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1. 发明申请

US20120053854A1 Identifying Features on a Surface of an Object Using Wavelet Analysis 有权
标题翻译：使用小波分析识别对象表面上的特征
公开(公告)号：US20120053854A1
公开(公告)日：2012-03-01
申请号：US12872389
申请日：2010-08-31
申请人： Michael David Huffman , Andrew James Booker , Thomas A. Hogan , Alan K. Jones , Bruce C. Andrews
发明人： Michael David Huffman , Andrew James Booker , Thomas A. Hogan , Alan K. Jones , Bruce C. Andrews
IPC分类号： G01B11/30 , B23Q17/00
CPC分类号： G01B11/30 , G01B21/20 , G01B21/30 , Y10T29/49771
摘要： A method and apparatus for inspecting a surface of an object. Data from measuring the surface of the object is obtained to form surface data for the object. A range of frequencies for features on the object is selected based on a range of distances between adjacent peaks for the features. The features are formed by a tool moving along a number of paths. Desired surface data for the features is obtained from the surface data using the range of frequencies selected. A determination is made as to whether the desired surface data for the features meets a policy specifying a desired surface for the object. In response to an absence of a determination that the desired surface data for the features meets the policy, the object is reworked.
摘要翻译：一种用于检查物体表面的方法和装置。获得测量对象表面的数据，以形成对象的表面数据。基于特征的相邻峰之间的距离范围来选择对象上的特征的频率范围。特征由沿着多个路径移动的工具形成。使用所选频率的范围，从表面数据中获得要素的所需表面数据。确定特征的期望表面数据是否满足指定对象的期望表面的策略。响应于不存在用于特征的所需表面数据满足策略的确定，对象被重新加工。

2. 发明授权

US08467978B2 Identifying features on a surface of an object using wavelet analysis 有权
标题翻译：使用小波分析识别对象表面上的特征
公开(公告)号：US08467978B2
公开(公告)日：2013-06-18
申请号：US12872389
申请日：2010-08-31
申请人： Michael David Huffman , Andrew James Booker , Thomas A. Hogan , Alan K. Jones , Bruce C. Andrews
发明人： Michael David Huffman , Andrew James Booker , Thomas A. Hogan , Alan K. Jones , Bruce C. Andrews
IPC分类号： G01B21/20 , G01B21/30 , B23Q17/20 , G06F11/30 , G06F19/00
CPC分类号： G01B11/30 , G01B21/20 , G01B21/30 , Y10T29/49771
摘要： A method and apparatus for inspecting a surface of an object. Data from measuring the surface of the object is obtained to form surface data for the object. A range of frequencies for features on the object is selected based on a range of distances between adjacent peaks for the features. The features are formed by a tool moving along a number of paths. Desired surface data for the features is obtained from the surface data using the range of frequencies selected. A determination is made as to whether the desired surface data for the features meets a policy specifying a desired surface for the object. In response to an absence of a determination that the desired surface data for the features meets the policy, the object is reworked.
摘要翻译：一种用于检查物体表面的方法和装置。获得测量对象表面的数据，以形成对象的表面数据。基于特征的相邻峰之间的距离范围来选择对象上的特征的频率范围。特征由沿着多个路径移动的工具形成。使用所选频率的范围，从表面数据中获得要素的所需表面数据。确定特征的期望表面数据是否满足指定对象的期望表面的策略。响应于不存在用于特征的所需表面数据满足策略的确定，对象被重新加工。

3. 发明授权

US08005563B2 System for assembling aircraft 有权
标题翻译：飞机组装系统
公开(公告)号：US08005563B2
公开(公告)日：2011-08-23
申请号：US12117093
申请日：2008-05-08
申请人： James M. Cobb , John G. Barnes , Alan K. Jones , Brian K. Sollenberger , Patrick B. Stone
发明人： James M. Cobb , John G. Barnes , Alan K. Jones , Brian K. Sollenberger , Patrick B. Stone
IPC分类号： G06F19/00 , G05B19/18
CPC分类号： B64F5/10 , Y10T29/49778 , Y10T29/4978 , Y10T29/53061
摘要： A system automatically moves large scale components of a vehicle such as an airplane, into final assembly alignment. A noncontact measurement system determines the locations of aerodynamically significant features on each of the components. The measured locations of the components are used to control an automated jacking system that includes assembly jacks for individually moving the components into assembly alignment. A system is provided for calculating the cruise configuration of the vehicle “as-built” and for transferring the cruise configuration into the vehicle where it is recorded in the form of a physical monument.
摘要翻译：系统自动将诸如飞机的车辆的大规模部件移动到最终的组装对准中。非接触测量系统确定每个部件上的空气动力学显着特征的位置。部件的测量位置用于控制自动起重系统，其包括用于单独地将部件移动到组件对准中的组装插座。提供了一种用于计算“建成”的车辆的巡航配置并将巡航配置传送到以物理纪念碑的形式记录的车辆中的系统。

