• Title/Summary/Keyword: 구조 시험

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대형 내진시험 구조물에 대한 강제진동시험 결과의 예측 및 예측후상관해석

  • 박형기;조양희;윤철호
    • Proceedings of the Korean Nuclear Society Conference
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    • 1995.05b
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    • pp.1005-1010
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    • 1995
  • 지반-구조물 상호작용해석에 부분구조법의 적용성 확인과 해석법의 개선을 모색하기 위하여, 대만 Hualien지방에 건설한 대형 내진시험 구조물의 뒷채움후 강제진동시험 결과를 부분구조법으로 예측하고 예측후상관해석을 수행하였다. 모델로서는 재료시험과 지반조사 결과로 작성된 통일모델과 예측후상관해석모델을 사용하였으며, 해석은 진동 수영역과 시간영역에서 각각 이루어졌다 연구 결과로 깊이 묻힌 구조물의 경우는 구조물이 묻힌 측면지반의 영향인 수평병진과 수평축회전의 연계 임피던스함수에 대한 적절한 평가와 해석시에 반드시 고려되어야함을 알 수 있었다.

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Development of Full-Scale Static Test System for Aircraft Sensor Pod (항공용 센서 포드의 정적 구조시험장비 개발)

  • Jae Myung Cho;Hoon Hyuk Park;Won Woong Lee;Jong In Bae;Han Sol Lee;Eui Hwan Oh
    • Journal of Aerospace System Engineering
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    • v.17 no.1
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    • pp.97-105
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    • 2023
  • For aviation sensor pod, structural integrity should be verified through static structural tests for flight loads induced in various maneuvering conditions of the aircraft. For this, it is necessary to develop a test system for full-scale static load test of sensor pod. Based on test requirements, this paper introduced a test system configuration of the static test and the development of test structure frame, restraints equipment, loading equipment, control, and measurement equipment. In addition, methods and procedures for verifying the developed test system were explained. In conclusion, the static load test and data acquisition were successfully performed. Reliability of the test equipment was also verified in the process.

The Study on Structural Strength Test Technique for Cylindrical Supersonic Vehicle Subjected to Severe Heating Environment (원통형 초음속 비행체 내열구조시험 기법 연구)

  • Lee, Kyung-Yong;Kim, Jong-Hwan;Lee, Kee-Bhum;Jung, Jae-Kwon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.6
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    • pp.83-91
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    • 2005
  • This paper describes the structural strength test technique and the results for cylindrical supersonic vehicle subjected to both aerodynamic load and thermal load. The special positioning system using spring links was designed to float, support and restrain the test airframe during the test and the down-time. The hydraulic system and the electric heating system were utilized to apply the aerodynamic load and the thermal load to the test airframe together. Particularly, several hundreds of infrared quartz lamps were used for the heating system, and the thermal test conditions were successfully simulated. The test results showed that this kind of high temperature test is adequate to verify the structure integrity and produce useful engineering data which is necessary for the possible structural modification under thermal environments.

구조안전과 구조시험

  • 이성근
    • Journal of the KSME
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    • v.28 no.4
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    • pp.408-414
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    • 1988
  • 근년에 항공 산업이 많은 관심을 불러일으키고 있음에 즈음하여 독자적인 항공기 구조개발시 구조적 안전성 확보를 위해서는 구조시험 기술의 확보가 필수적이다. 또한 구조시험 관련기술은 다른 기계 구조물의 초기 설계단계에서 구조 강도 및 피로 강도의 확인을 위해서도 응력될 수 있어 구조물의 설계 및 제작공정 결정에 큰 도움이 될 수 있으므로 기업체나 연구소에서도 충 분히 응용할 수 있도록 노력을 기울여야 할 분야이다.

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Evaluation of Static Structural Integrity for Composites Wing Structure by Acoustic Emission Technique (음향방출법을 응용한 복합재 날개 구조물의 정적구조 건전성 평가)

  • Jun, Joon-Tak;Lee, Young-Shin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.8
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    • pp.780-788
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    • 2009
  • AE technique was applied to the static structural test of the composite wing structure to evaluate the structural integrity and damage. During the test, strain and displacements measurement technique were used to figure out for static structural strength. AE parameter analysis and source location technique were used to evaluate the internal damage and find out damage source location. Design limit load test, the 1st and 2nd design ultimate load tests and fracture test were performed. Main AE source was detected by an sensor attached on skin near by front lug. Especially, at the 1st design ultimate test, strain and displacements results didn't show internal damage but AE signal presented a phenomenon that the internal damage was formed. At the fracture test, AE activities were very lively, and strain and displacements results showed a tendency that the load path was changed by severe damage. The internal damage initiation load and location were accurately evaluated during the static structural test using AE technique. It is certified from this paper that AE technique is useful technique for evaluation of internal damage at static structural strength test.

