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1. 发明授权

US09920625B2 Turbine blade with laterally biased airfoil and platform centers of mass 有权
公开(公告)号：US09920625B2
公开(公告)日：2018-03-20
申请号：US13005733
申请日：2011-01-13
申请人： Christopher Rawlings , Robert M. Dysert , Billie E. Sealey , Jose Paulino , Anthony J. Malandra
发明人： Christopher Rawlings , Robert M. Dysert , Billie E. Sealey , Jose Paulino , Anthony J. Malandra
IPC分类号： F01D5/14 , F01D5/02
CPC分类号： F01D5/027 , F01D5/147 , F05D2260/15 , F05D2260/961
摘要： A turbine blade airfoil (32) with a center of mass (ACM) that is laterally offset from the center of mass (PCM) of a platform (42) to which the airfoil is attached. Respective offsets (da, dp) balance these centers of mass (ACM, PCM) about an attachment plane (64) of the blade root (30), providing balanced centrifugal loading on opposite lobes (51, 52) or other attachment surfaces of the root. The attachment plane (64) may be a plane of bilateral symmetry of the root, and/or it may include an attachment axis (65) that passes through the root center of mass (RCM) along a radius of rotation of the airfoil. The airfoil and platform centers of mass (ACM, PCM) may be dynamically balanced about the attachment axis (65) and/or the attachment plane (64).

2. 发明申请

US20080141531A1 Non-stablug stator apparatus and assembly method 有权
标题翻译：非固定式定子设备及装配方法
公开(公告)号：US20080141531A1
公开(公告)日：2008-06-19
申请号：US11641349
申请日：2006-12-19
申请人： Jose Paulino , Mark Rogers , Charles H. Warner , Steven D. Jenkel , Kurt R. Heinemann , Steven R. Chabot , Chester D. Blackman , Paul S. Bean
发明人： Jose Paulino , Mark Rogers , Charles H. Warner , Steven D. Jenkel , Kurt R. Heinemann , Steven R. Chabot , Chester D. Blackman , Paul S. Bean
IPC分类号： F01D9/00 , B21K25/00
CPC分类号： F01D9/044 , B23K15/0006 , B23K15/0046 , B23K2101/001 , F05D2230/237 , F05D2240/12 , Y10T29/49323
摘要： A method of assembling a stator apparatus includes providing a first vane having an airfoil section located between a first platform section and a second platform section, positioning a first shroud ring adjacent to the first vane, welding the first platform section of the first vane to the first shroud ring relative to a first edge of the of the first platform section of the first vane, and welding the first platform section of the first vane to the first shroud ring relative to a second edge of the of the first platform section. The second edge is located opposite the first edge.
摘要翻译：一种组装定子装置的方法包括提供具有位于第一平台部分和第二平台部分之间的翼型部分的第一叶片，将第一护罩环定位成与第一叶片相邻，将第一叶片的第一平台部分焊接到相对于第一叶片的第一平台部分的第一边缘的第一护罩环，并且相对于第一平台部分的第二边缘将第一叶片的第一平台部分焊接到第一护罩环。第二边缘位于第一边缘的对面。

