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1. 发明授权

US07552027B2 Method and system for quantifying damage in a structure 有权
标题翻译：用于量化结构损伤的方法和系统
公开(公告)号：US07552027B2
公开(公告)日：2009-06-23
申请号：US11867210
申请日：2007-10-04
申请人： Justin D. Kearns , Jeong-Beom Ihn
发明人： Justin D. Kearns , Jeong-Beom Ihn
IPC分类号： G06F19/00
CPC分类号： G01N29/4481
摘要： A method for quantifying damage in a test structure having a plurality of transducer units coupled to at least one portion of the test structure includes: (a) training an evaluating algorithmic system coupled with the transducer units to establish a trained algorithmic system able to recognize a plurality of characteristics of signals traversing a plurality of paths through a training structure substantially similar to the test structure after the training structure is damaged. Each path is situated between a respective pair of transducer units coupled to the training structure; the plurality of characteristics relates each path to a plurality of physical aspects of the damage. A trained algorithmic system is employed to recognize the plurality of characteristics of signals traversing paths in the test structure to effect the quantifying. The plurality of physical aspects includes less than ten physical aspects.
摘要翻译：一种用于量化具有耦合到测试结构的至少一部分的多个换能器单元的测试结构中的损伤的方法包括：（a）训练与所述换能器单元耦合的评估算法系统，以建立训练有素的算法系统，在训练结构被损坏之后，通过穿过训练结构的多个路径的信号的多个特征基本上类似于测试结构。每个路径位于耦合到训练结构的相应的一对换能器单元之间; 多个特征将每个路径与损坏的多个物理方面相关联。采用经过训练的算法系统来识别测试结构中穿过路径的信号的多个特征，以实现量化。多个物理方面包括少于十个物理方面。

2. 发明申请

US20090093999A1 METHOD AND SYSTEM FOR QUANTIFYING DAMAGE IN A STRUCTURE 有权
标题翻译：用于量化结构损伤的方法和系统
公开(公告)号：US20090093999A1
公开(公告)日：2009-04-09
申请号：US11867210
申请日：2007-10-04
申请人： Justin D. Kearns , Jeong-Beom Ihn
发明人： Justin D. Kearns , Jeong-Beom Ihn
IPC分类号： G06F11/30
CPC分类号： G01N29/4481
摘要： A method for quantifying damage in a test structure having a plurality of transducer units coupled to at least one portion of the test structure includes: (a) training an evaluating algorithmic system coupled with the transducer units to establish a trained algorithmic system able to recognize a plurality of characteristics of signals traversing a plurality of paths through a training structure substantially similar to the test structure after the training structure is damaged. Each path is situated between a respective pair of transducer units coupled to the training structure; the plurality of characteristics relates each path to a plurality of physical aspects of the damage. A trained algorithmic system is employed to recognize the plurality of characteristics of signals traversing paths in the test structure to effect the quantifying. The plurality of physical aspects includes less than ten physical aspects.
摘要翻译：一种用于量化具有耦合到测试结构的至少一部分的多个换能器单元的测试结构中的损伤的方法包括：（a）训练与所述换能器单元耦合的评估算法系统，以建立训练有素的算法系统，在训练结构被损坏之后，通过穿过训练结构的多个路径的信号的多个特征基本上类似于测试结构。每个路径位于耦合到训练结构的相应的一对换能器单元之间; 多个特征将每个路径与损坏的多个物理方面相关联。采用经过训练的算法系统来识别测试结构中穿过路径的信号的多个特征，以实现量化。多个物理方面包括少于十个物理方面。