4. 发明申请

US20090312993A1 TAPE COURSE GENERATION METHOD AND APPARATUS FOR PROGRAMMING A COMPOSITE TAPE LAMINATION MACHINE 有权
标题翻译：复合胶带复合机编织带生产方法及装置
公开(公告)号：US20090312993A1
公开(公告)日：2009-12-17
申请号：US12545819
申请日：2009-08-22
申请人： Michael Drumheller , Alan K. Jones , Frederick W. Klein
发明人： Michael Drumheller , Alan K. Jones , Frederick W. Klein
IPC分类号： G06G7/48
CPC分类号： G05B19/41 , B29C70/386 , G05B2219/35113 , G05B2219/35115 , G05B2219/35129 , G05B2219/49002 , Y02T10/82
摘要： A method of defining a composite tape course to form at least a portion of a composite part ply comprises approximating a contoured surface with a reference plane. The method further includes selecting a three-dimensional reference surface to approximate the contoured surface and defining a first function to correlate a first point from the contoured surface to a first intermediate point on the reference surface. The method includes selecting the reference plane to approximate the reference surface, defining a second function to correlate the first intermediate point to a reference point in the reference plane, and mapping a ply boundary from the contoured surface to a reference ply boundary in the reference plane. A tape boundary may be mapped from the contoured surface to a reference tape boundary in the reference plane. A tape edge may be defined based at least in part on a reference intersection of the reference ply boundary and the reference tape boundary in order to form at least a portion of the composite part ply using the defined tape edge.
摘要翻译：定义复合带路线以形成复合部件帘布层的至少一部分的方法包括用参考平面近似轮廓表面。该方法还包括选择三维参考表面以近似轮廓表面并且限定第一功能以将从轮廓表面的第一点与参考表面上的第一中间点相关联。该方法包括选择参考平面以近似参考表面，定义第二函数以将第一中间点与参考平面中的参考点相关联，以及将层状边界从轮廓表面映射到参考平面中的参考层边界。磁带边界可以从轮廓表面映射到参考平面中的参考磁带边界。可以至少部分地基于参考层边界和参考带边界的参考交点来定义带边缘，以便使用限定的带边缘形成复合部件层的至少一部分。

5. 发明授权

US07869895B2 System, method, and computer program product for computing orientation alignment transfer tool locations to transfer predicted cruise orientation alignment of an as-built airplane 有权
标题翻译：系统，方法和计算机程序产品，用于计算定向对准传送工具位置，以传送建造的飞机的预测的巡航导向对准
公开(公告)号：US07869895B2
公开(公告)日：2011-01-11
申请号：US12002078
申请日：2007-12-13
申请人： Alan K. Jones
发明人： Alan K. Jones
IPC分类号： G06F19/00 , B23B5/28 , G01P21/00
CPC分类号： B64F5/10 , Y10T29/49778 , Y10T29/4978
摘要： Illustrative computer-executable methods, systems, and computer software program products compute orientation alignment transfer tool location. Orientation of at least one aerodynamically significant feature of an as-built airplane is automatically determined. Orientation of an orientation monument for the as-built airplane is automatically determined from the determined orientation of the at least one aerodynamically significant feature of the as-built airplane, and motion to align an orientation alignment transfer tool with the determined orientation of the orientation monument is automatically determined.
摘要翻译：说明性的计算机可执行方法，系统和计算机软件程序产品计算定向对准转移工具位置。自动确定建造的飞机的至少一个空气动力学特征的方位。建造的飞机的定向纪念碑的方向是根据所建造的飞机的至少一个空气动力学显着特征的确定方向自动确定的，以及使定向对准转移工具与确定的定向纪念碑的方向对齐的运动自动确定。

