专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20130236299A1 TUBULAR HEAT EXCHANGE SYSTEMS 有权
标题翻译：管式热交换系统
公开(公告)号：US20130236299A1
公开(公告)日：2013-09-12
申请号：US13412761
申请日：2012-03-06
申请人： Harry Lester Kington , Mark C. Morris , Donald G. Godfrey , John Meier , Charles Lo
发明人： Harry Lester Kington , Mark C. Morris , Donald G. Godfrey , John Meier , Charles Lo
IPC分类号： F28F9/02 , B23K26/00 , F01D25/12 , F28F13/12
CPC分类号： F28F9/0263 , B22F3/1055 , B22F2998/10 , B33Y80/00 , F02C7/08 , F02C7/10 , F05D2260/213 , F28D7/1669 , F28D21/001 , F28F9/0282 , F28F9/26 , F28F13/125 , Y02P10/295 , Y02T50/675 , B22F2003/247 , B22F2003/248 , B22F3/15
摘要： A heat exchange system includes a first flow passage and a second flow passage. The heat exchange system is configured to transfer heat between a first fluid flowing through the first flow passage and a second fluid flowing through the second flow passage. The first flow passage includes an inlet header, a plurality of tubes, and an outlet header. The inlet header includes a plurality of header-tube transition portions configured to allow the first fluid to flow from the inlet header and into the tubes, the plurality of header-tube transition portions each including a smoothly curved inlet portion and a tapered tube connection portion.
摘要翻译：热交换系统包括第一流动通道和第二流动通道。热交换系统被配置为在流过第一流动通道的第一流体和流过第二流动通道的第二流体之间传递热量。第一流动通道包括入口集管，多个管和出口集管。入口集管包括多个集流管过渡部分，其被构造成允许第一流体从入口集管流入管中，多个集流管过渡部分各自包括平滑弯曲的入口部分和锥形管连接部分。

2. 发明授权

US09200855B2 Tubular heat exchange systems 有权
标题翻译：管式热交换系统
公开(公告)号：US09200855B2
公开(公告)日：2015-12-01
申请号：US13412761
申请日：2012-03-06
申请人： Harry Lester Kington , Mark C. Morris , Donald G. Godfrey , John Meier , Charles Lo
发明人： Harry Lester Kington , Mark C. Morris , Donald G. Godfrey , John Meier , Charles Lo
IPC分类号： F28F9/02 , F28F13/12 , F02C7/08 , F28F9/26 , F28D7/16 , F28D21/00 , F02C7/10
CPC分类号： F28F9/0263 , B22F3/1055 , B22F2998/10 , B33Y80/00 , F02C7/08 , F02C7/10 , F05D2260/213 , F28D7/1669 , F28D21/001 , F28F9/0282 , F28F9/26 , F28F13/125 , Y02P10/295 , Y02T50/675 , B22F2003/247 , B22F2003/248 , B22F3/15
摘要： A heat exchange system includes a first flow passage and a second flow passage. The heat exchange system is configured to transfer heat between a first fluid flowing through the first flow passage and a second fluid flowing through the second flow passage. The first flow passage includes an inlet header, a plurality of tubes, and an outlet header. The inlet header includes a plurality of header-tube transition portions configured to allow the first fluid to flow from the inlet header and into the tubes, the plurality of header-tube transition portions each including a smoothly curved inlet portion and a tapered tube connection portion.
摘要翻译：热交换系统包括第一流动通道和第二流动通道。热交换系统被配置为在流过第一流动通道的第一流体和流过第二流动通道的第二流体之间传递热量。第一流动通道包括入口集管，多个管和出口集管。入口集管包括多个集流管过渡部分，其被构造成允许第一流体从入口集管流入管中，多个集流管过渡部分各自包括平滑弯曲的入口部分和锥形管连接部分。

3. 发明申请

US20140079540A1 TURBINE STATOR AIRFOIL ASSEMBLIES AND METHODS FOR THEIR MANUFACTURE 有权
标题翻译：涡轮机定子机组件及其制造方法
公开(公告)号：US20140079540A1
公开(公告)日：2014-03-20
申请号：US13621845
申请日：2012-09-17
申请人： Mark C. Morris , Donald G. Godfrey , Harry Lester Kington
发明人： Mark C. Morris , Donald G. Godfrey , Harry Lester Kington
IPC分类号： B23P15/02 , B22F7/04 , B22F3/105 , F01D9/02
CPC分类号： B22F3/1055 , B22F5/04 , B33Y80/00 , F01D5/147 , F01D5/187 , F01D5/189 , F01D9/02 , F01D9/041 , F01D9/065 , F05D2230/22 , F05D2230/31 , F05D2260/20 , Y02P10/295 , Y02T50/676 , Y10T29/49323
摘要： In accordance with an exemplary embodiment, a method of manufacturing a stator airfoil assembly includes forming an interior wall of a stator airfoil using an additive manufacturing technique, forming an exterior wall of the stator airfoil using the additive manufacturing technique, and forming a plurality of internal ribs between the interior wall and the exterior wall using the additive manufacturing technique. A cooling air circuit is formed in a space between the interior wall and the exterior wall. Further, the interior wall, the exterior wall, and the internal ribs are formed simultaneously as an integral structure by using the additive manufacturing technique.
摘要翻译：根据示例性实施例，制造定子翼型组件的方法包括使用添加剂制造技术形成定子翼型件的内壁，使用添加剂制造技术形成定子翼型件的外壁，以及形成多个内部使用添加剂制造技术在内壁和外壁之间的肋条。在内壁和外壁之间的空间中形成冷却空气回路。此外，通过使用添加剂制造技术，内壁，外壁和内肋同时形成为整体结构。