3. 发明授权

US09045216B2 Flight vehicle fairing having vibration-damping blankets 有权
标题翻译：具有减震毯的飞行器整流罩
公开(公告)号：US09045216B2
公开(公告)日：2015-06-02
申请号：US13169295
申请日：2011-06-27
申请人： Justin Christenson , Herbert L. Hoffman , Juhn-Shyue Lin , Gary R. Chewning , Alan Edgar Landmann , Adrian Viisoreanu , Hugh Poling , Balamurugan R. Annamalai , Justin D. Kearns , Jason Alexander Gordon
发明人： Justin Christenson , Herbert L. Hoffman , Juhn-Shyue Lin , Gary R. Chewning , Alan Edgar Landmann , Adrian Viisoreanu , Hugh Poling , Balamurugan R. Annamalai , Justin D. Kearns , Jason Alexander Gordon
IPC分类号： B64C1/40 , B64C1/26
CPC分类号： B64C1/26 , B64C1/40 , Y02T50/46 , Y10T29/49723 , Y10T29/49826
摘要： Vibration-damping blankets are attached to the back surfaces of fairing panels of a flight vehicle (e.g., an aircraft or spacecraft) to reduce vibration, fatigue, structure and airborne transmitted energy, and cabin noise. In one case, the flight vehicle fairing has an exterior comprising exterior surfaces of a multiplicity of removable panels. A method of retrofitting the flight vehicle with vibration-damping blankets comprises: removing a panel from the flight vehicle exterior; attaching a vibration-damping blanket to a back surface of the removed panel; and installing the panel with attached vibration-damping blanket on the flight vehicle with the exterior surface of the panel forming part of the flight vehicle exterior. In one embodiment, the vibration-damping blanket comprises polymeric (e.g., aromatic polyamide) fibers in a nonwoven structure.
摘要翻译：减振毯连接到飞行器（例如飞行器或航天器）的整流罩的背面，以减少振动，疲劳，结构和空中传播的能量以及舱室噪音。在一种情况下，飞行器整流罩具有包括多个可移除面板的外表面的外部。用减振毯改装飞行器的方法包括：从飞行器车外部去除一个面板; 将减振毯附接到所述移除的面板的后表面; 并且将具有附接的减振毯的面板安装在飞行器上，其中面板的外表面形成飞行器外部的一部分。在一个实施例中，减振毯包括非织造结构中的聚合物（例如，芳族聚酰胺）纤维。

4. 发明授权

US08400171B2 Transmission line moisture sensor 有权
标题翻译：传输线湿度传感器
公开(公告)号：US08400171B2
公开(公告)日：2013-03-19
申请号：US12750496
申请日：2010-03-30
申请人： Gerardo Pena , Justin D. Kearns , Jason P. Bommer , Matthew K. Fay
发明人： Gerardo Pena , Justin D. Kearns , Jason P. Bommer , Matthew K. Fay
IPC分类号： G01R27/08
CPC分类号： G01N17/04 , G01N27/20 , G01N27/24
摘要： A sensor device for monitoring and testing for potential corrosion of structural elements is disclosed comprising a soluble material disposed adjacent to at least one conductor in a transmission line that reacts to the presence of moisture causing a detectable change in an electrical property of the conductor. The conductor may comprise a conductive ink that is disrupted when the soluble material dissolves beneath it. Alternately, the nonconductive soluble membrane may separate two conductors and moisture causes a disruption in the soluble membrane allowing the two conductors to short. Detected changes in the electrical properties of the one or more conductors can be used to indicate potential corrosion or structural imparement in the structural element. Connection to the sensor device may be through a connector or using a wireless reader which remotely energizes the sensor device comprising one or more RFID chips.
摘要翻译：公开了一种用于监测和测试结构元件的潜在腐蚀的传感器装置，其包括与传输线中的至少一个导体相邻设置的可溶性材料，其与水分的存在反应，导致导体的电性能的可检测变化。导体可以包括当可溶性材料溶解在其下时被破坏的导电油墨。或者，不导电的可溶性膜可以分离两个导体，并且湿气导致可溶性膜的破坏，从而允许两个导体短路。检测到的一个或多个导体的电性能变化可用于表示结构元件中的潜在腐蚀或结构性污染。与传感器设备的连接可以通过连接器或使用远程激励包括一个或多个RFID芯片的传感器设备的无线读取器。

