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公开(公告)号：KR101549504B1
公开(公告)日：2015-09-03
申请号：KR1020140027652
申请日：2014-03-10
Applicant: 전북대학교산학협력단 , 한국항공우주연구원
CPC classification number: G01M7/08 , G01N21/17 , G01N29/2418
Abstract: 본 발명은 선형 화약 기반 파이로 장치에서 발생하는 충격파를 가시화하고 구조의 손상 여부를 파악하기 위한 선형 화약 유도 충격파 가시화 장치 및 방법에 관한 것으로, 본 발명의 선형 화약 유도 충격파 가시화 장치는 시편을 포함하며, 실제 선형 화약 유도 충격파를 측정하는 선형 화약 유도 충격파 측정부, 시편을 포함하며, 레이저 유도 충격파를 측정하는 레이저 유도 충격파 측정부, 레이저 유도 충격파가 실제 선형 화약 유도 충격파와 유사해지도록 트레이닝하며, 재구성되는 재구성부; 재구성된 레이저 유도 충격파를 스캐닝 과정을 통해 실험적 선형 화약 유도 충격파의 전파 영상으로 생성하는 영상 생성부; 다수의 센서로부터 획득된 신호의 위상배열 신호처리를 통해 특정 방향으로 신호대잡음비가 향상된 실험적 선형 화약 유도 충격파의 전파 영상을 사용해 구조 손상을 가시화하는 구조 손상 가시화부를 포함한다.
Abstract translation: 本发明涉及一种用于线性火药诱发的焦灼可视化的装置和方法，用于显现在基于线性火药的火焰装置中产生的剧烈震荡，并检查对结构的损害。 本发明的线性火药诱发的剧烈震荡显示装置包括线性火药诱发的包含样本的火山岩测量部分，并测量实际线性火药诱发的火山爆发; 包括样品的激光诱发的Pyroshock测量部件和测量激光诱发的pyroshock; 重新配置部分训练和重新配置激光诱发的Pyroshock，类似于实际线性火药诱发的pyroshock; 图像生成部，其通过扫描处理产生作为实验线性火药诱发的Pyroshock的无线电波图像的重新配置的激光诱发的Pyroshock; 以及通过使用通过从多个传感器获得的信号的相位阵列信号处理在特定方向上改善了信噪比的实验线性火药诱发的Pyroshock的无线电波图像来对结构造成损害的结构损伤可视化部分来显现对结构的损害。
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公开(公告)号：KR101280921B1
公开(公告)日：2013-07-02
申请号：KR1020120057692
申请日：2012-05-30
Applicant: 전북대학교산학협력단 , 한국항공우주연구원
CPC classification number: G01N29/2418 , G01M7/08 , G01N29/04 , G01N29/11 , G01N29/2437 , G01N29/4472
Abstract: PURPOSE: A guide wave simulation method using laser guide waves and a guide wave simulation device applied the same are provided to conveniently simulate physical guide waves by using the laser guide waves without performing a physical experiment requires various samples or inducing damages of the samples. CONSTITUTION: A guide wave simulation method is as follows. Physical guide waves generated at a specific portion of a sample are detected at various spots (S510). Laser guide waves corresponding to the various spots are detected (S520). The laser guide waves simulated by using the physical guide waves and the laser guide waves are calculated (S530). If the similarity of the simulated guide waves and the physical guide waves are more than a critical value, transformation models obtained in the calculation step are stored (S540-S550). The laser guide waves per each spot with respect to a specific portion of the sample are detected (S560). The simulated laser guide waves having the similarity with the physical guide waves are calculated by using the stored transformation models (S570). [Reference numerals] (AA) Start; (BB) Finish; (S510) Detect physical guide waves generated at a specific portion of a sample at various spots; (S520) Detect laser guide waves corresponding to the various spots; (S530) Calculate laser guide waves simulated by using the physical guide waves and the laser guide waves; (S540) Similarity > Critical value?; (S545) Increase a band division number (K); (S550) Record a conversion factor utilized in the prior calculation step; (S560) Detect the laser guide waves per each spot with respect to a specific portion of the sample at a predetermined interval; (S570) Calculate a model in respect to the physical guide waves; (S580) Generate an image in respect to the physical guide waves using the model