4. 发明申请

US20140037983A1 TITANIUM ALUMINIDE COMPONENTS AND METHODS FOR MANUFACTURING THE SAME FROM ARTICLES FORMED BY CONSOLIDATION PROCESSES 有权
标题翻译：钛白粉组分及其制备方法从合成工艺形成的制品
公开(公告)号：US20140037983A1
公开(公告)日：2014-02-06
申请号：US13564656
申请日：2012-08-01
申请人： Donald G. Godfrey , Mark C. Morris , George Reimer , William F. Hehmann , Daira Legzdina , Richard Fox , Yiping Hu , Harry Lester Kington
发明人： Donald G. Godfrey , Mark C. Morris , George Reimer , William F. Hehmann , Daira Legzdina , Richard Fox , Yiping Hu , Harry Lester Kington
IPC分类号： B05D7/14 , B05D3/12 , C23C14/34 , C23C16/48 , C23C4/12 , C23C14/35 , B32B15/01 , C23C16/06
CPC分类号： B22F3/1266 , B22F3/1055 , B22F3/15 , B33Y70/00 , B33Y80/00 , C22C1/0491 , C23C10/48 , C23C10/60 , C23C14/16 , Y02P10/295 , Y10T428/12764
摘要： Substantially defect-free titanium aluminide components and methods are provided for manufacturing the same from articles formed by consolidation processes. The method includes providing an intermediate article comprised of a titanium aluminide alloy and formed by a consolidation process. The intermediate article is encapsulated with an aluminum-containing encapsulation layer. The intermediate article is compacted after the encapsulation step. A substantially defect-free titanium aluminide component comprises a compacted three-dimensional article comprised of titanium aluminide and formed by a consolidation process and an aluminum-containing encapsulation layer on at least one surface of the compacted three-dimensional article. The aluminum-containing encapsulation layer comprises an aluminide material, MCrAlY wherein M is cobalt, nickel, or a combination of cobalt and nickel, or TiAlCr.
摘要翻译：提供了基本上无缺陷的钛铝化合物组分和方法，用于通过固化方法形成的制品来制造它们。该方法包括提供由钛化铝合金构成的中间制品，并通过固结方法形成。中间制品用含铝封装层包封。中间制品在封装步骤之后被压实。基本上无缺陷的钛铝化物组分包括由铝化钛组成的压实的三维制品，并且通过固结方法形成，并且在压实的三维制品的至少一个表面上包含含铝封装层。含铝封装层包括铝化物材料MCrAlY，其中M是钴，镍或钴和镍的组合，或TiAlCr。

5. 发明授权

US09289826B2 Turbine stator airfoil assemblies and methods for their manufacture 有权
标题翻译：涡轮机定子翼型组件及其制造方法
公开(公告)号：US09289826B2
公开(公告)日：2016-03-22
申请号：US13621845
申请日：2012-09-17
申请人： Mark C. Morris , Donald G. Godfrey , Harry Lester Kington
发明人： Mark C. Morris , Donald G. Godfrey , Harry Lester Kington
IPC分类号： F01D9/02 , B22F3/105 , F01D5/18 , B22F5/04 , F01D5/14 , F01D9/04 , F01D9/06
CPC分类号： B22F3/1055 , B22F5/04 , B33Y80/00 , F01D5/147 , F01D5/187 , F01D5/189 , F01D9/02 , F01D9/041 , F01D9/065 , F05D2230/22 , F05D2230/31 , F05D2260/20 , Y02P10/295 , Y02T50/676 , Y10T29/49323
摘要： In accordance with an exemplary embodiment, a method of manufacturing a stator airfoil assembly includes forming an interior wall of a stator airfoil using an additive manufacturing technique, forming an exterior wall of the stator airfoil using the additive manufacturing technique, and forming a plurality of internal ribs between the interior wall and the exterior wall using the additive manufacturing technique. A cooling air circuit is formed in a space between the interior wall and the exterior wall. Further, the interior wall, the exterior wall, and the internal ribs are formed simultaneously as an integral structure by using the additive manufacturing technique.
摘要翻译：根据示例性实施例，制造定子翼型组件的方法包括使用添加剂制造技术形成定子翼型件的内壁，使用添加剂制造技术形成定子翼型件的外壁，以及形成多个内部使用添加剂制造技术在内壁和外壁之间的肋条。在内壁和外壁之间的空间中形成冷却空气回路。此外，通过使用添加剂制造技术，内壁，外壁和内肋同时形成为整体结构。

