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

US20140070457A1 METHODS OF FORMING A CERAMIC COMPONENT AND A HIGH TEMPERATURE MOLD COMPONENT FOR USE THEREWITH 有权
标题翻译：形成陶瓷元件的方法及其使用的高温模具组件
公开(公告)号：US20140070457A1
公开(公告)日：2014-03-13
申请号：US13611011
申请日：2012-09-12
申请人： Gregory Thomas FOSTER , Eric Richard BONINI
发明人： Gregory Thomas FOSTER , Eric Richard BONINI
IPC分类号： C04B35/64
CPC分类号： C04B35/622 , B28B11/243 , B29C2035/005
摘要： Methods of forming a ceramic component and a high temperature mold for use therewith are provided. The method includes providing a fixture having a receiving surface configured to receive an unfired ceramic component. The method includes applying a continuous high temperature membrane to a surface of the unfired ceramic component. The method includes covering the continuous high temperature membrane and unfired ceramic component with a high temperature loose media. The method includes heating the unfired ceramic component to a firing temperature. The high temperature mold includes the fixture and a support structure forming a compartment surrounding the fixture. The mold allows the high temperature loose media to be contained within the compartment and to cover the continuous high temperature membrane. The continuous high temperature membrane and high temperature loose media are evenly distributed over the uncured ceramic component and operable to provide constant pressure during processing using the mold.
摘要翻译：提供形成陶瓷部件和使用其的高温模具的方法。该方法包括提供具有接收表面的夹具，该接收表面被配置为接收未焙烧的陶瓷部件。该方法包括将连续的高温膜施加到未焙烧的陶瓷部件的表面上。该方法包括用高温松散介质覆盖连续高温膜和未烧结陶瓷部件。该方法包括将未煅烧的陶瓷组分加热到焙烧温度。高温模具包括夹具和形成围绕夹具的隔室的支撑结构。模具允许高温松散介质被包含在隔室内并且覆盖连续的高温膜。连续的高温膜和高温松散介质均匀地分布在未固化的陶瓷组件上，并可操作以在使用模具的加工期间提供恒定的压力。

2. 发明申请

US20130043009A1 COMPONENTS WITH COOLING CHANNELS AND METHODS OF MANUFACTURE 有权
标题翻译：具有冷却通道的组件和制造方法
公开(公告)号：US20130043009A1
公开(公告)日：2013-02-21
申请号：US13210697
申请日：2011-08-16
申请人： Ronald Scott Bunker , Eric Richard Bonini
发明人： Ronald Scott Bunker , Eric Richard Bonini
IPC分类号： F28F13/06 , B23H1/00 , B05D3/12 , B23H5/00 , B24C1/00 , B21D53/02 , B23K26/00
CPC分类号： F01D5/186 , B23K26/38 , B23K26/384 , B23K26/388 , B23K26/389 , F01D5/183 , F01D5/187 , F01D9/041 , F01D25/28 , F01D25/30 , F05D2220/32 , F05D2230/90 , F05D2240/128 , F05D2240/30 , F05D2250/292 , F05D2260/202 , F05D2260/204 , Y02T50/672 , Y02T50/676 , Y10T29/4932 , Y10T29/49341
摘要： A component is provided and includes a substrate comprising an outer and an inner surface, where the inner surface defines at least one hollow, interior space. The component defines one or more grooves, where each groove extends at least partially along the outer surface of the substrate and has a base and a top. The base is wider than the top, such that each groove comprises a re-entrant shaped groove. 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. Each access hole has an exit diameter D that exceeds the opening width d of the top of the respective groove. The diameter D is an effective diameter based on the area enclosed. The component further includes at least one coating disposed over at least a portion of the surface of the substrate, wherein the groove(s) and the coating together define one or more re-entrant shaped channels for cooling the component. A method for manufacturing the component is also provided. A method for manufacturing a component is also provided, where the groove and the access hole(s) are machined as a single continuous process, such that the groove and the access hole(s) form a continuous cooling passage.
摘要翻译：提供部件并且包括包括外表面和内表面的基底，其中内表面限定至少一个中空的内部空间。该部件限定一个或多个凹槽，其中每个凹槽至少部分地沿着基底的外表面延伸并且具有基部和顶部。基部比顶部宽，使得每个凹槽包括凹入形状的凹槽。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。每个通孔的出口直径D超过相应槽的顶部的开口宽度d。直径D是基于封闭区域的有效直径。所述部件还包括设置在所述基底表面的至少一部分上的至少一个涂层，其中所述凹槽和所述涂层一起限定一个或多个重新形成的通道以冷却所述部件。还提供了一种制造该部件的方法。还提供了一种用于制造部件的方法，其中槽和进入孔被加工为单个连续过程，使得凹槽和进入孔形成连续的冷却通道。

