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1. 发明授权

US09486917B2 Mobile automated assembly tool for aircraft structures 有权
标题翻译：飞机结构的移动式自动装配工具
公开(公告)号：US09486917B2
公开(公告)日：2016-11-08
申请号：US14558859
申请日：2014-12-03
申请人： The Boeing Company
发明人： Eric M. Reid , Darrell Darwin Jones , Clayton Lynn Munk , Steven A. Best , Matthew Ray DesJardien , Carlos Daniel Crespo
IPC分类号： B25J5/00 , B23P19/06 , B25J11/00 , B23B41/00 , B64F5/00
CPC分类号： B25J5/007 , B23B41/00 , B23B2215/04 , B23P19/06 , B23Q3/15513 , B23Q3/15536 , B25J11/005 , B25J11/007 , B64F5/10 , Y10T29/49828 , Y10T29/4989 , Y10T29/5107 , Y10T408/03 , Y10T408/05 , Y10T408/55
摘要： A method and apparatus for performing an operation on a surface of a structure. An assembly system may comprise a motion platform and a mobile platform. The motion platform may be configured to be positioned below the surface of the structure to perform the operation on the surface. The mobile platform may be configured to carry the motion platform across a floor of a manufacturing environment from a first location to a second location.
摘要翻译：一种用于在结构的表面上执行操作的方法和装置。组装系统可以包括运动平台和移动平台。运动平台可以被配置为定位在结构的表面下方以在表面上执行操作。移动平台可以被配置为将运动平台跨越制造环境的地板从第一位置运送到第二位置。

2. 发明申请

US20150314436A1 Mobile Automated Assembly Tool for Aircraft Structures 有权
标题翻译：飞机结构的移动自动装配工具
公开(公告)号：US20150314436A1
公开(公告)日：2015-11-05
申请号：US14558859
申请日：2014-12-03
申请人： The Boeing Company
发明人： Eric M. Reid , Darrell Darwin Jones , Clayton Lynn Munk , Steven A. Best , Matthew Ray DesJardien , Carlos Daniel Crespo
IPC分类号： B25J5/00 , B23P19/06 , B23B41/00 , B25J11/00
CPC分类号： B25J5/007 , B23B41/00 , B23B2215/04 , B23P19/06 , B23Q3/15513 , B23Q3/15536 , B25J11/005 , B25J11/007 , B64F5/10 , Y10T29/49828 , Y10T29/4989 , Y10T29/5107 , Y10T408/03 , Y10T408/05 , Y10T408/55
摘要： A method and apparatus for performing an operation on a surface of a structure. An assembly system may comprise a motion platform and a mobile platform. The motion platform may be configured to be positioned below the surface of the structure to perform the operation on the surface. The mobile platform may be configured to carry the motion platform across a floor of a manufacturing environment from a first location to a second location.
摘要翻译：一种用于在结构的表面上执行操作的方法和装置。组装系统可以包括运动平台和移动平台。运动平台可以被配置为定位在结构的表面下方以在表面上执行操作。移动平台可以被配置为将运动平台跨越制造环境的地板从第一位置运送到第二位置。

3. 发明申请

US20150266174A1 Apparatus and Method for Remote Fastener Installation 有权
标题翻译：远程紧固件安装的装置和方法
公开(公告)号：US20150266174A1
公开(公告)日：2015-09-24
申请号：US14724892
申请日：2015-05-29
申请人： The Boeing Company
发明人： James Albert DeLand , Roger A. Gage , Darrell Darwin Jones
IPC分类号： B25B23/00 , B64F5/00 , B23P19/06
CPC分类号： B25B23/0085 , B23P19/069 , B23P2700/01 , B64F5/10 , Y10T29/49948
摘要： A tool configured to install and torque multiple fasteners, such as nuts and/or bolts, positioned in confined and/or hard to reach areas. The tool includes a body portion, a plurality of fastener retainers, and a structure which permits both the remote tightening and torquing of such fasters. The tool also provides an actuator for the remote release of torque loads which may build up in the fastener retainers during such torquing of the fasteners. The actuator includes a lever arm pivotally connected to the body portion and a cam that is rotatable between a first position and a second position. A linkage is engaged by the cam and urges the lever arm to a torquing position upon the cam being in the first position and to a torque release position upon the cam being in the second position.
摘要翻译：一种被配置为安装和扭转定位在有限和/或难以到达的区域中的多个紧固件（例如螺母和/或螺栓）的工具。该工具包括主体部分，多个紧固件保持器和允许这种更快的紧固和扭转两者的结构。该工具还提供用于远程释放扭矩负载的致动器，其可在紧固件扭转期间在紧固件保持器中累积。致动器包括枢转地连接到主体部分的杠杆臂和可在第一位置和第二位置之间旋转的凸轮。联动装置由凸轮接合，并且当凸轮处于第一位置并且当凸轮处于第二位置时，将杠杆臂推向扭矩位置。