Abstract translation: 目的：提供使用激光导波的导波模拟方法及其应用的导波模拟装置，以便在不进行物理实验的情况下使用激光导波方便地模拟物理导波，需要各种样品或诱导样品损坏。 构成：引导波仿真方法如下。 在各个点处检测在样品的特定部分产生的物理引导波（S510）。 检测对应于各个点的激光导波（S520）。 计算通过使用物理引导波和激光导波而模拟的激光导波（S530）。 如果模拟引导波和物理引导波的相似度大于临界值，则存储在计算步骤中获得的变换模型（S540-S550）。 检测相对于样品的特定部分的每个点的激光引导波（S560）。 通过使用所存储的变换模型来计算与物理引导波相似的模拟激光导波（S570）。 （附图标记）（AA）开始; （BB）完成; （S510）检测在各个点处在样品的特定部分产生的物理引导波; （S520）检测对应于各个点的激光导波; （S530）计算通过使用物理引导波和激光引导波模拟的激光导波; （S540）相似度>临界值 （S545）增加频带划分数（K）; （S550）记录先前计算步骤中使用的转换因子; （S560）以预定的间隔相对于样品的特定部分检测每个点的激光导波; （S570）计算相对于物理引导波的模型; （S580）使用模型生成关于物理引导波的图像
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公开(公告)号：KR1020140084990A
公开(公告)日：2014-07-07
申请号：KR1020120155057
申请日：2012-12-27
Applicant: 한국항공우주연구원
CPC classification number: G01N3/08 , B25B11/02 , G01N3/02 , G01N2203/0017 , G01N2203/04
Abstract: The present invention relates to a jig for a tensile test of a composite laminated structure, whereby is used to conduct a tensile test of a composite laminated structure (1) including a honeycomb core (10) and composites (30) attached to the top and bottom of the honeycomb core (10) respectively using an adhesive (20). The jig for a tensile test of a composite laminated structure comprises: a first tensile fixture (100) combined with a composite (30) attached to the top of a honeycomb core (10); and a second tensile fixture (200) combined with a composite (30) attached to the bottom of the honeycomb core (10). The first and second tensile fixtures (100, 200) are made of the same material as the composite (30). In addition, a tensile test of the composite laminated structure (1) can be conducted by extending the first and second tensile fixtures (100, 200) in a vertical direction.
Abstract translation: 本发明涉及一种用于复合叠层结构的拉伸试验的夹具，由此用于进行包括蜂窝芯（10）和复合材料（30）的复合层压结构（1）的拉伸试验，所述复合层压结构（1）附接到顶部和 蜂窝芯（10）的底部分别使用粘合剂（20）。 用于复合层压结构的拉伸试验的夹具包括：与附接到蜂窝芯（10）的顶部的复合材料（30）组合的第一拉伸夹具（100）。 以及与附接到蜂窝芯（10）的底部的复合材料（30）组合的第二拉伸夹具（200）。 第一和第二拉伸夹具（100,200）由与复合材料（30）相同的材料制成。 此外，复合层压结构（1）的拉伸试验可以通过沿垂直方向延伸第一和第二拉伸固定装置（100,200）来进行。
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公开(公告)号：KR101376499B1
公开(公告)日：2014-03-25
申请号：KR1020120146076
申请日：2012-12-14
Applicant: 한국항공우주연구원
CPC classification number: B32B3/12 , B32B2250/40 , B32B2305/024 , B32B2305/34 , B32B2307/202 , B32B2605/18
Abstract: The present invention relates to a laminated composite structure having an electric bonding insert, including: a honeycomb core (100) An insertion hole (110) perforated in a heightwise direction; an electric boding insert (200) which is inserted to the insertion hole (110), and which can adjusted of the length in the heightwise direction of the honeycomb core (110); and a composite (300) which is adhered to one and the other sides of the heightwise direction of the honeycomb core (100). All of the above components are made of conductive material.