5. 发明申请

US20080319692A1 TRANSDUCER HEALTH DIAGNOSTICS FOR STRUCTURAL HEALTH MONITORING (SHM) SYSTEMS 有权
标题翻译：用于结构健康监测（SHM）系统的传感器健康诊断
公开(公告)号：US20080319692A1
公开(公告)日：2008-12-25
申请号：US11766445
申请日：2007-06-21
申请人： Christopher L. Davis , Justin D. Kearns , V. John Mathews
发明人： Christopher L. Davis , Justin D. Kearns , V. John Mathews
IPC分类号： G01R23/00
CPC分类号： G01N29/09 , B06B1/06 , B06B2201/40 , G01H3/005 , G01N29/348 , G01N29/4418 , G01N29/4454 , G01N2291/0258
摘要： A method for diagnosing the health of a transducer may include transmitting a signal to a transducer to cause the transducer to transmit a stress wave into an object being monitored, wherein the signal has a predetermined frequency range or bandwidth. The method may also include receiving response data for the transducer and transforming the response data to data representative of an impedance curve of impedance versus frequency for the predetermined frequency range. The method may further include extracting selected parameters from the impedance curve to diagnose the health of the transducer.
摘要翻译：用于诊断换能器健康的方法可以包括将信号发送到换能器以使得换能器将应力波传输到被监视的对象中，其中该信号具有预定的频率范围或带宽。该方法还可以包括接收换能器的响应数据，并将响应数据转换成代表预定频率范围的阻抗对频率的阻抗曲线的数据。该方法还可以包括从阻抗曲线提取所选参数以诊断换能器的健康状况。

6. 发明申请

US20120325966A1 Flight Vehicle Fairing Having Vibration-Damping Blankets 有权
标题翻译：具有振动阻尼毯的飞行器整流罩
公开(公告)号：US20120325966A1
公开(公告)日：2012-12-27
申请号：US13169295
申请日：2011-06-27
申请人： Justin Christenson , Herbert L. Hoffman , Juhn-Shyue Lin , Gary R. Chewning , Alan Edgar Landmann , Adrian Viisoreanu , Hugh Poling , Balamurugan R. Annamalai , Justin D. Kearns , Jason Alexander Gordon
发明人： Justin Christenson , Herbert L. Hoffman , Juhn-Shyue Lin , Gary R. Chewning , Alan Edgar Landmann , Adrian Viisoreanu , Hugh Poling , Balamurugan R. Annamalai , Justin D. Kearns , Jason Alexander Gordon
IPC分类号： B64C1/00 , B23P11/00 , B23P6/00
CPC分类号： B64C1/26 , B64C1/40 , Y02T50/46 , Y10T29/49723 , Y10T29/49826
摘要： Vibration-damping blankets are attached to the back surfaces of fairing panels of a flight vehicle (e.g., an aircraft or spacecraft) to reduce vibration, fatigue, structure and airborne transmitted energy, and cabin noise. In one case, the flight vehicle fairing has an exterior comprising exterior surfaces of a multiplicity of removable panels. A method of retrofitting the flight vehicle with vibration-damping blankets comprises: removing a panel from the flight vehicle exterior; attaching a vibration-damping blanket to a back surface of the removed panel; and installing the panel with attached vibration-damping blanket on the flight vehicle with the exterior surface of the panel forming part of the flight vehicle exterior. In one embodiment, the vibration-damping blanket comprises polymeric (e.g., aromatic polyamide) fibers in a nonwoven structure.
摘要翻译：减振毯连接到飞行器（例如飞行器或航天器）的整流罩的背面，以减少振动，疲劳，结构和空中传播的能量以及舱室噪音。在一种情况下，飞行器整流罩具有包括多个可移除面板的外表面的外部。用减振毯改装飞行器的方法包括：从飞行器车外部去除一个面板; 将减振毯附接到所述移除的面板的后表面; 并且将具有附接的减振毯的面板安装在飞行器上，其中面板的外表面形成飞行器外部的一部分。在一个实施例中，减振毯包括非织造结构中的聚合物（例如，芳族聚酰胺）纤维。