4. 发明申请

US20210354404A1 AUTOMATED COMPOSITE FABRICATION SYSTEMS AND METHODS 有权
公开(公告)号：US20210354404A1
公开(公告)日：2021-11-18
申请号：US16875908
申请日：2020-05-15
申请人： The Boeing Company
发明人： Raviendra Sidath Suriyaarachchi , Darrell Darwin Jones
IPC分类号： B29C70/54 , B29C70/38
摘要： A system and a method for manufacturing laminated composite components is described. The system may include a cutting station configured to separate component layers from a ply of composition material according to a predefined pattern, a build station configured to stack the component layers according to a predetermined orientation, and a finishing station configured to compact the stacked component layers and provide the laminated composite component to an installation station.

5. 发明授权

US10507554B2 Methods for processing a workpiece 有权
公开(公告)号：US10507554B2
公开(公告)日：2019-12-17
申请号：US15598980
申请日：2017-05-18
申请人： The Boeing Company
发明人： James Albert DeLand , Darrell Darwin Jones
IPC分类号： B23Q5/08 , B23B35/00 , B23B45/04 , B23B23/00 , B25B23/145 , B25B23/00
摘要： A method of processing a workpiece comprises identifying processing locations on the workpiece, drilling a first hole at one of the processing locations using a rotary drive, sensing a flow of fluid while drilling, generating an operation signal based on the flow, comparing the duration interval of the operation signal to a predetermined temporal value, and drilling a different hole at a different processing location based on the duration interval and the temporal value.

6. 发明授权

US09878450B2 Method and apparatus for multi-stage spar assembly 有权
公开(公告)号：US09878450B2
公开(公告)日：2018-01-30
申请号：US14614886
申请日：2015-02-05
申请人： The Boeing Company
发明人： Monica Joy Brockway , Tanni Sisco , Daniel Richard Smith, Jr. , Victor Joseph Bolton , Fei Cai , Eric Scott Patton , Thomas Dee Hall , Clayton Lynn Munk , James C. Murphy , Darrell Darwin Jones , Paul Reed Stone
IPC分类号： B25J9/16
CPC分类号： B25J9/1687 , B25J9/1694 , Y10S901/01 , Y10S901/41
摘要： A method and apparatus for positioning one component relative to another component. First metrology data may be identified for a first component and second metrology data may be identified for a second component. First locations of first features may be identified on the first component using the first metrology data. Second locations of second features on the second component may be identified using the second metrology data. A transformation may be computed based on the first locations identified and the second locations identified for use in modifying a movement plan of a robotic system for positioning the second component relative to the first component.

7. 发明申请

US20160158940A1 Method and Apparatus for Multi-Stage Spar Assembly 有权
标题翻译：多级翼梁装配方法与装置
公开(公告)号：US20160158940A1
公开(公告)日：2016-06-09
申请号：US14614886
申请日：2015-02-05
申请人： The Boeing Company
发明人： Monica Joy Brockway , Tanni Sisco , Daniel Richard Smith, JR. , Victor Joseph Bolton , Fei Cai , Eric Scott Patton , Thomas Dee Hall , Clayton Lynn Munk , James C. Murphy , Darrell Darwin Jones , Paul Reed Stone
IPC分类号： B25J9/16
CPC分类号： B25J9/1687 , B25J9/1694 , Y10S901/01 , Y10S901/41
摘要： A method and apparatus for positioning one component relative to another component. First metrology data may be identified for a first component and second metrology data may be identified for a second component. First locations of first features may be identified on the first component using the first metrology data. Second locations of second features on the second component may be identified using the second metrology data. A transformation may be computed based on the first locations identified and the second locations identified for use in modifying a movement plan of a robotic system for positioning the second component relative to the first component.
摘要翻译：一种用于相对于另一组件定位一个部件的方法和装置。可以为第一部件识别第一计量数据，并且可以为第二部件识别第二计量数据。可以使用第一测量数据在第一组件上识别第一特征的第一位置。可以使用第二测量数据来识别第二组件上的第二特征的第二位置。可以基于所识别的第一位置和所识别的用于修改用于相对于第一组件定位第二组件的机器人系统的移动计划来使用的第二位置来计算变换。