6. 发明申请

US20090112349A1 SYSTEM FOR ASSEMBLING AIRCRAFT 有权
标题翻译：组装飞机的系统
公开(公告)号：US20090112349A1
公开(公告)日：2009-04-30
申请号：US12117093
申请日：2008-05-08
申请人： James M. Cobb , John G. Barnes , Alan K. Jones , Brian K. Sollenberger , Patrick B. Stone
发明人： James M. Cobb , John G. Barnes , Alan K. Jones , Brian K. Sollenberger , Patrick B. Stone
IPC分类号： B23P21/00 , G06F19/00
CPC分类号： B64F5/10 , Y10T29/49778 , Y10T29/4978 , Y10T29/53061
摘要： A system automatically moves large scale components of a vehicle such as an airplane, into final assembly alignment. A noncontact measurement system determines the locations of aerodynamically significant features on each of the components. The measured locations of the components are used to control an automated jacking system that includes assembly jacks for individually moving the components into assembly alignment. A system is provided for calculating the cruise configuration of the vehicle “as-built” and for transferring the cruise configuration into the vehicle where it is recorded in the form of a physical monument.
摘要翻译：系统自动将诸如飞机的车辆的大规模部件移动到最终的组装对准中。非接触测量系统确定每个部件上的空气动力学显着特征的位置。部件的测量位置用于控制自动起重系统，其包括用于单独地将部件移动到组件对准中的组装插座。提供了一种用于计算“建成”的车辆的巡航配置并将巡航配置传送到以物理纪念碑的形式记录的车辆中的系统。

7. 发明授权

US08620470B2 System for assembling aircraft 有权
标题翻译：飞机组装系统
公开(公告)号：US08620470B2
公开(公告)日：2013-12-31
申请号：US13183002
申请日：2011-07-14
申请人： James M. Cobb , John G. Barnes , Alan K. Jones , Brian K. Sollenberger , Patrick B. Stone
发明人： James M. Cobb , John G. Barnes , Alan K. Jones , Brian K. Sollenberger , Patrick B. Stone
IPC分类号： G05D3/12 , G06F19/00
CPC分类号： B64F5/10 , Y10T29/49778 , Y10T29/4978 , Y10T29/53061
摘要： A system for assembling aircraft is disclosed. An example system for moving components of an airplane into assembly alignment includes a jacking system including assembly jacks for supporting and moving components of the airplane into assembly alignment; a measurement system independent of the jacking system for determining locations of a plurality of features the components of the airplane while the components are supported on the assembly jacks; and a computer system for determining the relative positions of the components in a coordinate system of the airplane and for controlling the movement of the assembly jacks to bring the components into assembly alignment.
摘要翻译：公开了一种用于组装飞行器的系统。用于将飞机的部件移动到组装对准的示例系统包括顶升系统，其包括用于将飞机的部件支撑并移动到组件对准中的组件千斤顶; 独立于顶升系统的测量系统，用于在组件支撑在组件插座上时确定飞机的部件的多个特征的位置; 以及用于确定所述部件在所述飞机的坐标系中的相对位置并且用于控制所述组件千斤顶的运动以使部件进入组装对准的计算机系统。

8. 发明授权

US07917242B2 System, method, and computer program product for computing jack locations to align parts for assembly 有权
标题翻译：系统，方法和计算机程序产品，用于计算插座位置以对齐零件进行组装
公开(公告)号：US07917242B2
公开(公告)日：2011-03-29
申请号：US11977987
申请日：2007-10-26
申请人： Alan K. Jones
发明人： Alan K. Jones
IPC分类号： G06F19/00 , G05B19/18
CPC分类号： B64F5/10 , Y10T29/4978 , Y10T29/53974
摘要： Illustrative computer-executable methods, systems, and computer software program products compute assembly jack locations to align parts for assembly. Initial locations of at least one component to be moved and a desired final location for the at least one component to be moved are determined from initial position measurement data for the at least one component to be moved and the final location. Motion to align the at least one component to be moved with the final location is automatically determined. Optimal displacements of assembly jacks to produce the determined motion are automatically determined. After movement, location of the at least one moved part at a final assembled position is automatically determined. If applicable, data regarding additional assembly jack displacement can be inputted, the determined optimal location for the at least one part to be moved can be adjusted, and additional motion due to additional assembly jack displacement can be determined.
摘要翻译：说明性的计算机可执行方法，系统和计算机软件程序产品计算组装插座位置以对准用于组装的部件。要移动的至少一个部件的初始位置和用于要移动的至少一个部件的期望的最终位置由待移动的至少一个部件的最初位置测量数据和最终位置确定。自动确定要移动的至少一个组件与最终位置对齐的运动。自动确定组装千斤顶的最佳位移以产生确定的运动。在移动之后，自动确定至少一个移动部件在最终组装位置的位置。如果适用，可以输入关于附加组装插座位移的数据，可以调整用于待移动的至少一个部件的确定的最佳位置，并且可以确定由于额外的组装插座位移引起的附加运动。

