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1. 发明授权

US10035609B2 Wireless engine monitoring system for environmental emission control and aircraft networking 有权
公开(公告)号：US10035609B2
公开(公告)日：2018-07-31
申请号：US15063856
申请日：2016-03-08
申请人： HARRIS CORPORATION
发明人： James J. Ziarno
IPC分类号： B64D45/00 , B64F5/00 , G07C5/00 , G07C5/08
CPC分类号： B64D45/00 , B64F5/60 , F02C9/00 , F05D2260/80 , G05B23/0283 , G05B2219/15117 , G05B2219/45071 , G07C5/008 , G07C5/0808 , G07C5/085
摘要： A wireless engine monitoring system for an aircraft engine includes a housing and wireless transceiver that receives engine data, including engine data relating to environmental engine emissions. A processor processes the engine data and generates an alarm report when the environmental engine emissions exceed a threshold.

2. 发明申请

US20180113425A1 AUTOMATED SYSTEM AND METHOD TO MANUFACTURE AERONAUTIC JUNCTION PARTS 审中-公开
公开(公告)号：US20180113425A1
公开(公告)日：2018-04-26
申请号：US15335202
申请日：2016-10-26
申请人： Embraer S.A.
发明人： Megumi NAKASHIMA , Erik Spada DA SILVA , Lincoln José LEPRI , Pércio Roiz SAITO
IPC分类号： G05B13/04 , B23C3/13
CPC分类号： G05B13/041 , B23C3/13 , B23C2215/04 , B23C2220/28 , B23C2260/56 , B64C1/26 , B64F5/10 , G05B2219/33198 , G05B2219/37355 , G05B2219/45071
摘要： Every junction part for an airplane wing is manufactured with overmaterial. Each part is measured with a laser based interferometer or other scanning technique and the “as built” measurements are compared with a model to generate a new trajectory milling program to fill or prevent gaps between parts using a points cloud and B-Spline algorithm to generate a new surface to be milled. Once the program is generated (new trajectories) and post processed, it is sent to a milling machine to perform overmaterial milling on already milled parts with overmaterial. This technique can be used to eliminate gaps between junction parts and the corresponding need for shims.

3. 发明授权

US09815202B2 Control method for robot apparatus, computer readable recording medium, and robot apparatus 有权
公开(公告)号：US09815202B2
公开(公告)日：2017-11-14
申请号：US14792987
申请日：2015-07-07
申请人： CANON KABUSHIKI KAISHA
发明人： Tsutomu Osaka , Takahiro Ishikawa , Shunsuke Kawamura
IPC分类号： G06F19/00 , B25J9/16 , B25J9/06 , G05B19/404
CPC分类号： B25J9/1692 , B25J9/06 , B25J9/1602 , B25J9/1628 , G05B19/404 , G05B2219/14016 , G05B2219/14126 , G05B2219/37325 , G05B2219/39206 , G05B2219/42318 , G05B2219/45071 , Y10S901/02 , Y10S901/09
摘要： Semi-closed control or fully closed control is selected as a control system for a joint using a motor configured to drive a joint of a robot arm via a reduction gear, an input-side encoder, and an output-side encoder, the semi-closed control being control in which an output of the input-side encoder is used, the fully closed control being control in which an output of the output-side encoder is used. A test run is performed plural times in which the robot arm is caused to perform a specific operation while semi-closed control is being performed on the joint, and semi-closed control or fully closed control is selected using outputs of the output-side encoder obtained in the test runs or in accordance with the content of a task that the robot arm is to be caused to perform.