8. 发明申请

US20150314888A1 System and Method for Positioning an Automated Assembly Tool Relative to a Structure 审中-公开
标题翻译：相对于结构定位自动组装工具的系统和方法
公开(公告)号：US20150314888A1
公开(公告)日：2015-11-05
申请号：US14558853
申请日：2014-12-03
申请人： The Boeing Company
发明人： Eric M. Reid , David Paul Banks , Darrell Darwin Jones
IPC分类号： B64F5/00 , B25J9/16
CPC分类号： B25J9/1687 , B25J13/089 , B64F5/10 , Y10S901/41 , Y10S901/44 , Y10S901/46
摘要： A method and apparatus for positioning an end effector relative to a structure. The apparatus may comprise the end effector and a sensor system. The end effector may be configured to perform an operation on the structure. The sensor system may have a plurality of sensors extending outward from the end effector.
摘要翻译：一种用于将端部执行器相对于结构定位的方法和装置。该装置可以包括端部执行器和传感器系统。末端执行器可以被配置为对结构执行操作。传感器系统可以具有从端部执行器向外延伸的多个传感器。

9. 发明申请

US20140353894A1 Modular and Reconfigurable Support System 有权
标题翻译：模块化和可重构支持系统
公开(公告)号：US20140353894A1
公开(公告)日：2014-12-04
申请号：US13904789
申请日：2013-05-29
申请人： THE BOEING COMPANY
发明人： Matthew R. DesJardien , Eric M. Reid , James N. Buttrick , Darrell Darwin Jones , Dan Dresskell Day , Paul Reed Stone
IPC分类号： B23Q1/64 , B23Q1/25
CPC分类号： B23Q1/64 , B23P19/10 , B23P2700/01 , B23Q1/25 , B64F5/10 , Y10T29/49998
摘要： An apparatus and method for supporting an object. In one illustrative embodiment, an apparatus may comprise a support structure, a positioning system, and a retention system. The positioning system may be associated with the support structure and configured to position the support structure with respect to a number of linear axes. The retention system may be associated with the support structure. The retention system may be configured to retain a portion of an object and move the portion of the object towards a platform such that the portion of the object substantially conforms to a shape of the platform.
摘要翻译：一种用于支撑物体的装置和方法。在一个说明性实施例中，装置可以包括支撑结构，定位系统和保持系统。定位系统可以与支撑结构相关联并且被配置为相对于多个线性轴定位支撑结构。保持系统可以与支撑结构相关联。保持系统可以被配置为保持物体的一部分并将物体的一部分朝向平台移动，使得物体的该部分基本上符合平台的形状。

10. 发明授权

US11623766B2 Systems and methods for manufacturing aircraft 有权
公开(公告)号：US11623766B2
公开(公告)日：2023-04-11
申请号：US17505505
申请日：2021-10-19
申请人： The Boeing Company
发明人： Jeremy Justice , Daniel Richard Smith, Jr. , Darrell Darwin Jones
IPC分类号： B64F5/10 , B23P21/00 , B62D65/02
摘要： Systems and methods for manufacturing aircraft are disclosed. For example, an aircraft manufacturing system for repetitively manufacturing aircraft comprises a first manufacturing zone configured to repetitively manufacture first aircraft subassemblies, a second manufacturing zone configured to repetitively manufacture second aircraft subassemblies, and a third manufacturing zone configured to receive the first aircraft subassemblies from the first manufacturing zone, to receive the second aircraft subassemblies from the second manufacturing zone, and to repetitively assemble the first aircraft subassemblies and the second aircraft subassemblies into the aircraft. In another example, a method for repetitively manufacturing aircraft assemblies comprises assembling first aircraft subassemblies and second aircraft subassemblies in parallel on separate assembly lines at a common geographic region; and transferring the first aircraft subassemblies and the second aircraft subassemblies to a final assembly facility located in the same common geographic region.

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