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51.发明授权公开(公告)号：US09446575B1
公开(公告)日：2016-09-20
申请号：US13791207
申请日：2013-03-08
Applicant: The Boeing Company
Inventor： Gary Ernest Georgeson , Richard H. Bossi
CPC classification number: B32B41/00 , B23P6/00 , B29C73/10 , B29C2035/0827 , B32B33/00 , B32B43/00 , B32B2307/422 , B32B2556/00 , B32B2605/18 , B64F5/40 , G01B11/16 , G01B15/06 , G01K13/00 , G01L1/24 , G01L5/00 , G01M5/0091 , Y10T428/28
Abstract: A composite structure is processed using heat and pressure. A chromatic film is placed in proximity to the composite structure and is used to monitor at least one of the temperature of the heat and the pressure during processing.
Abstract translation: 使用热和压力处理复合结构。 彩色薄膜放置在复合结构附近，用于在加工过程中监测热和压力的至少一个温度。
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52.发明授权公开(公告)号：US09297649B2
公开(公告)日：2016-03-29
申请号：US14001433
申请日：2011-12-12
Applicant: Hiroki Kawada , Norio Hasegawa , Toru Ikegami
Inventor： Hiroki Kawada , Norio Hasegawa , Toru Ikegami
IPC: G01B15/06 , G01N23/225 , H01J37/28 , H01J37/22 , G01N23/00 , H01J37/244
CPC classification number: G01B15/06 , G01N23/00 , H01J37/222 , H01J37/244 , H01J37/28 , H01J2237/24578 , H01J2237/2816 , H01J2237/2817
Abstract: The present invention aims to provide a pattern dimension measurement method for accurately measuring an amount of shrinkage of a pattern that shrinks and an original dimension value before the shrinkage and a charged particle beam apparatus.In order to attain the above-mentioned object, there are proposed a pattern dimension measurement method and a charged particle beam apparatus that are characterized by: forming a thin film on a sample including the pattern after carrying out beam scanning onto a first portion of the pattern; acquiring a first measurement value by scanning a beam onto a region corresponding to the first portion on which the thin film is formed; acquiring a second measurement value by scanning a beam onto a second portion that has identical dimensions as those of the first portion on design data; and finding the amount of shrinkage of the pattern based on subtraction processing of subtracting the first measurement value from the second measurement value.
Abstract translation: 本发明的目的在于提供一种图形尺寸测量方法，用于精确测量收缩的图案的收缩量和收缩前的原始尺寸值以及带电粒子束装置。 为了实现上述目的，提出了一种图案尺寸测量方法和带电粒子束装置，其特征在于：在对包含图案的样品进行束扫描之后，在包含该图案的样品上形成薄膜至第一部分 模式; 通过将光束扫描到与其上形成有薄膜的第一部分对应的区域来获取第一测量值; 通过将光束扫描到与设计数据上的第一部分具有相同尺寸的第二部分上来获取第二测量值; 并且基于从第二测量值减去第一测量值的减法处理来找出图案的收缩量。
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53.发明申请STRUCTURAL REPAIR HAVING OPTICAL WITNESS AND METHOD OF MONITORING REPAIR PERFORMANCE 审中-公开具有光学性能的结构修复和监测维修性能的方法公开(公告)号：US20150338296A1
公开(公告)日：2015-11-26
申请号：US14722149
申请日：2015-05-27
Applicant: The Boeing Company
Inventor： Gary E. Georgeson , Kenneth Harlan Griess , Russell Lee Keller , Everett A. Westerman
CPC classification number: B32B41/00 , B23P6/00 , B29C73/10 , B29C2035/0827 , B32B33/00 , B32B43/00 , B32B2307/422 , B32B2556/00 , B32B2605/18 , B64F5/40 , G01B11/16 , G01B15/06 , G01K13/00 , G01L1/24 , G01L5/00 , G01M5/0091 , Y10T428/28
Abstract: A structural repair includes a tell-tale optical witness that allows the health of the repair to be visually monitored. The optical witness includes a stress sensitive fluorescent dye that shows changes in local strain/stress patterns when the repair is subjected to electromagnetic energy of a particular wavelength. The dyes fluoresce more or less strongly as a function of the local stress/strain.