4. 发明申请

US20170066044A1 MOBILE PLATFORMS FOR PERFORMING OPERATIONS ALONG AN EXTERIOR OF A FUSELAGE ASSEMBLY 审中-公开
标题翻译：用于执行装配操作的移动平台
公开(公告)号：US20170066044A1
公开(公告)日：2017-03-09
申请号：US15352524
申请日：2016-11-15
申请人： The Boeing Company
发明人： Harinder S. Oberoi , Richard Griffith Reese, IV , Kevin Marion Barrick , Quang T. Do , Jeffrey Lawrence Miller , Vanco Stojanoski
IPC分类号： B21J15/28 , B21J15/32 , B23P19/10 , F16B19/06 , B64F5/00 , B25J9/16 , B25J11/00 , G05B19/418 , G05D1/00 , G05D3/12 , B21J15/14 , B25J5/00
CPC分类号： B21J15/28 , B21J15/02 , B21J15/10 , B21J15/142 , B21J15/32 , B21J15/40 , B23P19/10 , B23P21/002 , B23P2700/00 , B25B5/163 , B25J5/007 , B25J9/1682 , B25J9/1687 , B25J9/1697 , B25J11/005 , B25J11/007 , B29C39/026 , B29C39/10 , B29C39/123 , B29C39/22 , B29C45/14336 , B29C2045/14368 , B29C2793/0081 , B29K2715/00 , B29L2031/748 , B60G3/145 , B60G7/001 , B60G7/008 , B60G2204/143 , B60G2204/418 , B60G2206/8207 , B60G2300/60 , B60P3/025 , B64C1/06 , B64F5/10 , B64F5/50 , F16B19/06 , G05B19/41805 , G05B2219/45071 , G05D1/0088 , G05D3/12 , Y02P90/86 , Y10S901/01 , Y10S901/02 , Y10S901/41
摘要： A method and apparatus for performing an assembly operation. A tool may be macro-positioned relative to an exterior of a fuselage assembly. The tool may be micro-positioned relative to a particular location on the exterior of the fuselage assembly. An end effector is removably associated with an external robotic device associated with an external mobile platform. The tool is removably associated with the end effector. An assembly operation may be performed at the particular location on the panel using the tool.
摘要翻译：一种用于执行组装操作的方法和装置。相对于机身组件的外部，工具可以被宏定位。该工具可以相对于机身组件的外部上的特定位置被微定位。端部执行器可移除地与与外部移动平台相关联的外部机器人装置相关联。该工具可拆卸地与末端执行器相关联。可以使用该工具在面板上的特定位置处执行组装操作。

5. 发明申请

US20160048113A1 SYSTEM AND METHOD FOR ADVANCED PROCESS CONTROL 有权
标题翻译：高级过程控制系统与方法
公开(公告)号：US20160048113A1
公开(公告)日：2016-02-18
申请号：US14459041
申请日：2014-08-13
申请人： HONEYWELL INTERNATIONAL INC.
发明人： GOBINATH PANDURANGAN , KISHEN MANJUNATH , SANJAY KANTILAL DAVE
IPC分类号： G05B13/04
CPC分类号： G05B13/04 , G05B13/045 , G05B13/048 , G05B17/02 , G05B23/0243 , G05B2219/14016 , G05B2219/14126 , G05B2219/37325 , G05B2219/42318 , G05B2219/45071
摘要： A system and method for performing management and diagnostic functions in an advanced process control (APC) system. An APC management computer retrieves operating process data from an APC control computer and performs an iterative step test on the APC system. The iterative step test modifies at least one test parameter of the operating process data and identifies changes to a set of remaining parameters of the operating process data resulting from modification of the test parameter. The APC management computer determines at least one process variable from the iterative step test and generates at least one process model based on the process variable. The APC management computer transmits the process model to the APC control computer.
摘要翻译：一种用于在先进过程控制（APC）系统中执行管理和诊断功能的系统和方法。 APC管理计算机从APC控制计算机检索操作过程数据，并对APC系统执行迭代步骤测试。迭代步骤测试修改操作过程数据的至少一个测试参数，并识别由修改测试参数导致的操作过程数据的一组剩余参数的变化。 APC管理计算机从迭代步骤测试中确定至少一个过程变量，并基于过程变量生成至少一个过程模型。 APC管理计算机将过程模型发送到APC控制计算机。