7. 发明授权

US08237548B2 Structural health management device and associated system and method 有权
标题翻译：结构健康管理装置及相关系统及方法
公开(公告)号：US08237548B2
公开(公告)日：2012-08-07
申请号：US12791300
申请日：2010-06-01
申请人： Matthew K. Fay , Justin D. Kearns , Gerardo Pena , Jason P. Bommer
发明人： Matthew K. Fay , Justin D. Kearns , Gerardo Pena , Jason P. Bommer
IPC分类号： H04Q5/22
CPC分类号： G01M5/0033
摘要： A structural health management device, system and method are provided for facilitating the inspection of a structure, such as in accordance with a condition-based maintenance strategy. A structural health management device may include a radio frequency identification (RFID) tag and at least one sense line communicably coupled to the RFID tag and configured to extend at least partially along a workpiece. The sense line may be formed of different materials depending upon the objective of the inspection. The RFID tag may include processing circuitry and an antenna configured to facilitate offboard communication. The processing circuitry may be configured to interrogate the at least one sense line to determine a change in continuity which is indicative of a change in the structural health of the workpiece. The structural health management device may therefore detect the onset of structural issues in a timely manner.
摘要翻译：提供了结构健康管理装置，系统和方法，用于便于对结构的检查，例如根据基于条件的维护策略。结构健康管理设备可以包括射频识别（RFID）标签和可通信地耦合到RFID标签并被配置为至少部分地沿着工件延伸的至少一个感测线。感测线可以由不同的材料形成，这取决于检查的目的。 RFID标签可以包括处理电路和配置成便于越野通信的天线。处理电路可以被配置成询问至少一条感测线以确定连续性的变化，其指示工件的结构健康状况的改变。因此，结构健康管理装置可及时发现结构性问题的发生。

8. 发明授权

US07302866B1 Device, system, and method for structural health monitoring 有权
标题翻译：用于结构健康监测的装置，系统和方法
公开(公告)号：US07302866B1
公开(公告)日：2007-12-04
申请号：US11621594
申请日：2007-01-10
申请人： Matthew C. Malkin , Justin D. Kearns
发明人： Matthew C. Malkin , Justin D. Kearns
IPC分类号： G01D7/00
CPC分类号： B06B1/0622 , B06B1/0696
摘要： A phased array sensor assembly is presented that can be permanently adhered to and impart ultrasonic waves to a structural surface and receive ultrasonic waves from a structural surface. The sensor assembly includes piezo-electric disks, a plurality of electrically conductive epoxy film adhesive contacts positioned such that an electrical coupling is formed with the piezo-electric disks, piezo transducer flex wire trace circuits aligned to be electrically coupled respectively with the electrically conductive epoxy film adhesive contacts on one end and including a plurality of wire trace electrical contact pads on the other end, and a flexible polyimide layer. The polyimide layer includes laser ablated areas for exposing the contact pads such that they can be electrically coupled with an external device.
摘要翻译：提出了一种相控阵传感器组件，其可以永久地粘附到超声波并向结构表面施加超声波并从结构表面接收超声波。传感器组件包括压电盘，多个导电环氧膜粘合触点，其定位成使得电耦合由压电盘形成，压电换能器柔性线迹线电路对准以分别与导电环氧树脂膜粘合剂在一端接触并且在另一端包括多个线迹电接触焊盘，以及柔性聚酰亚胺层。聚酰亚胺层包括用于暴露接触焊盘的激光烧蚀区域，使得它们可以与外部设备电耦合。

