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91. 发明申请

US20160101877A1 SUSPENSION STRUT SERVICING 审中-公开
标题翻译：停牌服务
公开(公告)号：US20160101877A1
公开(公告)日：2016-04-14
申请号：US14891599
申请日：2014-05-09
申请人： AIRBUS OPERATIONS LIMITED
发明人： Alan SHEPHERD , Julian DUNCAN
IPC分类号： B64F5/00 , G01F23/296 , G01M17/04
CPC分类号： G01M17/04 , B64C25/60 , B64C2230/02 , B64F5/60 , F16F9/063 , G01F23/296 , Y02T50/166
摘要： A method for servicing a landing gear strut in service supporting an aircraft including: determining a current amount of damping fluid in the landing gear strut; determining a required amount of the damping fluid for correct servicing of the landing gear strut; and adjusting the current amount of damping fluid in the landing gear strut so that the current amount of damping fluid complies with the required amount of damping fluid.
摘要翻译：一种用于维修支撑飞行器的起落架支柱的方法，包括：确定起落架支柱中的阻尼流体的当前量; 确定用于正确维修起落架支柱的阻尼流体的所需量; 并且调节起落架支柱中的阻尼流体的当前量，使得阻尼流体的当前量符合所需量的阻尼流体。

92. 发明申请

US20160097842A1 AUTOMATED MOBILE INVERTIBLE MEASUREMENT DEVICE 有权
标题翻译：自动移动可逆测量装置
公开(公告)号：US20160097842A1
公开(公告)日：2016-04-07
申请号：US14506846
申请日：2014-10-06
申请人： The Boeing Company
发明人： Kyle S. Biondich , Truong D. Pham , Zachary Talus
IPC分类号： G01S7/481 , G01S7/48 , G01S17/06
CPC分类号： G01S7/481 , B64F5/10 , B64F5/60 , G01C15/002 , G01S7/4808 , G01S17/66 , G05D1/0236 , G05D1/0255 , G05D2201/0207
摘要： An apparatus is utilized for measuring a circumference. The apparatus includes a body section, and at least one wheel rotatably attached to the body section. Additionally, at least one vacuum generating device is disposed on the body section, and is configured to generate an effective amount of vacuum between the body section and an adjacent arcuate surface which is sufficient to retain the body section against the arcuate surface. At least one of a reflector and a gap detector may also be affixed to the body section.
摘要翻译：使用一种测量圆周的装置。该装置包括主体部分和至少一个可旋转地附接到主体部分的轮。此外，至少一个真空发生装置设置在主体部分上，并且被构造成在主体部分和相邻的弓形表面之间产生有效量的真空，其足以将主体部分保持抵靠在弓形表面上。反射器和间隙检测器中的至少一个也可以固定到主体部分。

93. 发明申请

US20160096637A1 Automated Non-Destructive Inspection of Surface Skins Using Transporter System 审中-公开
标题翻译：使用运输系统对表面皮肤进行自动非破坏性检测
公开(公告)号：US20160096637A1
公开(公告)日：2016-04-07
申请号：US14966516
申请日：2015-12-11
申请人： The Boeing Company
发明人： James J. Troy , William P. Motzer , Scott W. Lea , James C. Kennedy , Michael C. Hutchinson
IPC分类号： B64F5/00 , B62D63/06 , B62D63/08 , B62D49/06
CPC分类号： B62D49/0642 , B62D49/065 , B62D63/068 , B62D63/08 , B64F5/40 , B64F5/60 , G01N29/043 , G01N29/225 , G01N29/26 , G01N29/265 , G01N29/28 , G01N2291/0231 , G01N2291/26 , G01N2291/2694
摘要： Systems and methods for automated maintenance of the top and bottom surfaces or skins of an integrally stiffened hollow structure (e.g., a horizontal stabilizer) using surface crawling vehicles. Each system uses dynamically controlled magnetic coupling to couple an external drive tractor to a pair of passive trailers disposed in the interior of the hollow structure on opposite sides of a vertical structural element. The external drive tractor is also coupled to an external maintenance tool, which the tractor pushes or pulls across the surface skin to perform a maintenance function. The systems allow maintenance operations to be performed on both surface skins without turning the hollow structure over. Each system is modular and can be transported to and easily set up in a building or factory.
摘要翻译：使用表面爬行车辆自动维护整体加固的中空结构（例如水平稳定器）的顶面和底面或表皮的系统和方法。每个系统使用动态控制的磁耦合将外部驱动拖拉机耦合到设置在垂直结构元件的相对侧上的中空结构内部的一对被动拖车。外部驱动拖拉机还耦合到外部维护工具，拖拉机推动或拉动穿过表面皮肤以执行维护功能。这些系统允许在两个表面皮肤上执行维护操作，而不使中空结构转动。每个系统都是模块化的，可以运输到建筑物或工厂容易地设置。