6. 发明申请

US20160009420A1 Assembly Fixture for Supporting a Fuselage Assembly 审中-公开
标题翻译：用于支持机身组件的组装夹具
公开(公告)号：US20160009420A1
公开(公告)日：2016-01-14
申请号：US14559277
申请日：2014-12-03
申请人： The Boeing Company
发明人： Harinder S. Oberoi , Richard Griffith Reese, IV , Kevin Marion Barrick , Quang T. Do , Alan S. Draper , Alfredo Jose Gerosa , Branko Sarh , Gregory Gudzinski
IPC分类号： B64F5/00
CPC分类号： B21J15/28 , B21J15/02 , B21J15/10 , B21J15/142 , B21J15/32 , B21J15/40 , B23P19/10 , B23P21/002 , B23P2700/00 , B23P2700/01 , B25B5/163 , B25J5/007 , B25J9/1682 , B25J9/1687 , B25J9/1697 , B25J11/005 , B25J11/007 , B29C39/026 , B29C39/10 , B29C39/123 , B29C39/22 , B29C45/14336 , B29C2045/14368 , B29C2793/0081 , B29K2715/00 , B29L2031/748 , B60G3/145 , B60G7/001 , B60G7/008 , B60G2204/143 , B60G2204/418 , B60G2206/8207 , B60G2300/60 , B60P3/025 , B64C1/06 , B64F5/10 , B64F5/50 , F16B19/06 , G05B19/41805 , G05B2219/45071 , G05D1/0088 , G05D3/12 , Y02P90/86 , Y10S901/01 , Y10S901/02 , Y10S901/41
摘要： A method and apparatus for building an assembly fixture for holding a fuselage assembly. A number of cradle fixtures may be driven across a floor to an assembly area. The number of cradle fixtures may be configured to form the assembly fixture.
摘要翻译：一种用于构建用于保持机身组件的组装夹具的方法和装置。一些托架固定装置可以穿过地板被驱动到组装区域。托架固定件的数量可以被配置成形成装配夹具。

7. 发明申请

US20160009418A1 Clamping Feet for an End Effector 审中-公开
标题翻译：夹紧脚的终点效应器
公开(公告)号：US20160009418A1
公开(公告)日：2016-01-14
申请号：US14559191
申请日：2014-12-03
申请人： The Boeing Company
发明人： Harinder S. Oberoi , Melissa Ann Findlay , Jorge Alberto Arriaga , Branko Sarh , Alan S. Draper
IPC分类号： B64F5/00 , B29C39/12 , B29C39/22 , B25B5/16
CPC分类号： B21J15/28 , B21J15/02 , B21J15/10 , B21J15/142 , B21J15/32 , B21J15/40 , B23P19/10 , B23P21/002 , B23P2700/00 , B25B5/163 , B25J5/007 , B25J9/1682 , B25J9/1687 , B25J9/1697 , B25J11/005 , B25J11/007 , B29C39/026 , B29C39/10 , B29C39/123 , B29C39/22 , B29C45/14336 , B29C2045/14368 , B29C2793/0081 , B29K2715/00 , B29L2031/748 , B60G3/145 , B60G7/001 , B60G7/008 , B60G2204/143 , B60G2204/418 , B60G2206/8207 , B60G2300/60 , B60P3/025 , B64C1/06 , B64F5/10 , B64F5/50 , F16B19/06 , G05B19/41805 , G05B2219/45071 , G05D1/0088 , G05D3/12 , Y02P90/86 , Y10S901/01 , Y10S901/02 , Y10S901/41
摘要： An attachment for an end effector. The attachment may include a clamp and a foot adhesively bonded to an edge of the clamp and having a set of interlocking features that form a mechanical interlock with the clamp.
摘要翻译：末端执行器的附件。附件可以包括夹具和脚部，其粘合地结合到夹具的边缘并且具有与夹具形成机械互锁的一组互锁特征。

8. 发明申请

US20160008869A1 Two-Stage Riveting 有权
标题翻译：两阶段铆接
公开(公告)号：US20160008869A1
公开(公告)日：2016-01-14
申请号：US14559483
申请日：2014-12-03
申请人： The Boeing Company
发明人： Harinder S. Oberoi , Melissa Ann Findlay , Branko Sarh , Alan S. Draper , Jorge Alberto Arriaga
IPC分类号： B21J15/28 , B21J15/14 , F16B19/06 , B21J15/02 , B25J11/00 , B25J9/16
CPC分类号： B21J15/28 , B21J15/02 , B21J15/10 , B21J15/142 , B21J15/32 , B21J15/40 , B23P19/10 , B23P21/002 , B23P2700/00 , B25B5/163 , B25J5/007 , B25J9/1682 , B25J9/1687 , B25J9/1697 , B25J11/005 , B25J11/007 , B29C39/026 , B29C39/10 , B29C39/123 , B29C39/22 , B29C45/14336 , B29C2045/14368 , B29C2793/0081 , B29K2715/00 , B29L2031/748 , B60G3/145 , B60G7/001 , B60G7/008 , B60G2204/143 , B60G2204/418 , B60G2206/8207 , B60G2300/60 , B60P3/025 , B64C1/06 , B64F5/10 , B64F5/50 , F16B19/06 , G05B19/41805 , G05B2219/45071 , G05D1/0088 , G05D3/12 , Y02P90/86 , Y10S901/01 , Y10S901/02 , Y10S901/41
摘要： A method and apparatus for fastening two parts together. An initial interference fit may be created between a fastener and at least a portion of a hole extending through the two parts while maintaining a force equilibrium. A final interference fit may be created between the fastener and the hole, while maintaining a new force equilibrium.
摘要翻译：一种用于将两部分紧固在一起的方法和装置。可以在紧固件和延伸穿过两个部件的孔的至少一部分之间产生初始的过盈配合，同时保持力平衡。可以在紧固件和孔之间产生最终的过盈配合，同时保持新的力平衡。