Abstract translation: 结构修复包括一个能够视觉监控修复的健康状况的指示性光学证人。 光学目击者包括应力敏感荧光染料，其在修复受特定波长的电磁能量时显示局部应变/应力模式的变化。 染料作为局部应力/应变的函数或多或少地发挥强烈的荧光。
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54.发明授权Structural repair having optical witness and method of monitoring repair performance 有权具有光学见证的结构修复和监测维修性能的方法公开(公告)号：US09085052B1
公开(公告)日：2015-07-21
申请号：US13310539
申请日：2011-12-02
Applicant: Gary E. Georgeson , Kenneth Harlan Griess , Russell Lee Keller , Everett A. Westerman, Jr.
Inventor： Gary E. Georgeson , Kenneth Harlan Griess , Russell Lee Keller , Everett A. Westerman, Jr.
CPC classification number: B32B41/00 , B23P6/00 , B29C73/10 , B29C2035/0827 , B32B33/00 , B32B43/00 , B32B2307/422 , B32B2556/00 , B32B2605/18 , B64F5/40 , G01B11/16 , G01B15/06 , G01K13/00 , G01L1/24 , G01L5/00 , G01M5/0091 , Y10T428/28
Abstract: A structural repair includes a tell-tale optical witness that allows the health of the repair to be visually monitored. The optical witness includes a stress sensitive fluorescent dye that shows changes in local strain/stress patterns when the repair is subjected to electromagnetic energy of a particular wavelength. The dyes fluoresce more or less strongly as a function of the local stress/strain.
Abstract translation: 结构修复包括一个能够视觉监控修复的健康状况的指示性光学证人。 光学目击者包括应力敏感荧光染料，其在修复受特定波长的电磁能量时显示局部应变/应力模式的变化。 染料作为局部应力/应变的函数或多或少地发挥强烈的荧光。
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55.发明授权Passive wireless antenna sensor for strain, temperature, crack and fatigue measurement 有权被动无线天线传感器用于应变，温度，裂纹和疲劳测量公开(公告)号：US08868355B2
公开(公告)日：2014-10-21
申请号：US12867801
申请日：2009-02-15
Applicant: Haiying Huang , Jung-Chih Chiao , Ronald L. Carter , Uday Shankar Tata
Inventor： Haiying Huang , Jung-Chih Chiao , Ronald L. Carter , Uday Shankar Tata
CPC classification number: G01B7/16 , G01B15/06 , H01Q1/2225 , H01Q21/065
Abstract: An apparatus and method is provided for monitoring a condition of a structure using a passive wireless antenna sensor having a known resonant frequency when mounted on the structure. A series of radio frequency signals are transmitted with sweeping frequencies around the known resonant frequency to the passive wireless antenna sensor. The passive wireless antenna sensor includes a dielectric substrate disposed between an antenna pattern and a ground plane such that a change in the condition of the structure will cause a change in one or more characteristics of the passive wireless sensor. A signal is received from the passive wireless antenna sensor and a resonant frequency of the passive wireless antenna sensor is determined based on the received signal. The determined resonant frequency is then compared to the known resonant frequency, whereby a change in the resonant frequency indicates a change in the condition of the structure.
Abstract translation: 提供了一种装置和方法，用于当安装在结构上时，使用具有已知共振频率的无源无线天线传感器监测结构的状况。 将一系列射频信号以围绕已知谐振频率的扫频以无源无线天线传感器传输。 无源无线天线传感器包括设置在天线图案和接地平面之间的电介质基板，使得结构状况的变化将导致无源无线传感器的一个或多个特性的改变。 从无源无线天线传感器接收信号，并且基于接收到的信号确定无源无线天线传感器的谐振频率。 然后将确定的谐振频率与已知的谐振频率进行比较，由此谐振频率的变化表示结构状况的变化。
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Patent Agency Ranking
公开(公告)号：US20140266861A1
公开(公告)日：2014-09-18
申请号：US14181689
申请日：2014-02-16
Applicant: Per Egedal , Jesper Winther Staerdahl , Andreas Ziroff
Inventor： Per Egedal , Jesper Winther Staerdahl , Andreas Ziroff
CPC classification number: F03D7/06 , F03D17/00 , F05B2270/17 , G01B15/06 , G01S13/08 , Y02E10/722
Abstract: An arrangement to measure deflection of a blade of a wind turbine is provided. A transmitter is arranged close to the tip end of the blade, while a receiver is arranged close to the root end of the blade. The transmitter and receiver are prepared for a wireless transfer of a monitoring signal, which is sent from the transmitter to the receiver. A monitoring system is arranged close to the root end of the blade. The monitoring system is adapted to generate the monitoring signal. The monitoring system is connected with the transmitter by a cable-bound communication line, thus the monitoring signal is transferred from the monitoring system to the transmitter. The monitoring system is connected with the receiver, thus the monitoring signal is transferred from the receiver to the monitoring system. The monitoring system is adapted to determine the deflection of the blade based on the transferred monitoring signal.