3. 发明申请

US20120269649A1 TURBINE BLADE WITH IMPROVED TRAILING EDGE COOLING 审中-公开
标题翻译：涡轮叶片改进后跟边缘冷却
公开(公告)号：US20120269649A1
公开(公告)日：2012-10-25
申请号：US13092312
申请日：2011-04-22
申请人： Christopher Rawlings , Robert M. Dysert , Billie E. Sealey , Jose Paulino , Anthony J. Malandra
发明人： Christopher Rawlings , Robert M. Dysert , Billie E. Sealey , Jose Paulino , Anthony J. Malandra
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F05D2210/33 , F05D2240/127 , F05D2250/185 , F05D2260/2212
摘要： A turbine blade (110) is provided, where an exterior surface of the turbine blade (110) is exposed to a hot combustion gas (125) above a flow path line (141). The turbine blade (110) includes a trailing edge pin bank cooling channel (118) in an airfoil section (112), a cooling air supply channel (120) in a root section (114), and a channel (122) shaped with a radius of curvature (126), to extend the channel (122) across the flow path line (141) and interconnect the cooling air supply channel (120) to the trailing edge pin bank cooling channel (118). A width of the trailing edge pin bank cooling channel (118) is adjusted, such that the width at an inner diameter region (128) and an outer diameter region (131) is less than the width at an intermediate region (130) between the inner and outer diameter regions (128,131).
摘要翻译：提供了一种涡轮机叶片（110），其中涡轮机叶片（110）的外表面暴露于流动路线（141）上方的热燃烧气体（125）。涡轮叶片（110）包括翼型部分（112）中的后缘销组冷却通道（118），根部部分（114）中的冷却空气供应通道（120）和形成有曲率半径（126），以使通道（122）跨过流动路径（141）延伸，并将冷却空气供应通道（120）与后缘销钉组冷却通道（118）互连。调节后缘销组排冷却通道（118）的宽度，使得内径区域（128）和外径区域（131）处的宽度小于中间区域（130）之间的宽度，内外径区域（128,131）。

4. 发明授权

US08016297B2 Gas turbine engine seals and engines incorporating such seals 有权
标题翻译：燃气涡轮发动机密封件和包含这种密封件的发动机
公开(公告)号：US08016297B2
公开(公告)日：2011-09-13
申请号：US12056792
申请日：2008-03-27
申请人： Kurt R. Heinemann , Jose Paulino , Scot A. Webb , Mark Ring , Charles H. Warner
发明人： Kurt R. Heinemann , Jose Paulino , Scot A. Webb , Mark Ring , Charles H. Warner
IPC分类号： F16J15/02
CPC分类号： F01D11/005
摘要： Gas turbine engine seals and engines incorporating such seals are provided. In this regard, a representative seal includes: an annular seal body having an inner diameter and an outer diameter, the seal body extending along an axis of symmetry between a first end and a second end; the seal body being formed of a strip of material having first and second opposing edges, the strip of material being deformed to exhibit a first sealing surface at the first end, a second sealing surface at the second end, and a third sealing surface along the inner diameter, the first edge being located adjacent to the third sealing surface, the second edge being located adjacent to the second sealing surface; the first edge being spaced from the second edge to define an annular opening, the annular opening providing access to an annular cavity of the seal body.
摘要翻译：提供了包括这种密封件的燃气涡轮发动机密封件和发动机。在这方面，代表性的密封件包括：具有内径和外径的环形密封体，密封体沿第一端和第二端之间的对称轴延伸; 所述密封体由具有第一和第二相对边缘的材料条形成，所述材料条变形以在第一端处呈现第一密封表面，在第二端处具有第二密封表面，以及沿着所述第二密封表面的第三密封表面所述第一边缘邻近所述第三密封表面定位，所述第二边缘邻近所述第二密封表面定位; 所述第一边缘与所述第二边缘间隔开以限定环形开口，所述环形开口提供对所述密封体的环形腔的通路。