6. 发明授权

US09120151B2 Methods for manufacturing titanium aluminide components from articles formed by consolidation processes 有权
标题翻译：从固结过程形成的制品中制备铝化铝组分的方法
公开(公告)号：US09120151B2
公开(公告)日：2015-09-01
申请号：US13564656
申请日：2012-08-01
申请人： Donald G. Godfrey , Mark C. Morris , George Reimer , William F. Hehmann , Daira Legzdina , Richard Fox , Yiping Hu , Harry Lester Kington
发明人： Donald G. Godfrey , Mark C. Morris , George Reimer , William F. Hehmann , Daira Legzdina , Richard Fox , Yiping Hu , Harry Lester Kington
IPC分类号： C23C16/06 , C23C16/48 , B05D3/12 , B05D7/14 , B22F3/12 , B22F3/15 , C23C10/48 , C23C10/60 , C22C1/04 , C23C14/16 , B22F3/105
CPC分类号： B22F3/1266 , B22F3/1055 , B22F3/15 , B33Y70/00 , B33Y80/00 , C22C1/0491 , C23C10/48 , C23C10/60 , C23C14/16 , Y02P10/295 , Y10T428/12764
摘要： Substantially defect-free titanium aluminide components and methods are provided for manufacturing the same from articles formed by consolidation processes. The method includes providing an intermediate article comprised of a titanium aluminide alloy and formed by a consolidation process. The intermediate article is encapsulated with an aluminum-containing encapsulation layer. The intermediate article is compacted after the encapsulation step. A substantially defect-free titanium aluminide component comprises a compacted three-dimensional article comprised of titanium aluminide and formed by a consolidation process and an aluminum-containing encapsulation layer on at least one surface of the compacted three-dimensional article. The aluminum-containing encapsulation layer comprises an aluminide material, MCrAlY wherein M is cobalt, nickel, or a combination of cobalt and nickel, or TiAlCr.
摘要翻译：提供了基本上无缺陷的钛铝化合物组分和方法，用于通过固化方法形成的制品来制造它们。该方法包括提供由钛化铝合金构成的中间制品，并通过固结方法形成。中间制品用含铝封装层包封。中间制品在封装步骤之后被压实。基本上无缺陷的钛铝化物组分包括由铝化钛组成的压实的三维制品，并且通过固结方法形成，并且在压实的三维制品的至少一个表面上包含含铝封装层。含铝封装层包括铝化物材料MCrAlY，其中M是钴，镍或钴和镍的组合，或TiAlCr。

7. 发明授权

US08434543B2 Method of making turbine stator airfoils with individual orientations 失效
标题翻译：制造具有各个方位的涡轮机定子翼型的方法
公开(公告)号：US08434543B2
公开(公告)日：2013-05-07
申请号：US12500453
申请日：2009-07-09
申请人： Mark C. Morris , Harry Lester Kington , James Neumann
发明人： Mark C. Morris , Harry Lester Kington , James Neumann
IPC分类号： B22D46/00 , B22D27/04
CPC分类号： F01D9/00 , F01D5/284 , F01D9/041 , F05D2300/606 , Y02T50/673
摘要： In accordance with an exemplary embodiment, a turbine stator component includes a first endwall; a second endwall; a first stator airfoil coupled between the first and second endwalls; and a second stator airfoil adjacent to the first airfoil and coupled between the first and second endwalls. The first stator airfoil has first crystallographic primary and secondary orientations. The second stator airfoil has second crystallographic primary and secondary orientations, the first crystallographic primary and secondary orientations being different from the second crystallographic primary and secondary orientations.
摘要翻译：根据示例性实施例，涡轮机定子部件包括第一端壁; 第二端壁耦合在第一和第二端壁之间的第一定子翼型件; 以及与第一翼型件相邻并且连接在第一和第二端壁之间的第二定子翼型件。第一定子翼型件具有第一晶体初级和次级方向。第二定子翼型具有第二晶体初级和次级取向，第一晶体初级和次级取向不同于第二晶体初级和次级取向。

