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Patent Agency Ranking
公开(公告)号：US20130270231A1
公开(公告)日：2013-10-17
申请号：US13914097
申请日：2013-06-10
Applicant: General Electric Company
Inventor： Mark Samuel Bailey , Michelle Rene Bezdecny , Stefan Andreas Moser
IPC: B23K26/00
CPC classification number: B23K26/00 , B23K26/03 , B23K26/356 , B23K2101/001 , C21D10/005 , F01D5/005 , F05D2230/41
Abstract: A system for determining accessibility of a tool to an object is provided. The system provides for selecting one or more sections on the object to be laser shock peened, selecting a region of interest on the one or more sections and determining a set of feasible solutions to access the selected region of interest on each of the one or more sections via use of an accessibility system.
Abstract translation: 提供了一种用于确定工具对物体的可访问性的系统。 该系统提供选择对象上的一个或多个部分进行激光冲击喷丸处理，在该一个或多个部分上选择感兴趣的区域，并且确定一组可行的解决方案以在所述一个或多个部分中的每个部分上访问所选择的感兴趣的区域 通过使用辅助功能系统进行部分。
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公开(公告)号：US20140115892A1
公开(公告)日：2014-05-01
申请号：US13665364
申请日：2012-10-31
Applicant: GENERAL ELECTRIC COMPANY
CPC classification number: G01M13/00 , B23H9/10 , B23P15/02 , F01D5/085 , G05B13/041 , Y10T29/49341
Abstract: Methods for testing turbine blades. One method for testing turbine blades includes measuring dimensions of each of a first set of turbine blades. The method also includes testing airflow through first openings in each of the first set of turbine blades to determine airflow properties of each of the first set of turbine blades. The method includes determining a relationship between the dimensions and the airflow properties of each of the first set of turbine blades. The method includes measuring dimensions of each of a second set of turbine blades. The method also includes determining airflow properties for each of the second set of turbine blades based at least partially on the dimensions of the second set of turbine blades and the relationship.
Abstract translation: 涡轮叶片测试方法。 用于测试涡轮叶片的一种方法包括测量第一组涡轮叶片中的每一个的尺寸。 该方法还包括通过第一组涡轮叶片中的每一个中的第一开口测试气流，以确定第一组涡轮叶片中的每一个的气流特性。 该方法包括确定第一组涡轮叶片中的每一个的尺寸和气流性质之间的关系。 该方法包括测量第二组涡轮叶片中的每一个的尺寸。 该方法还包括至少部分地基于第二组涡轮叶片的尺寸和关系确定第二组涡轮叶片中的每一个的气流特性。
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公开(公告)号：US09188504B2
公开(公告)日：2015-11-17
申请号：US13665364
申请日：2012-10-31
Applicant: General Electric Company
CPC classification number: G01M13/00 , B23H9/10 , B23P15/02 , F01D5/085 , G05B13/041 , Y10T29/49341
Abstract: Methods for testing turbine blades. One method for testing turbine blades includes measuring dimensions of each of a first set of turbine blades. The method also includes testing airflow through first openings in each of the first set of turbine blades to determine airflow properties of each of the first set of turbine blades. The method includes determining a relationship between the dimensions and the airflow properties of each of the first set of turbine blades. The method includes measuring dimensions of each of a second set of turbine blades. The method also includes determining airflow properties for each of the second set of turbine blades based at least partially on the dimensions of the second set of turbine blades and the relationship.
Abstract translation: 涡轮叶片测试方法。 用于测试涡轮叶片的一种方法包括测量第一组涡轮叶片中的每一个的尺寸。 该方法还包括通过第一组涡轮叶片中的每一个中的第一开口测试气流，以确定第一组涡轮叶片中的每一个的气流特性。 该方法包括确定第一组涡轮叶片中的每一个的尺寸和气流性质之间的关系。 该方法包括测量第二组涡轮叶片中的每一个的尺寸。 该方法还包括至少部分地基于第二组涡轮叶片的尺寸和关系确定第二组涡轮叶片中的每一个的气流特性。
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公开(公告)号：US08809729B2
公开(公告)日：2014-08-19
申请号：US13914097
申请日：2013-06-10
Applicant: General Electric Company
Inventor： Mark Samuel Bailey , Michelle Rene Bezdecny , Stefan Andreas Moser
IPC: B23K23/00
CPC classification number: B23K26/00 , B23K26/03 , B23K26/356 , B23K2101/001 , C21D10/005 , F01D5/005 , F05D2230/41
Abstract: A system for determining accessibility of a tool to an object is provided. The system provides for selecting one or more sections on the object to be laser shock peened, selecting a region of interest on the one or more sections and determining a set of feasible solutions to access the selected region of interest on each of the one or more sections via use of an accessibility system.
Abstract translation: 提供了一种用于确定工具对物体的可访问性的系统。 该系统提供选择对象上的一个或多个部分进行激光冲击喷丸处理，在该一个或多个部分上选择感兴趣的区域，并且确定一组可行的解决方案以在所述一个或多个部分中的每个部分上访问所选择的感兴趣区域 通过使用辅助功能系统进行部分。
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公开(公告)号：US20140041183A1
公开(公告)日：2014-02-13
申请号：US14048174
申请日：2013-10-08
Applicant: General Electric Company
CPC classification number: F01D5/005 , B23P6/007 , G05B19/4083 , G05B19/4097 , G05B2219/35031 , G05B2219/35097 , G05B2219/45147 , G05B2219/49066 , G05B2219/50214 , Y02T50/673 , Y10T29/49318 , Y10T29/49718 , Y10T29/49732
Abstract: A method of repair includes removing a deformed portion of a component to define a native component portion and adding a replacement portion to the native component portion. The replacement portion is adaptively machined based on one or more parameters of the native component portion and based on one or more original design parameters of the component.
Abstract translation: 一种修复方法包括去除组件的变形部分以限定本机组件部分并将替换部分添加到本机组件部分。 替换部分基于原始组件部分的一个或多个参数并且基于组件的一个或多个原始设计参数自适应地加工。
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