스트레인게이지를 이용한 고속화차 대차프레임의 정하중시험 및 진동가속도 측정시험

  • 홍재성;함영삼;백영남
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.05a
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    • pp.114-114
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    • 2004
  • 주)태양금속에서 고속화차 용접구조형 대차를 채택하여 화차론 제작하였는데 한국철도기술연구원에서는 대차의 구조강도론 검증하기 위해 구조해석을 시행한 후 스트레인게이지를 실재 대차에 장착하여 정하중 시험을 시행하였고 또한 진동가속도계를 차체 및 대차프레임에 장착하여 주행안전성과 관련된 진동성능시험을 시행하였다. 본 논문은 새로 개발된 용접구조형 대차 및 이를 장착한 화차에 대해 대차프레임의 강도 검증과 화차의 안정성 여부를 판단하기 위한 시험을 시행한 결과에 대한 내용이다.(중략)

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A Study on the Performance Analysis of an Extended Scan Path Architecture (확장된 스캔 경로 구조의 성능 평가에 관한 연구)

  • 손우정
    • Journal of the Korea Society of Computer and Information
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    • v.3 no.2
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    • pp.105-112
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    • 1998
  • In this paper, we propose a ESP(Extended Scan Path) architecture for multi-board testing. The conventional architectures for board testing are single scan path and multi-scan path. In the single scan path architecture, the scan path for test data is just one chain. If the scan path is faulty due to short or open, the test data is not valid. In the multi-scan path architecture, there are additional signals in multi-board testing. So conventional architectures are not adopted to multi-board testing. In the case of the ESP architecture, even though scan path is either short or open, it doesn't affect remaining other scan paths. As a result of executing parallel BIST and IEEE 1149.1 boundary scan test by using the proposed ESP architecture, we observed that the test time is short compared with the single scan path architecture. By comparing the ESP architecture with single scan path responding to independency of scan path, test time and with multi-scan path responding to signal, synchronization, we showed that the architecture has improved results.

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A Study on Structural Design and Analysis of Small Engine Test Equipment for Use in Aircraft (항공기 소형 엔진 시험 장치의 구조 설계 및 해석 연구)

  • Back, Kyeongmi;Park, Hyunbum
    • Journal of Aerospace System Engineering
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    • v.12 no.1
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    • pp.42-46
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    • 2018
  • The subject of this study dealt with the structural safety analysis regarding the measured thrust test equipment as noted on a small engine. In this work, the structural design and analysis of steel and aluminum alloy structure for a small engine test of equipment were performed. Firstly, the structural design requirements of the engine test equipment were identified and investigated. After the structural design was reviewed, next the structural analysis of the engine test equipment was performed by the utilization of the finite element analysis method. The study was performed to determine that the stress and displacement analysis was appropriately managed regarding the applied load condition. As a result, it was determined that through the structural analysis, this study has confirmed that the designed engine test equipment is approved for safety, and meets its design purpose at this time.

Development of Continuous Capture Test Architecture in the Boundary Scan (경계면스캔에서의 연속캡쳐 시험구조 개발)

  • Jhang, Young-Sig;Lee, Chang-Hee
    • The KIPS Transactions:PartA
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    • v.16A no.2
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    • pp.79-88
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    • 2009
  • In boundary scan architecture, test stimuli are shifted in one at a time and applied to the on-chip system logic. The test results are captured into the BSR and are examined by subsequent shifting. In this paper, we developed a continuous capture test architecture and test procedure using TPG based on boundary scan is used to performance test. In this architecture, test patterns of TPG are applied to CUT with system clock rate, and response of CUT is continuously captured by CBSR(Continuous Capture Boundary Scan Register) at the same rate and the captured results is shifted to TDO at the same rate. The suggested a continuous capture test architecture and test procedure is simulated by Altera Max+Plus 10.0. The simulation results shows the accurate operation and effectiveness of the proposed test architecture and procedure.