8. 发明申请

US20100126276A1 METHOD FOR DETECTING DEVIATION IN CRYSTALLOGRAPHIC ORIENTATION IN A METAL STRUCTURE 有权
标题翻译：用于检测金属结构中晶体取向偏差的方法
公开(公告)号：US20100126276A1
公开(公告)日：2010-05-27
申请号：US12276969
申请日：2008-11-24
申请人： Harry Lester Kington , Surendra Singh , Mark C. Morris
发明人： Harry Lester Kington , Surendra Singh , Mark C. Morris
IPC分类号： G01H5/00
CPC分类号： G01H5/00
摘要： A method of detecting a deviation angle in a single-crystal metal structure is disclosed. The single-crystal metal structure has a crystallographic orientation, a length, a first side, a second side, and a first axis extending through the structure. The method comprises determining the length of the single-crystal metal structure along the first axis, transmitting a signal through the single-crystal metal structure from the first side, the signal oriented to propagate along the first axis, receiving the signal, determining a time-of-flight for the signal to traverse the length from the first side to the second side, determining a speed of the signal based on the time-of-flight and the length, and comparing the speed of the signal to a reference speed to detect the deviation angle.
摘要翻译：公开了一种在单晶金属结构中检测偏斜角的方法。单晶金属结构具有晶体取向，长度，第一侧，第二侧和延伸穿过该结构的第一轴。该方法包括：沿着第一轴确定单晶金属结构的长度，从第一侧传输通过单晶金属结构的信号，所述信号被定向为沿着第一轴传播，接收信号，确定时间用于使信号从第一侧到第二侧的长度穿过，基于飞行时间和长度确定信号的速度，并将信号的速度与参考速度比较为检测偏角。

9. 发明授权

US07946177B2 Method for detecting deviation in crystallographic orientation in a metal structure 有权
标题翻译：用于检测金属结构中晶体取向偏差的方法
公开(公告)号：US07946177B2
公开(公告)日：2011-05-24
申请号：US12276969
申请日：2008-11-24
申请人： Harry Lester Kington , Surendra Singh , Mark C. Morris
发明人： Harry Lester Kington , Surendra Singh , Mark C. Morris
IPC分类号： G01H5/00
CPC分类号： G01H5/00
摘要： A method of detecting a deviation angle in a single-crystal metal structure is disclosed. The single-crystal metal structure has a crystallographic orientation, a length, a first side, a second side, and a first axis extending through the structure. The method comprises determining the length of the single-crystal metal structure along the first axis, transmitting a signal through the single-crystal metal structure from the first side, the signal oriented to propagate along the first axis, receiving the signal, determining a time-of-flight for the signal to traverse the length from the first side to the second side, determining a speed of the signal based on the time-of-flight and the length, and comparing the speed of the signal to a reference speed to detect the deviation angle.
摘要翻译：公开了一种在单晶金属结构中检测偏斜角的方法。单晶金属结构具有晶体取向，长度，第一侧，第二侧和延伸穿过该结构的第一轴。该方法包括：沿着第一轴确定单晶金属结构的长度，从第一侧传输通过单晶金属结构的信号，所述信号被定向为沿着第一轴传播，接收信号，确定时间用于使信号从第一侧到第二侧的长度穿过，基于飞行时间和长度确定信号的速度，并将信号的速度与参考速度比较为检测偏角。

10. 发明申请

US20110008157A1 TURBINE STATOR AIRFOILS WITH INDIVIDUAL ORIENTATIONS 失效
标题翻译：具有个体定位的涡轮机定子机构
公开(公告)号：US20110008157A1
公开(公告)日：2011-01-13
申请号：US12500453
申请日：2009-07-09
申请人： Mark C. Morris , Harry Lester Kington , James Neumann
发明人： Mark C. Morris , Harry Lester Kington , James Neumann
IPC分类号： F01D9/04 , G06F19/00 , G06F17/50
CPC分类号： F01D9/00 , F01D5/284 , F01D9/041 , F05D2300/606 , Y02T50/673
摘要： In accordance with an exemplary embodiment, a turbine stator component includes a first endwall; a second endwall; a first stator airfoil coupled between the first and second endwalls; and a second stator airfoil adjacent to the first airfoil and coupled between the first and second endwalls. The first stator airfoil has first crystallographic primary and secondary orientations. The second stator airfoil has second crystallographic primary and secondary orientations, the first crystallographic primary and secondary orientations being different from the second crystallographic primary and secondary orientations.
摘要翻译：根据示例性实施例，涡轮机定子部件包括第一端壁; 第二端壁耦合在第一和第二端壁之间的第一定子翼型件; 以及与第一翼型件相邻并且连接在第一和第二端壁之间的第二定子翼型件。第一定子翼型件具有第一晶体初级和次级取向。第二定子翼型具有第二晶体初级和次级取向，第一晶体初级和次级取向不同于第二晶体初级和次级取向。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式