3. 发明授权

US09206696B2 Components with cooling channels and methods of manufacture 有权
标题翻译：具有冷却通道和制造方法的部件
公开(公告)号：US09206696B2
公开(公告)日：2015-12-08
申请号：US13210697
申请日：2011-08-16
申请人： Ronald Scott Bunker , Eric Richard Bonini
发明人： Ronald Scott Bunker , Eric Richard Bonini
IPC分类号： F28F13/06 , F01D5/18 , B23K26/38
CPC分类号： F01D5/186 , B23K26/38 , B23K26/384 , B23K26/388 , B23K26/389 , F01D5/183 , F01D5/187 , F01D9/041 , F01D25/28 , F01D25/30 , F05D2220/32 , F05D2230/90 , F05D2240/128 , F05D2240/30 , F05D2250/292 , F05D2260/202 , F05D2260/204 , Y02T50/672 , Y02T50/676 , Y10T29/4932 , Y10T29/49341
摘要： A component is provided and includes a substrate comprising an outer and an inner surface, where the inner surface defines at least one hollow, interior space. The component defines one or more grooves, where each groove extends at least partially along the outer surface of the substrate and has a base and a top. The base is wider than the top, such that each groove comprises a re-entrant shaped groove. 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. Each access hole has an exit diameter D that exceeds the opening width d of the top of the respective groove. The diameter D is an effective diameter based on the area enclosed. The component further includes at least one coating disposed over at least a portion of the surface of the substrate, wherein the groove(s) and the coating together define one or more re-entrant shaped channels for cooling the component. A method for manufacturing the component is also provided. A method for manufacturing a component is also provided, where the groove and the access hole(s) are machined as a single continuous process, such that the groove and the access hole(s) form a continuous cooling passage.
摘要翻译：提供部件并且包括包括外表面和内表面的基底，其中内表面限定至少一个中空的内部空间。该部件限定一个或多个凹槽，其中每个凹槽至少部分地沿着基底的外表面延伸并且具有基部和顶部。基部比顶部宽，使得每个凹槽包括凹入形状的凹槽。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。每个通孔的出口直径D超过相应槽的顶部的开口宽度d。直径D是基于封闭区域的有效直径。所述部件还包括设置在所述基底表面的至少一部分上的至少一个涂层，其中所述凹槽和所述涂层一起限定一个或多个重新形成的通道以冷却所述部件。还提供了一种制造该部件的方法。还提供了一种用于制造部件的方法，其中槽和进入孔被加工为单个连续过程，使得凹槽和进入孔形成连续的冷却通道。