5. 发明申请

US20120183405A1 TURBINE BLADE WITH LATERALLY BIASED AIRFOIL AND PLATFORM CENTERS OF MASS 有权
标题翻译：涡轮叶片具有横向偏置的飞机和平台中心的质量
公开(公告)号：US20120183405A1
公开(公告)日：2012-07-19
申请号：US13005733
申请日：2011-01-13
申请人： Christopher Rawlings , Robert M. Dysert , Billie E. Sealey , Jose Paulino , Anthony J. Malandra
发明人： Christopher Rawlings , Robert M. Dysert , Billie E. Sealey , Jose Paulino , Anthony J. Malandra
IPC分类号： F01D5/14
CPC分类号： F01D5/027 , F01D5/147 , F05D2260/15 , F05D2260/961
摘要： A turbine blade airfoil (32) with a center of mass (ACM) that is laterally offset from the center of mass (PCM) of a platform (42) to which the airfoil is attached. Respective offsets (da, dp) balance these centers of mass (ACM, PCM) about an attachment plane (64) of the blade root (30), providing balanced centrifugal loading on opposite lobes (51, 52) or other attachment surfaces of the root. The attachment plane (64) may be a plane of bilateral symmetry of the root, and/or it may include an attachment axis (65) that passes through the root center of mass (RCM) along a radius of rotation of the airfoil. The airfoil and platform centers of mass (ACM, PCM) may be dynamically balanced about the attachment axis (65) and/or the attachment plane (64).
摘要翻译：具有中心质量（ACM）的涡轮叶片翼型件（32），其横向偏离所述翼型件附接到所述平台（42）的质心（PCM）。相应的偏移量（da，dp）围绕叶片根部（30）的附接平面（64）平衡这些质心（ACM，PCM），从而在相对的叶片（51,52）或其他附接表面根。附接平面（64）可以是根部的双侧对称的平面，和/或其可以包括沿着翼型的旋转半径穿过根质心（RCM）的附接轴线（65）。翼型和平台质心（ACM，PCM）可围绕附接轴线（65）和/或附接平面（64）动态平衡。

6. 发明授权

US07819622B2 Method for securing a stator assembly 有权
标题翻译：固定定子组件的方法
公开(公告)号：US07819622B2
公开(公告)日：2010-10-26
申请号：US11641326
申请日：2006-12-19
申请人： Jose Paulino , Richard K. Hayford
发明人： Jose Paulino , Richard K. Hayford
IPC分类号： F01D9/04
CPC分类号： F01D25/246 , F01D9/041 , F01D11/005 , F05D2230/642
摘要： An example exit guide vane for a gas turbine engine is mounted adjacent to a diffuser case defining an air flow path. A thrust balance seal is attached to the diffuser and the exit guide vane is mounted adjacent the diffuser case for guiding air flow into the air flow path. The exit guide vane is mounted adjacent to the diffuser without interfering with the air flow path or restricting thermal expansion.
摘要翻译：用于燃气涡轮发动机的示例性出口导叶安装在限定空气流动路径的扩散器壳体附近。推力平衡密封件附接到扩散器，并且出口导向叶片安装在扩散器壳体附近，用于引导空气流入空气流动路径。出口导向叶片与扩散器相邻地安装，而不干扰空气流动路径或限制热膨胀。

7. 发明授权

US07748956B2 Non-stablug stator apparatus and assembly method 有权
标题翻译：非固定式定子设备及装配方法
公开(公告)号：US07748956B2
公开(公告)日：2010-07-06
申请号：US11641349
申请日：2006-12-19
申请人： Jose Paulino , Mark Rogers , Charles H. Warner , Steven D. Jenkel , Kurt R. Heinemann , Steven R. Chabot , Chester D. Blackman, Jr. , Paul S. Bean, Jr.
发明人： Jose Paulino , Mark Rogers , Charles H. Warner , Steven D. Jenkel , Kurt R. Heinemann , Steven R. Chabot , Chester D. Blackman, Jr. , Paul S. Bean, Jr.
IPC分类号： F01D9/02
CPC分类号： F01D9/044 , B23K15/0006 , B23K15/0046 , B23K2101/001 , F05D2230/237 , F05D2240/12 , Y10T29/49323
摘要： A method of assembling a stator apparatus includes providing a first vane having an airfoil section located between a first platform section and a second platform section, positioning a first shroud ring adjacent to the first vane, welding the first platform section of the first vane to the first shroud ring relative to a first edge of the of the first platform section of the first vane, and welding the first platform section of the first vane to the first shroud ring relative to a second edge of the of the first platform section. The second edge is located opposite the first edge.
摘要翻译：一种组装定子装置的方法包括提供具有位于第一平台部分和第二平台部分之间的翼型部分的第一叶片，将第一护罩环定位成与第一叶片相邻，将第一叶片的第一平台部分焊接到相对于第一叶片的第一平台部分的第一边缘的第一护罩环，并且相对于第一平台部分的第二边缘将第一叶片的第一平台部分焊接到第一护罩环。第二边缘与第一边缘相对。

