s) and the coating together define one or more channels for cooling the component. One or more trenches are formed through one or more coating layers and at least partially define at least one exit region for the cooling channel(s). A method of fabricating a component is also provided.

    摘要翻译： 公开了一个组件。 该组件包括包括外表面和内表面的基底。 内表面限定至少一个中空的内部空间，并且外表面限定一个或多个凹槽，其至少部分地沿着外部衬底表面延伸并且具有相应的底座。 通过相应凹槽的基部形成一个或多个通孔，以将凹槽与相应的中空内部空间流体连通。 该组件还包括涂层，其包括设置在外基材表面的至少一部分上的一层或多层。 凹槽和涂层一起限定一个或多个通道以冷却部件。 一个或多个沟槽通过一个或多个涂层形成，并且至少部分地限定用于冷却通道的至少一个出口区域。 还提供了一种制造部件的方法。