4. 发明申请

US20140030098A1 ARTICLE OF MANUFACTURE 有权
标题翻译：制造品
公开(公告)号：US20140030098A1
公开(公告)日：2014-01-30
申请号：US13556323
申请日：2012-07-24
申请人： Michael James Dutka , John Duong , Ya-Tien Chiu , Alexander David Shrum , Kelvin Rono Aaron , Christopher Edward LaMaster , San-Dar Gau , Franco Monteleone , Paul Griffin Delvernois , Matthew John McKeever , Govindarajan Rengarajan , Jeremy Peter Latimer , Marc Edward Blohm , Eric Richard Bonini , Venkata Siva Prasad Chaluvadi , Jamie Dean Lumpkin , Thomas Robbins Tipton
发明人： Michael James Dutka , John Duong , Ya-Tien Chiu , Alexander David Shrum , Kelvin Rono Aaron , Christopher Edward LaMaster , San-Dar Gau , Franco Monteleone , Paul Griffin Delvernois , Matthew John McKeever , Govindarajan Rengarajan , Jeremy Peter Latimer , Marc Edward Blohm , Eric Richard Bonini , Venkata Siva Prasad Chaluvadi , Jamie Dean Lumpkin , Thomas Robbins Tipton
IPC分类号： F01D5/30 , F01D5/14
CPC分类号： F01D5/3038 , F04D29/322 , F05D2250/74
摘要： An article of manufacture has a first component configured for use with a turbomachine. The first component is configured for attachment to a second component, and reduces the possibility of attachment with an undesired third component by modification of a. characteristic of the first component. This modification is matched by a complementary characteristic of the second component. The first component has a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table selected from the group consisting of TABLES 1-11. Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying by a number. X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height. The airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.
摘要翻译：制造品具有配置成与涡轮机一起使用的第一部件。第一部件被配置为附接到第二部件，并且通过修改a来减少与不希望的第三部件的连接的可能性。第一部分的特征。该修改由第二组件的互补特性匹配。第一部件具有基本上根据从由表1-11组成的组中选择的可缩放表格中阐述的X，Y和Z的笛卡尔坐标值的标称翼型分布。 X，Y和Z的笛卡尔坐标值是通过乘以数字可转换为尺寸距离的无量纲值。 X和Y是当通过连续弧连接时在每个Z高度处限定翼型轮廓部分的坐标。每个Z高度处的翼型轮廓部分彼此连接以形成完整的翼型形状。

5. 发明申请

US20130336798A1 AIRFOIL SHAPE FOR A COMPRESSOR 有权
公开(公告)号：US20130336798A1
公开(公告)日：2013-12-19
申请号：US13526832
申请日：2012-06-19
申请人： Michael James Dutka , John Duong , Ya-Tien Chiu , Alexander David Shrum , Kelvin Rono Aaron , Christopher Edward LaMaster , San-Dar Gau , Franco Monteleone , Paul Griffin Delvernois , Matthew John McKeever , Govindarajan Rengarajan , Jeremy Peter Latimer , Marc Edward Blohm , Eric Richard Bonini , Venkata Siva Prasad Chaluvadi
发明人： Michael James Dutka , John Duong , Ya-Tien Chiu , Alexander David Shrum , Kelvin Rono Aaron , Christopher Edward LaMaster , San-Dar Gau , Franco Monteleone , Paul Griffin Delvernois , Matthew John McKeever , Govindarajan Rengarajan , Jeremy Peter Latimer , Marc Edward Blohm , Eric Richard Bonini , Venkata Siva Prasad Chaluvadi
IPC分类号： F04D29/38
CPC分类号： F04D29/324 , F01D5/141 , F05D2250/74
摘要： An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLES 1-11, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

6. 发明授权

US09175693B2 Airfoil shape for a compressor 有权
公开(公告)号：US09175693B2
公开(公告)日：2015-11-03
申请号：US13526832
申请日：2012-06-19
申请人： Michael James Dutka , John Duong , Ya-Tien Chiu , Alexander David Shrum , Kelvin Rono Aaron , Christopher Edward LaMaster , San-Dar Gau , Franco Monteleone , Paul Griffin Delvernois , Matthew John McKeever , Govindarajan Rengarajan , Jeremy Peter Latimer , Marc Edward Blohm , Eric Richard Bonini , Venkata Siva Prasad Chaluvadi
发明人： Michael James Dutka , John Duong , Ya-Tien Chiu , Alexander David Shrum , Kelvin Rono Aaron , Christopher Edward LaMaster , San-Dar Gau , Franco Monteleone , Paul Griffin Delvernois , Matthew John McKeever , Govindarajan Rengarajan , Jeremy Peter Latimer , Marc Edward Blohm , Eric Richard Bonini , Venkata Siva Prasad Chaluvadi
IPC分类号： F01D5/14 , F01D5/16 , F04D29/32
CPC分类号： F04D29/324 , F01D5/141 , F05D2250/74
摘要： An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLES 1-11, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