8. 发明申请

US20090243228A1 Gas Turbine Engine Seals and Engines Incorporating Such Seals 有权
标题翻译：装有这种密封件的燃气轮机发动机密封和发动机
公开(公告)号：US20090243228A1
公开(公告)日：2009-10-01
申请号：US12056792
申请日：2008-03-27
申请人： Kurt R. Heinemann , Jose Paulino , Scot A. Webb , Mark Ring , Charles H. Warner
发明人： Kurt R. Heinemann , Jose Paulino , Scot A. Webb , Mark Ring , Charles H. Warner
IPC分类号： F02F11/00
CPC分类号： F01D11/005
摘要： Gas turbine engine seals and engines incorporating such seals are provided. In this regard, a representative seal includes: an annular seal body having an inner diameter and an outer diameter, the seal body extending along an axis of symmetry between a first end and a second end; the seal body being formed of a strip of material having first and second opposing edges, the strip of material being deformed to exhibit a first sealing surface at the first end, a second sealing surface at the second end, and a third sealing surface along the inner diameter, the first edge being located adjacent to the third sealing surface, the second edge being located adjacent to the second sealing surface; the first edge being spaced from the second edge to define an annular opening, the annular opening providing access to an annular cavity of the seal body.
摘要翻译：提供了包括这种密封件的燃气涡轮发动机密封件和发动机。在这方面，代表性的密封件包括：具有内径和外径的环形密封体，密封体沿第一端和第二端之间的对称轴延伸; 所述密封体由具有第一和第二相对边缘的材料条形成，所述材料条变形以在第一端处呈现第一密封表面，在第二端处具有第二密封表面，以及沿着所述第二密封表面的第三密封表面所述第一边缘邻近所述第三密封表面定位，所述第二边缘邻近所述第二密封表面定位; 所述第一边缘与所述第二边缘间隔开以限定环形开口，所述环形开口提供对所述密封体的环形腔的通路。

9. 发明申请

US20080145217A1 Method for securing a stator assembly 有权
标题翻译：固定定子组件的方法
公开(公告)号：US20080145217A1
公开(公告)日：2008-06-19
申请号：US11641326
申请日：2006-12-19
申请人： Jose Paulino , Richard K. Hayford
发明人： Jose Paulino , Richard K. Hayford
IPC分类号： F04D29/44 , F04D29/08
CPC分类号： F01D25/246 , F01D9/041 , F01D11/005 , F05D2230/642
摘要： An example exit guide vane for a gas turbine engine is mounted adjacent to a diffuser case defining an air flow path. A thrust balance seal is attached to the diffuser and the exit guide vane is mounted adjacent the diffuser case for guiding air flow into the air flow path. The exit guide vane is mounted adjacent to the diffuser without interfering with the air flow path or restricting thermal expansion.
摘要翻译：用于燃气涡轮发动机的示例性出口导叶安装在限定空气流动路径的扩散器壳体附近。推力平衡密封件附接到扩散器，并且出口导向叶片安装在扩散器壳体附近，用于引导空气流入空气流动路径。出口导向叶片与扩散器相邻地安装，而不干扰空气流动路径或限制热膨胀。

10. 发明专利

CA3093030A1 STRIP CONTAINING ACARICIDE 未知
公开(公告)号：CA3093030A1
公开(公告)日：2019-10-03
申请号：CA3093030
申请日：2019-03-05
申请人： CHICON CARNERO JOSE PAULINO
发明人： CHICON CARNERO JOSE PAULINO
IPC分类号： A01K47/06
摘要： The invention relates to a strip containing acaricide, which is made up of a plurality of compartments, placed in parallel and connected to one another, which serve to house an acaricide substance, in semi-solid state, characterised in that the tube-shaped compartments are square, rectangular, cylindrical, hexagonal or of any other geometric shape on the inside, and the inlet is open at both ends, the smaller inlet having an opening of 5 mm; an acaricide substance which acts by contact is deposited inside of same; the containing strip has a length of 10 mm to 500 mm, a width of 10 mm to 400 mm, and a height of 1 mm to 5 mm, all inclusive.

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