Abstract translation: 本发明涉及具有电接合插入物的层压复合结构体，其包括：蜂窝芯（100），在高度方向上穿孔的插入孔（110） 电插入插入件（200），其插入到插入孔（110）中，并且可以调节蜂窝芯（110）的高度方向上的长度; 以及粘合到蜂窝芯（100）的高度方向的一侧和另一侧的复合体（300）。 所有上述组件均由导电材料制成。
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公开(公告)号：KR101205773B1
公开(公告)日：2012-12-03
申请号：KR1020100123681
申请日：2010-12-06
Applicant: 전북대학교산학협력단 , 한국항공우주연구원
Abstract: 본발명은변형률및 손상동시능동센싱섬유파압전트랜스듀서를개시한다. 본발명은구조에일정한거리를두고설치되는송수신용압전소자와, 상기송수신용압전소자를연결하는섬유와, 상기송신용압전소자에설계된전압신호를인가하여초음파를발생시키는초음파송신부와, 상기수신용압전소자에서검출된전압신호의변화의형태인초음파신호를수신하는초음파수신부와, 수신된초음파신호에서변형률정보를처리하는변형률모니터링부와, 수신된초음파신호에서손상정보를처리하는손상모니터링부를포함한다.
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Patent Agency Ranking
公开(公告)号：KR1020120062423A
公开(公告)日：2012-06-14
申请号：KR1020100123681
申请日：2010-12-06
Applicant: 전북대학교산학협력단 , 한국항공우주연구원
Abstract: PURPOSE: A fiber waves piezoelectric transducer for simultaneously active-sensing a strain and damage is provided to obtain a sufficient signal-to-noise ratio even though fiber waves are transmitted tens of meters because the index of dispersion is low in the silica fiber or the metal fiber and to manufacture a sensor which signal-to-noise ratio is dramatically long. CONSTITUTION: A fiber waves piezoelectric transducer(100) for simultaneously active-sensing a strain and damage comprises a sender-receiver piezoelectric device(110), a fiber(120), an ultrasonic wave transmitter(132), a strain monitoring part(150), and a damage information monitoring part(140). The fiber connects the sender-receiver piezoelectric device. The ultrasonic wave transmitter transmits voltage signals to the sender-receiver piezoelectric device, thereby generating ultrasonic waves. The ultrasonic wave receiver receives ultrasonic signals which are a changed form of the voltage signals detected from the piezoelectric device. The strain monitoring part processes strain information from the received ultrasonic signals. The damage information monitoring part processes damage information from the received ultrasonic signals.
Abstract translation: 目的：提供一种用于同时主动感测应变和损伤的光纤波形压电传感器，以获得足够的信噪比，即使光纤传输数十米，因为二氧化硅光纤中的色散指数低 金属纤维，并制造信噪比显着长的传感器。 构成：用于同时主动感测应变和损坏的光纤波长压电传感器（100）包括发送器 - 接收器压电装置（110），光纤（120），超声波发射器（132），应变监测部分（150） ）和损伤信息监视部（140）。 光纤连接发送器 - 接收器压电器件。 超声波发射器将电压信号发送到发送器 - 接收器压电器件，从而产生超声波。 超声波接收器接收作为从压电装置检测出的电压信号的变化形式的超声波信号。 应变监测部分从接收到的超声波信号中处理应变信息。 损伤信息监控部分从接收到的超声波信号中处理损伤信息。
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公开(公告)号：KR1020120055062A
公开(公告)日：2012-05-31
申请号：KR1020100116560
申请日：2010-11-23
Applicant: 한국항공우주연구원
Abstract: PURPOSE: A prefabricated bolt in which the bending load is reinforced is provided to couple a bolt by reinforcing the bending load because the strength of materials of a connection and reinforcement bar is enhance without increasing a size of the blot in a place under more bending load. CONSTITUTION: A prefabricated bolt(10) in which the bending load is reinforced comprises a bolt head unit(11), a bolt screw unit(12), and a connection and reinforcement bar(13). The bolt head unit comprises a coupling groove in a longitudinal direction. A screw thread is formed in both outer circumferences in a longitudinal direction of the coupling groove. The bolt screw unit comprises a through-hole in a longitudinal direction. A screw thread is formed in both outer circumferences in a longitudinal direction of the through-hole. A screw thread is formed in the outer circumferences in a longitudinal direction of the connection and reinforcement bar.