9. 发明申请

US20150344149A1 FAILURE ANALYSIS SYSTEM 有权
标题翻译：故障分析系统
公开(公告)号：US20150344149A1
公开(公告)日：2015-12-03
申请号：US14490458
申请日：2014-09-18
申请人： THE BOEING COMPANY
发明人： Randall J. Mumaw , Roger Nicholson , Lars Fucke
IPC分类号： B64D45/00 , G07C5/08
CPC分类号： B64D45/00 , B64D2045/0085 , G05B23/0251 , G05B23/027 , G05B2219/45071 , G07C5/0808 , G07C5/0816 , G07C5/0841
摘要： A failure analysis system for monitoring sub-system failures in an aircraft that comprises a plurality of sub-systems, the aircraft having a plurality of functions, wherein each function is available when one or more associated sub-systems is operating correctly. The failure analysis system comprising: a plurality of monitors for monitoring the status of one or more sub-systems of the aircraft and determining if a failure has occurred; a memory arranged to store a list of a plurality of flight phases or operating modes to be completed by the monitored system and data associating one or more of the functions with each flight phase or operating mode; and a processor in communication with the monitors and the memory and arranged to model the response of the sub-systems to a failure determined by the monitors to identify which functions required by the flight phases or operating modes are degraded or are not available.
摘要翻译：一种用于监视包括多个子系统的飞机中的子系统故障的故障分析系统，所述飞机具有多个功能，其中当一个或多个相关联的子系统正常工作时，每个功能可用。该故障分析系统包括：多个监视器，用于监视飞行器的一个或多个子系统的状态并确定是否发生故障; 存储器，其被布置成存储由所监视的系统完成的多个飞行阶段或操作模式的列表以及将一个或多个功能与每个飞行阶段或操作模式相关联的数据; 以及与监视器和存储器通信的处理器，并且被布置成将子系统的响应建模到由监视器确定的故障，以识别飞行阶段或操作模式所需的功能降级或不可用。

10. 发明授权

US09149929B2 Methods and systems for inspection sensor placement 有权
标题翻译：检查传感器放置的方法和系统
公开(公告)号：US09149929B2
公开(公告)日：2015-10-06
申请号：US12787885
申请日：2010-05-26
申请人： William P. Motzer , Gary E. Georgeson , Scott W. Lea , Peter J. Hellenbrand , James J. Troy
发明人： William P. Motzer , Gary E. Georgeson , Scott W. Lea , Peter J. Hellenbrand , James J. Troy
IPC分类号： B25J9/16 , B25J9/06
CPC分类号： B25J9/162 , B25J9/06 , B25J9/065 , B25J9/1694 , G05B2219/39014 , G05B2219/39024 , G05B2219/40039 , G05B2219/40234 , G05B2219/45071
摘要： Methods and systems are provided for positioning a remote sensor within a target object. An articulated robotic system is coupled to the remote sensor. A positioning system determines a position of the target object to be inspected and determines a first position of the remote sensor. A control system calibrates a virtual representation of the target object with respect to the position of the target object, and tracks movement of the remote sensor relative to the target object.
摘要翻译：提供了用于将远程传感器定位在目标对象内的方法和系统。铰接机器人系统耦合到远程传感器。定位系统确定要检查的目标对象的位置并确定远程传感器的第一位置。控制系统相对于目标对象的位置校准目标对象的虚拟表示，并跟踪远程传感器相对于目标对象的移动。

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