94. 发明申请

US20160019212A1 MAINTENANCE ASSISTANCE FOR AN AIRCRAFT BY AUGMENTED REALITY 审中-公开
标题翻译：维护现有的飞机维修保养
公开(公告)号：US20160019212A1
公开(公告)日：2016-01-21
申请号：US14805115
申请日：2015-07-21
申请人： Airbus Operations (SAS)
发明人： Siegfried Soldani
IPC分类号： G06F17/30 , G09G5/00 , G06T1/00 , B64F5/00 , G06K9/32 , G06K9/22 , G06F3/01 , G06T19/00 , G06T15/00
CPC分类号： G06F17/30047 , B64F5/40 , B64F5/60 , G06F3/011 , G06F3/147 , G06K9/22 , G06K9/3241 , G06Q10/20 , G06Q50/30 , G06T1/0007 , G06T15/005 , G06T19/006 , G06T2200/04 , G06T2200/28 , G06T2207/10004 , G06T2210/61 , G06T2215/16 , G06T2219/004 , G09G5/00 , G09G2354/00 , G09G2370/022 , G09G2380/12
摘要： A method for supporting aircraft maintenance, performed in a system comprising a display selection device and a portable device with a camera and an augmented reality display. The method comprises the steps of acquiring images of an equipment of the aircraft with the camera, and sending them to the display selection device; identifying the equipment present in these images with the display selection device and determining the identifier thereof, referred to as the useful identifier; on the basis of the useful identifier, sending maintenance assistance data with the display selection device to the augmented reality display; in response, displaying, in augmented reality, images corresponding to the data with the augmented reality display device. The method also comprises steps for displaying guidance data guiding towards one equipment in particular. A device for implementing such a method is also disclosed.
摘要翻译：一种用于支持飞机维护的方法，在包括显示器选择装置和具有相机的便携式装置和增强现实显示器的系统中执行。该方法包括以下步骤：用相机获取飞机设备的图像，并将其发送到显示选择装置; 使用显示选择装置识别这些图像中存在的设备，并确定其标识符，称为有用标识符; 基于有用标识符，将显示选择装置的维护辅助数据发送到增强现实显示; 作为响应，在增强现实中显示与增强现实显示装置对应的数据的图像。该方法还包括用于显示特别指向一个设备的引导数据的步骤。还公开了一种用于实现这种方法的装置。

95. 发明授权

US09227738B2 Automated diagnostic inspection of mechanical controls 有权
标题翻译：机械控制自动诊断检查
公开(公告)号：US09227738B2
公开(公告)日：2016-01-05
申请号：US13731974
申请日：2012-12-31
申请人： BELL HELICOPTER TEXTRON INC.
发明人： John R. Wittmaak, Jr. , Jayme Gonzalez , Charles Eric Covington , Carlos Fenny
IPC分类号： B64F5/00 , G05B23/02
CPC分类号： B64F5/0045 , B64F5/60 , G05B23/0256
摘要： A system and method to diagnosis an actuator of a flight control system. The system and method includes interfacing a diagnostic computer to the flight control system, commanding movement of an actuator with the diagnostic computer via the flight control system, measuring performance of the actuator via the diagnostic computer, and comparing the measured performance of the actuator with allowable performance values.
摘要翻译：一种用于诊断飞行控制系统的执行器的系统和方法。该系统和方法包括将诊断计算机连接到飞行控制系统，通过飞行控制系统命令致动器与诊断计算机的运动，通过诊断计算机测量致动器的性能，并将执行器的测量性能与允许的性能价值。