7. 发明授权

US09145777B2 Article of manufacture 有权
标题翻译：制造条款
公开(公告)号：US09145777B2
公开(公告)日：2015-09-29
申请号：US13556323
申请日：2012-07-24
申请人： Michael James Dutka , John Duong , Ya-Tien Chiu , Alexander David Shrum , Kelvin Rono Aaron , Christopher Edward LaMaster , San-Dar Gau , Franco Monteleone , Paul Griffin Delvernois , Matthew John McKeever , Govindarajan Rengarajan , Jeremy Peter Latimer , Marc Edward Blohm , Eric Richard Bonini , Venkata Siva Prasad Chaluvadi , Jamie Dean Lumpkin , Thomas Robbins Tipton
发明人： Michael James Dutka , John Duong , Ya-Tien Chiu , Alexander David Shrum , Kelvin Rono Aaron , Christopher Edward LaMaster , San-Dar Gau , Franco Monteleone , Paul Griffin Delvernois , Matthew John McKeever , Govindarajan Rengarajan , Jeremy Peter Latimer , Marc Edward Blohm , Eric Richard Bonini , Venkata Siva Prasad Chaluvadi , Jamie Dean Lumpkin , Thomas Robbins Tipton
IPC分类号： F01D5/30 , F04D29/34 , F04D29/32
CPC分类号： F01D5/3038 , F04D29/322 , F05D2250/74
摘要： An article of manufacture has a first component configured for use with a turbomachine. The first component is configured for attachment to a second component, and reduces the possibility of attachment with an undesired third component by modification of a characteristic of the first component. This modification is matched by a complementary characteristic of the second component. The first component has a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table selected from the group consisting of TABLES 1-11. Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying by a number. X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height. The airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.
摘要翻译：制造品具有配置成与涡轮机一起使用的第一部件。第一部件被配置为附接到第二部件，并且通过修改第一部件的特性来减少与不需要的第三部件的连接的可能性。该修改由第二组件的互补特性匹配。第一部件具有基本上根据从由表1-11组成的组中选择的可缩放表格中阐述的X，Y和Z的笛卡尔坐标值的标称翼型分布。 X，Y和Z的笛卡尔坐标值是通过乘以数字可转换为尺寸距离的无量纲值。 X和Y是当通过连续弧连接时在每个Z高度处限定翼型轮廓部分的坐标。每个Z高度处的翼型轮廓部分彼此连接以形成完整的翼型形状。

8. 发明授权

US09096472B2 Methods of forming a ceramic component and a high temperature mold component for use therewith 有权
标题翻译：形成陶瓷部件和与其一起使用的高温模具部件的方法
公开(公告)号：US09096472B2
公开(公告)日：2015-08-04
申请号：US13611011
申请日：2012-09-12
申请人： Gregory Thomas Foster , Eric Richard Bonini
发明人： Gregory Thomas Foster , Eric Richard Bonini
IPC分类号： C04B35/64 , C04B35/622 , B28B11/24 , B29C35/00
CPC分类号： C04B35/622 , B28B11/243 , B29C2035/005
摘要： Methods of forming a ceramic component and a high temperature mold for use therewith are provided. The method includes providing a fixture having a receiving surface configured to receive an unfired ceramic component. The method includes applying a continuous high temperature membrane to a surface of the unfired ceramic component. The method includes covering the continuous high temperature membrane and unfired ceramic component with a high temperature loose media. The method includes heating the unfired ceramic component to a firing temperature. The high temperature mold includes the fixture and a support structure forming a compartment surrounding the fixture. The mold allows the high temperature loose media to be contained within the compartment and to cover the continuous high temperature membrane. The continuous high temperature membrane and high temperature loose media are evenly distributed over the uncured ceramic component and operable to provide constant pressure during processing using the mold.
摘要翻译：提供形成陶瓷部件和使用其的高温模具的方法。该方法包括提供具有接收表面的夹具，该接收表面被配置为接收未焙烧的陶瓷部件。该方法包括将连续的高温膜施加到未焙烧的陶瓷部件的表面上。该方法包括用高温松散介质覆盖连续高温膜和未烧结陶瓷部件。该方法包括将未煅烧的陶瓷组分加热到焙烧温度。高温模具包括夹具和形成围绕夹具的隔室的支撑结构。模具允许高温松散介质被包含在隔室内并且覆盖连续的高温膜。连续的高温膜和高温松散介质均匀地分布在未固化的陶瓷组件上，并可操作以在使用模具的加工期间提供恒定的压力。

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