Abstract translation: 提供了一种用于测量风力涡轮机的叶片的偏转的装置。 发射器布置成靠近叶片的尖端，而接收器布置成靠近叶片的根端。 准备发射机和接收机用于从发射机发送到接收机的监视信号的无线传输。 监视系统靠近叶片的根端设置。 监控系统适于产生监控信号。 监控系统通过电缆绑定通信线路与发射机连接，监控信号从监控系统传输到发射机。 监控系统与接收器连接，监控信号从接收器传输到监控系统。 监测系统适于基于所传送的监视信号来确定叶片的偏转。
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57.发明申请公开(公告)号：US20140048706A1
公开(公告)日：2014-02-20
申请号：US14001433
申请日：2011-12-12
Applicant: Hiroki Kawada , Norio Hasegawa , Toru Ikegami
Inventor： Hiroki Kawada , Norio Hasegawa , Toru Ikegami
IPC: G01N23/00
CPC classification number: G01B15/06 , G01N23/00 , H01J37/222 , H01J37/244 , H01J37/28 , H01J2237/24578 , H01J2237/2816 , H01J2237/2817
Abstract: The present invention aims to provide a pattern dimension measurement method for accurately measuring an amount of shrinkage of a pattern that shrinks and an original dimension value before the shrinkage and a charged particle beam apparatus.In order to attain the above-mentioned object, there are proposed a pattern dimension measurement method and a charged particle beam apparatus that are characterized by: forming a thin film on a sample including the pattern after carrying out beam scanning onto a first portion of the pattern; acquiring a first measurement value by scanning a beam onto a region corresponding to the first portion on which the thin film is formed; acquiring a second measurement value by scanning a beam onto a second portion that has identical dimensions as those of the first portion on design data; and finding the amount of shrinkage of the pattern based on subtraction processing of subtracting the first measurement value from the second measurement value.
Abstract translation: 本发明的目的在于提供一种图形尺寸测量方法，用于精确测量收缩的图案的收缩量和收缩前的原始尺寸值以及带电粒子束装置。 为了实现上述目的，提出了一种图案尺寸测量方法和带电粒子束装置，其特征在于：在对包含图案的样品进行束扫描之后，在包含该图案的样品上形成薄膜至第一部分 模式; 通过将光束扫描到与其上形成有薄膜的第一部分对应的区域来获取第一测量值; 通过将光束扫描到与设计数据上的第一部分具有相同尺寸的第二部分上来获取第二测量值; 并且基于从第二测量值减去第一测量值的减法处理来找出图案的收缩量。
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58.发明申请Passive Wireless Antenna Sensor for Strain, Temperature, Crack and Fatigue Measurement 有权用于应变，温度，裂纹和疲劳测量的无源无线天线传感器公开(公告)号：US20110040498A1
公开(公告)日：2011-02-17
申请号：US12867801
申请日：2009-02-15
Applicant: Haiying Huang , Jung-Chih Chiao , Ronald L. Carter , Uday Shankar Tata
Inventor： Haiying Huang , Jung-Chih Chiao , Ronald L. Carter , Uday Shankar Tata
IPC: G01B7/16
CPC classification number: G01B7/16 , G01B15/06 , H01Q1/2225 , H01Q21/065
Abstract: An apparatus and method is provided for monitoring a condition of a structure using a passive wireless antenna sensor having a known resonant frequency when mounted on the structure. A series of radio frequency signals are transmitted with sweeping frequencies around the known resonant frequency to the passive wireless antenna sensor. The passive wireless antenna sensor includes a dielectric substrate disposed between an antenna pattern and a ground plane such that a change in the condition of the structure will cause a change in one or more characteristics of the passive wireless sensor. A signal is received from the passive wireless antenna sensor and a resonant frequency of the passive wireless antenna sensor is determined based on the received signal. The determined resonant frequency is then compared to the known resonant frequency, whereby a change in the resonant frequency indicates a change in the condition of the structure.