96. 发明授权

US09221506B1 Location tracking and motion control of automated marking device 有权
标题翻译：自动标记装置的位置跟踪和运动控制
公开(公告)号：US09221506B1
公开(公告)日：2015-12-29
申请号：US13948195
申请日：2013-07-23
申请人： The Boeing Company
发明人： Gary E. Georgeson , John R. Linn , James J. Troy , Karl Edward Nelson , Daniel J. Wright , Scott W. Lea
IPC分类号： B25J5/00 , B62D57/024 , G05D1/02 , B05C1/00 , B05D7/00 , G05D1/00 , B64F5/00 , F41J2/00 , B62D55/265 , B60B19/00
CPC分类号： B62D57/024 , B05C1/00 , B05D7/00 , B25J5/007 , B60B19/003 , B64F5/40 , B64F5/60 , F02K1/1207 , F02K1/763 , G05D1/00 , G05D1/0236 , G05D1/0282 , Y10S901/01
摘要： A system in accordance with one embodiment comprises a marking device attached to a holonomic-motion crawler vehicle capable of movement on non-horizontal surfaces. Modular attachment and motion control interfaces on the platform allow attachment of various types of marking and non-destructive inspection (NDI) sensor modules. The crawling vehicle marks the location of sub-surface features on an aircraft skin or overlaid patch (doubler) using a pen or sticker or tape applicator that is guided based on either a 3-D CAD model or NDI data collected as the vehicle crawls. A second embodiment utilizes an automated NDI scanner to collect 2-D image data of the substructure to enable manual or automated feature/edge selection for marking. Location tracking of the marking device can be implemented using a local positioning system or a motion capture system.
摘要翻译：根据一个实施例的系统包括连接到能够在非水平表面上移动的整体式履带式车辆的标记装置。平台上的模块化附件和运动控制界面允许连接各种类型的标记和非破坏性检测（NDI）传感器模块。爬行车辆使用笔或贴纸或胶带施加器来标记飞机皮肤上的子表面特征的位置或覆盖的贴片（双倍），该笔或贴纸或胶带施加器基于车辆爬行时收集的3-D CAD模型或NDI数据而被引导。第二实施例利用自动NDI扫描器来收集子结构的二维图像数据，以使得能够进行标记的手动或自动特征/边缘选择。标记装置的位置跟踪可以使用本地定位系统或运动捕捉系统来实现。

97. 发明授权

US09216830B2 Method and device for detecting oscillatory failures in a position servocontrol subsystem of an aircraft control surface 有权
标题翻译：用于检测飞机控制表面的位置伺服控制子系统中的振荡故障的方法和装置
公开(公告)号：US09216830B2
公开(公告)日：2015-12-22
申请号：US13904382
申请日：2013-05-29
申请人： AIRBUS OPERATIONS SAS , UNIVERSITE BORDEAUX 1
发明人： Philippe Goupil , Olivier Babando , Mohcine Sifi , Loïc Lavigne , Franck Cazaurang
IPC分类号： B64F5/00 , G05B23/02
CPC分类号： B64F5/0045 , B64F5/60 , G05B23/0254
摘要： Methods and devices for detecting oscillatory faults in a positional servocontrol arrangement for an aircraft control surface are provided. The detection device estimates a reference position of the control surface and, with the aid of a model in which at each iteration a residual value of the previous iteration, multiplied by a dynamic gain, is injected, detects an oscillatory fault with the aid of this reference position.
摘要翻译：提供了用于检测用于飞行器控制表面的位置伺服控制装置中的振荡故障的方法和装置。检测装置估计控制表面的参考位置，并借助于其中在每次迭代中注入前一次迭代的残余值乘以动态增益的模型，借助于此来检测振荡故障参考位置。