9. 发明授权

US07869982B2 Tape course generation method and apparatus for programming a composite tape lamination machine 有权
标题翻译：用于编织复合胶带层压机的胶带行程生成方法和装置
公开(公告)号：US07869982B2
公开(公告)日：2011-01-11
申请号：US12545819
申请日：2009-08-22
申请人： Michael Drumheller , Alan K. Jones , Frederick K. Klein
发明人： Michael Drumheller , Alan K. Jones , Frederick K. Klein
IPC分类号： G06F17/50
CPC分类号： G05B19/41 , B29C70/386 , G05B2219/35113 , G05B2219/35115 , G05B2219/35129 , G05B2219/49002 , Y02T10/82
摘要： A method of defining a composite tape course to form at least a portion of a composite part ply comprises approximating a contoured surface with a reference plane. The method further includes selecting a three-dimensional reference surface to approximate the contoured surface and defining a first function to correlate a first point from the contoured surface to a first intermediate point on the reference surface. The method includes selecting the reference plane to approximate the reference surface, defining a second function to correlate the first intermediate point to a reference point in the reference plane, and mapping a ply boundary from the contoured surface to a reference ply boundary in the reference plane. A tape boundary may be mapped from the contoured surface to a reference tape boundary in the reference plane. A tape edge may be defined based at least in part on a reference intersection of the reference ply boundary and the reference tape boundary in order to form at least a portion of the composite part ply using the defined tape edge.
摘要翻译：定义复合带路线以形成复合部件帘布层的至少一部分的方法包括用参考平面近似轮廓表面。该方法还包括选择三维参考表面以近似轮廓表面并且限定第一功能以将从轮廓表面的第一点与参考表面上的第一中间点相关联。该方法包括选择参考平面以近似参考表面，定义第二函数以将第一中间点与参考平面中的参考点相关联，以及将层状边界从轮廓表面映射到参考平面中的参考层边界。磁带边界可以从轮廓表面映射到参考平面中的参考磁带边界。可以至少部分地基于参考层边界和参考带边界的参考交点来定义带边缘，以便使用限定的带边缘形成复合部件层的至少一部分。

10. 发明授权

US07769481B2 Head assignment system and method 有权
标题翻译：头部分配系统和方法
公开(公告)号：US07769481B2
公开(公告)日：2010-08-03
申请号：US11315101
申请日：2005-12-23
申请人： Wei-Pai Tang , Alan K. Jones , Daniel E. Gonsor
发明人： Wei-Pai Tang , Alan K. Jones , Daniel E. Gonsor
IPC分类号： G06F19/00
CPC分类号： B29C70/386
摘要： To generate course head assignments for a multihead composite material application machine having a set of heads, a set of paths for a ply for a composite part is received and it is determined whether each path of the set of paths complies with a head characteristic for the set of heads. In addition, a special head of the set of heads is assigned to a non-standard path of the set of paths in response to determining the non-standard path does not comply with the head characteristic and ones of the set of heads are assigned to corresponding ones of the set of paths in response to the ones of the set of paths being in compliance with the head characteristics. Furthermore, a constellation of head locations is calculated in response to the set of paths being in compliance with the head characteristic and the set of heads are assigned to the constellation of head locations in response to calculating the constellation of head locations.
摘要翻译：为了为具有一组头部的多头复合材料应用机器生成路线头分配，接收用于复合部件的层的一组路径，并且确定该组路径中的每个路径是否符合一套头此外，响应于确定非标准路径不符合头部特性而将该组头部的特殊头部分配给该组路径的非标准路径，并且将该组头部中的一个分配给响应于该组路径中的路径符合头部特征的路径组中的相应路径。此外，响应于一组路径符合头部特性来计算头部位置的星座，并且响应于计算头部位置的星座，将该组头部分配给头部位置的星座。

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