Abstract translation: 提供了一种装置和方法，用于当安装在结构上时，使用具有已知共振频率的无源无线天线传感器监测结构的状况。 将一系列射频信号以围绕已知谐振频率的扫频以无源无线天线传感器传输。 无源无线天线传感器包括设置在天线图案和接地平面之间的电介质基板，使得结构状态的变化将导致无源无线传感器的一个或多个特性的改变。 从无源无线天线传感器接收信号，并且基于接收到的信号确定无源无线天线传感器的谐振频率。 然后将确定的谐振频率与已知的谐振频率进行比较，由此谐振频率的变化表示结构状况的变化。
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公开(公告)号：US20090189784A1
公开(公告)日：2009-07-30
申请号：US12022320
申请日：2008-01-30
Applicant: Lawrence S. Lindgren
Inventor： Lawrence S. Lindgren
CPC classification number: G01B15/06 , G01M5/0033 , G01M5/0083 , G01M5/0091
Abstract: a plurality of RFIDs is installed on aircraft or other structure. The RFIDs can query one another upon original installation and in response to predetermined event detection, and determine their relative locations within a mesh. The determined location data and other information are stored within the respect memories of the RFIDs. The stored data can be later accessed and used in analyzing damage or structural failure of the aircraft. Corrective measures are thus expedited because before-and-after structural comparisons can be readily made, with or without reference to original engineering data for the aircraft.
Abstract translation: 多个RFID安装在飞机或其他结构上。 RFID可以在原始安装和响应于预定的事件检测时相互查询，并且确定它们在网格内的相对位置。 确定的位置数据和其他信息被存储在RFID的尊重存储器内。 存储的数据可以稍后被访问并用于分析飞机的损坏或结构故障。 因此，加快了纠正措施，因为可以轻松地进行前后结构比较，有或没有参考飞机的原始工程数据。
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60.发明申请Systems and methods for monitoring thermal growth and controlling clearances, and maintaining health of turbo machinery applications 有权用于监测热增长和控制间隙的系统和方法，并保持涡轮机械应用的健康公开(公告)号：US20070043497A1
公开(公告)日：2007-02-22
申请号：US11204490
申请日：2005-08-16
Applicant: John Leogrande , Peter Jalbert , C. Wood , Matthew Schryver
Inventor： John Leogrande , Peter Jalbert , C. Wood , Matthew Schryver
IPC: G06F19/00
CPC classification number: F01D11/24 , F01D21/003 , F01D21/04 , F05D2220/36 , F05D2270/304 , F05D2270/305 , G01B15/06
Abstract: A system and method for determining thermal growth of motor or engine parts to thereupon control the clearance of motor or engine fan blades is disclosed herein. In addition, a system and method for monitoring the health of a turbine engine, its components and sub-components is also described herein. The system(s) and method(s) described herein permit continuous monitoring during the life of the engine for radial clearances and blade and rotor vibration problems, which will assist in correcting and retaining performance for a longer on-wing time in operation. In addition, inconsistent engine-to-engine performance variations due to component tolerances, engine operation characteristics, and operation during extremes in ambient temperatures can be eliminated or significantly minimized when employing the system(s) and method(s) described herein.
Abstract translation: 本文公开了一种用于确定马达或发动机部件的热增长的系统和方法，从而控制马达或发动机风扇叶片的间隙。 此外，还描述了用于监测涡轮发动机，其部件和子部件的健康状态的系统和方法。 本文所述的系统和方法允许在发动机寿命期间对于径向间隙和叶片和转子振动问题进行连续监测，这将有助于校正和保持操作中更长的机翼时间的性能。 此外，当使用本文所述的系统和方法时，可以消除或显着地最小化由于部件公差，发动机操作特性和在环境温度极限期间的操作引起的发动机与发动机性能的不一致。
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