9. 发明申请

US20140361120A9 Flight Vehicle Fairing Having Vibration-Damping Blankets 有权
标题翻译：具有振动阻尼毯的飞行器整流罩
公开(公告)号：US20140361120A9
公开(公告)日：2014-12-11
申请号：US13169295
申请日：2011-06-27
申请人： Justin Christenson , Herbert L. Hoffman , Juhn-Shyue Lin , Gary R. Chewning , Alan Edgar Landmann , Adrian Viisoreanu , Hugh Poling , Balamurugan R. Annamalai , Justin D. Kearns , Jason Alexander Gordon
发明人： Justin Christenson , Herbert L. Hoffman , Juhn-Shyue Lin , Gary R. Chewning , Alan Edgar Landmann , Adrian Viisoreanu , Hugh Poling , Balamurugan R. Annamalai , Justin D. Kearns , Jason Alexander Gordon
IPC分类号： B64C1/00 , B23P11/00 , B23P6/00
CPC分类号： B64C1/26 , B64C1/40 , Y02T50/46 , Y10T29/49723 , Y10T29/49826
摘要： Vibration-damping blankets are attached to the back surfaces of fairing panels of a flight vehicle (e.g., an aircraft or spacecraft) to reduce vibration, fatigue, structure and airborne transmitted energy, and cabin noise. In one case, the flight vehicle fairing has an exterior comprising exterior surfaces of a multiplicity of removable panels. A method of retrofitting the flight vehicle with vibration-damping blankets comprises: removing a panel from the flight vehicle exterior; attaching a vibration-damping blanket to a back surface of the removed panel; and installing the panel with attached vibration-damping blanket on the flight vehicle with the exterior surface of the panel forming part of the flight vehicle exterior. In one embodiment, the vibration-damping blanket comprises polymeric (e.g., aromatic polyamide) fibers in a nonwoven structure.
摘要翻译：减振毯连接到飞行器（例如飞行器或航天器）的整流罩的背面，以减少振动，疲劳，结构和空中传播的能量以及舱室噪音。在一种情况下，飞行器整流罩具有包括多个可移除面板的外表面的外部。用减振毯改装飞行器的方法包括：从飞行器车外部去除一个面板; 将减振毯附接到所述移除的面板的后表面; 并且将具有附接的减振毯的面板安装在飞行器上，其中面板的外表面形成飞行器外部的一部分。在一个实施例中，减振毯包括非织造结构中的聚合物（例如，芳族聚酰胺）纤维。

10. 发明申请

US20130238532A1 Method and Apparatus for Identifying Structural Deformation 有权
标题翻译：识别结构变形的方法和装置
公开(公告)号：US20130238532A1
公开(公告)日：2013-09-12
申请号：US13418081
申请日：2012-03-12
申请人： Justin D. Kearns , Manny Salazar Urcia, JR. , Christopher Lee Davis , Clarence L. Gordon, III
发明人： Justin D. Kearns , Manny Salazar Urcia, JR. , Christopher Lee Davis , Clarence L. Gordon, III
IPC分类号： G06F15/18
CPC分类号： G06N5/047 , G01B21/32 , G01M5/005 , G01M5/0091 , G06N99/005 , H01Q3/267 , H01Q3/34
摘要： A method and apparatus for identifying deformation of a structure. Training deformation data is identified for each training case in a plurality of training cases. Training strain data is identified for each training case in the plurality of training cases. The training deformation data and the training strain data are configured for use by a heuristic model to increase an accuracy of output data generated by the heuristic model. A group of parameters for the heuristic model is adjusted using the training deformation data and the training strain data for the each training case in the plurality of training cases such that the heuristic model is trained to generate estimated deformation data for the structure based on input strain data. The estimated deformation data has a desired level of accuracy.
摘要翻译：一种用于识别结构变形的方法和装置。在多个训练情况下针对每个训练情况识别训练变形数据。针对多个训练情况下的每个训练情况确定训练应变数据。训练变形数据和训练应变数据被配置为由启发式模型使用以增加由启发式模型生成的输出数据的精度。使用训练变形数据和多个训练情况下的每个训练情况的训练应变数据来调整启发式模型的一组参数，使得启发式模型被训练以基于输入应变生成用于结构的估计变形数据数据。估计的变形数据具有期望的精度水平。

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