Abstract translation: 目的：提供弯曲载荷被加固的预制螺栓，用于通过加强弯曲载荷来联接螺栓，因为连接件和钢筋的材料的强度在不增加在更多弯曲载荷下的位置的印迹尺寸的情况下增强 。 构成：其中弯曲载荷被增强的预制螺栓（10）包括螺栓头单元（11），螺栓螺钉单元（12）和连接和加强杆（13）。 螺栓头单元包括在纵向方向上的联接槽。 在连接槽的长度方向的两个外周形成螺纹。 螺栓螺钉单元在纵向方向上包括通孔。 在通孔的长度方向的两个外周形成螺纹。 在连接和加强条的纵向方向上的外周中形成有螺纹。
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公开(公告)号：KR1020030092250A
公开(公告)日：2003-12-06
申请号：KR1020020029862
申请日：2002-05-29
Applicant: 한국항공우주연구원
IPC: F17C13/08
Abstract: PURPOSE: A device for fixing a boss is provided to prevent the damage of threads in a boss fitting screw by transmitting force applied to the boss fitting screw to composite fiber. CONSTITUTION: In a tank made of composite materials, a metallic ring(3) and a coupling bolt(4) are installed between a boss fitting screw(5) and composite fiber(2). The force applied to the boss fitting screw is transmitted to the composite fiber, thereby preventing the damage of threads in the boss fitting screw.
Abstract translation: 目的：提供一种用于固定凸台的装置，以通过将施加到凸台装配螺钉的力传递给复合纤维来防止凸起装配螺钉中的螺纹损坏。 构成：在由复合材料制成的罐中，金属环（3）和联接螺栓（4）安装在凸台配合螺钉（5）和复合纤维（2）之间。 施加到凸台接合螺钉的力传递到复合纤维，从而防止凸台接合螺钉中的螺纹损坏。
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公开(公告)号：KR1020140121609A
公开(公告)日：2014-10-16
申请号：KR1020130038024
申请日：2013-04-08
Applicant: 한국항공우주연구원
Abstract: 기폭에 의해 폭발하는 화약의 가스 및 파편을 외부로 방출시키지 않는 파이로 연결 및 차단장치에 있어서, 화약을 지지하며, 내부에 공간을 가진 차단바디, 화약에 기폭을 전달하는 기폭부, 화약 폭발 시 차단바디와 조립되는 연결바디, 연결 바디에 형성되어 있는 화약 연결홈으로 구성된다. 연결바디 및 차단 바디로 인하여 화약 폭발에 의한 가스 및 파편이 외부로 방출 되지 않아, 주변 부품 및 주변 시스템에 악 영향을 끼치는 문제를 해결하는 효과가 있다.
Abstract translation: 本发明涉及一种不发射气体和火焰碎片的火焰连接和阻塞装置，其通过点燃向外部分解。 火焰连接和阻塞装置包括支撑火药并且在其内部具有空间的阻挡体; 点火单元将点火传递到火药; 当火药爆炸时组装到阻塞体上的连接体; 以及形成在连接体中的火药连接槽。 热连接和阻塞装置包括连接体和阻塞体，以防止由于火药爆炸而引起的气体和碎片被排放到外部。 因此，本发明可以解决对周围部件和周围系统的不良影响的问题。
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