98. 发明申请

US20150360135A1 HELICOPTER RETENTION PLATE HARDWARE STAND 审中-公开
标题翻译：直升机保持板硬件架
公开(公告)号：US20150360135A1
公开(公告)日：2015-12-17
申请号：US14721147
申请日：2015-05-26
申请人： Stephen George MOSCICKI, SR.
发明人： Stephen George MOSCICKI, SR.
IPC分类号： A63H27/00 , B25H1/04
CPC分类号： A63H27/001 , B64F5/10 , B64F5/60
摘要： A standardized hardware stand for organizing the components and subcomponents of helicopter retention plates is provided. The hardware stand could be adapted to be distributed to all air stations so that a repeatable, teachable skill set can be developed, minimizing costly vibratory analysis, problematic clamp-up procedures, and other unnecessary additional maintenance during re-installation of the helicopter retention plates. The hardware stand includes a mock plate forming a plurality of mimicking holes and identifying marks, each dimensioned and adapted to match that of each retention plate maintained, and wherein the mock plate is perpendicularly and rotatably joined to an attachments stem.
摘要翻译：提供了用于组织直升机固定板的部件和子部件的标准化硬件架构。硬件支架可以适应于分配给所有的空气站，从而可以开发可重复的，可教导的技能，最小化昂贵的振动分析，有问题的夹紧程序以及重新安装直升机保持板时的其他不必要的附加维护。五金支架包括形成多个模拟孔和识别标记的模拟板，每个模拟孔的尺寸和尺寸适于与保持的每个保持板的尺寸相匹配，并且其中模拟板垂直和可旋转地连接到附接杆上。

99. 发明授权

US09205934B2 Adaptive oscillatory fault monitoring 有权
标题翻译：自适应振荡故障监测
公开(公告)号：US09205934B2
公开(公告)日：2015-12-08
申请号：US14166518
申请日：2014-01-28
申请人： Gulfstream Aerospace Corporation
发明人： Ventseslav Rashkov , Michael Curtis
IPC分类号： B64F5/00 , G01R23/15 , G01R31/00 , G01N29/12
CPC分类号： B64F5/0045 , B64F5/60 , G01N29/12 , G01N2291/2694 , G01R23/15 , G01R31/008
摘要： Systems, media, and methods are provided for oscillation monitoring. An aircraft system includes a first oscillation monitoring module and a second oscillation monitoring module. The first oscillation monitoring module is configured to select first oscillating portions of an input signal, generate a frequency signal that indicates a frequency of the first oscillating portions, and generate a first failure signal in response to the frequency of the first oscillating portions exceeding first oscillatory fault detection requirements for the input signal. The second oscillation monitoring module is configured to select second oscillating portions of the input signal based on the frequency signal generated by the first oscillation monitoring module and to generate a second failure signal in response to a frequency of the second oscillating portions exceeding second oscillatory fault detection requirements for the input signal.
摘要翻译：提供系统，介质和方法进行振荡监测。飞机系统包括第一振荡监测模块和第二振荡监测模块。第一振荡监视模块被配置为选择输入信号的第一振荡部分，产生指示第一振荡部分的频率的频率信号，并响应于第一振荡部分的频率超过第一振荡产生第一故障信号输入信号的故障检测要求。第二振荡监视模块被配置为基于由第一振荡监测模块产生的频率信号来选择输入信号的第二振荡部分，并且响应于第二振荡部分的频率超过第二振荡故障检测而产生第二故障信号对输入信号的要求。

100. 发明申请

US20150344156A1 STABLE GROUNDING SYSTEM TO AVOID CATASTROPHIC ELECTRICAL FAILURES IN FIBER-REINFORCED COMPOSITE AIRCRAFT 审中-公开
标题翻译：稳定的接地系统，以避免光纤加固复合飞机中的电气故障
公开(公告)号：US20150344156A1
公开(公告)日：2015-12-03
申请号：US14826127
申请日：2015-08-13
申请人： SMART DRILLING AND COMPLETION, INC.
发明人： WILLIAM BANNING VAIL, III , TOMISLAV SKERL , PAUL B. SCHWINBERG , STEVEN T. MOMII
IPC分类号： B64F5/00 , G01R31/00
CPC分类号： G01R31/008 , B64F5/60
摘要： Methods and apparatus are described to detect, measure, and determine the presence of unknown Groundloop currents flowing through unidentified circuit pathways within the wiring system distributed within a portion of a fuselage of an airplane substantially made from fiber-reinforced composite materials to avoid catastrophic failures of the electrical system within such an airplane.
摘要翻译：描述了用于检测，测量和确定分布在基本上由纤维增强的复合材料制成的飞机的机身的一部分内的布线系统中流经未识别的电路路径的未知的地球环流的存在，以避免灾难性故障这种飞机内的电气系统。

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