• Journal of the Korean Society for Nondestructive Testing
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• v.36 no.3
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• pp.225-230
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• 2016

Fiber Bragg grating (FBG) sensors are currently the most prevalent sensors because of their unique advantages such as ease of multiplexing and capability of performing absolute measurements. They are applied to various structures for structural health monitoring (SHM). The signal characteristics of FBG sensors under thermal loading should be investigated to enhance the reliability of these sensors, because they are exposed to certain cyclic thermal loads due to temperature changes resulting from change of seasons, when they are applied to structures for SHM. In this study, tests on specimens are conducted in a thermal chamber with temperature changes from -$20^{\circ}C$ to $60^{\circ}C$ for 300 cycles. For the specimens, two types of base materials and adhesives that are normally used in the manufacture of packaged FBG sensors are selected. From the test results, it is confirmed that the FBG sensors undergo some degree of compressive strain under cyclic thermal load; this can lead to measurement errors. Hence, a pre-calibration is necessary before applying these sensors to structures for long-term SHM.

• Proceedings of the Materials Research Society of Korea Conference
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• 2002.05a
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• pp.163-163
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• 2002

• Proceedings of the Korean Nuclear Society Conference
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• 2002.05a
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• pp.254-254
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• 2002

• Proceedings of the Materials Research Society of Korea Conference
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• 2002.11a
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• pp.191-191
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• 2002

• Proceedings of the KIPE Conference
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• 2013.07a
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• pp.220-221
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• 2013

UPS 부하시험시 또는 DC 전압원 방전 시험시에 사용되는 일반 저항 또는 역률 부하 시험기를 사용하지 않고 UPS 내부 역변환부 출력전원을 출력 스위치와 바이패스 스위치를 통해서 순변환부 입력전원에 재공급함으로써 시험용 저항부하기 또는 역률 부하 시험기와 같이 모든 에너지를 열로 소비하지 않고 순변환부 측으로 재 순환시켜서 UPS 부하시험 시 입력 전원용량이 UPS 최소 내부 손실분만으로도 이미 현장 설치 및 운영 중인 UPS에서도 별도의 부하 시험기 및 시험용 케이블을 이동, 설치하지 않고 주기적인 UPS 점검 시, 적용 가능한 에너지 절감형 부하시험기법에 관해 연구하였다.

• Journal of Korea Society of Industrial Information Systems
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• v.28 no.6
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• pp.21-27
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• 2023

Modern naval ships install an Infra-Red Signature Suppression system (IRSS) in their exhaust pipe to reduce infrared signature emitted to the outside. In addition, naval ships are strategic assets with a very long life cycle, so high reliability of the performance of the equipment on board must be guaranteed. Therefore, equipment such as IRSS is evaluated for performance through model testing at the design stage. A variety of measuring instruments are used in IRSS model testing, and the reliability of these instruments must also be guaranteed. In this paper, a study was conducted to evaluate the reliability of measurement equipment used in IRSS model testing. The test equipment and instruments used were a hot gas wind tunnel, pitot tube, digital differential pressure gauge, thermocouple sensor, and digital recorder. As the fan speed of the hot gas wind tunnel increased, the measurement deviation of the flow decreased, and the temperature output of the thermocouple sensor showed differences in response time and stability depending on the method used.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2003.05b
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• pp.16-19
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• 2003

YBCO film을 이용하여 2 stripe-meander 형태의 초전도 한류기를 제작하고 시험하였다. 초전도 film의 hot spot에 의해 발생하는 열을 분산시키기 위해 gold shunt layer를 입혔다. 사고각 $0^{\circ}$에서 사고발생 후 최초 quench 전류값은 $9.56A_{peak}$이었고 약 0.63 msec동안 fast quench 가 진행되고 이후에는 gold층의 열발생에 의한 저항증가가 약 3주기동안 진행된 후 안정되었다. 사고각 $45^{\circ}$와 $90^{\circ}$ 에서는 전류가 상승하는 도중 혹은 최고지점에서 사고가 발생했기 때문에 fast quench time이 각각 0.56 msec와 0.26msec를 보였다. 초전도 한류기를 적용하였을 때 사고전류는 사고직후 약 5배, 3주기후에는 약 8.5배까지 효과적으로 제한함을 알 수 있었다.

• Proceedings of the KAIS Fall Conference
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• 2011.12b
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• pp.492-495
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• 2011

본 연구는 가속수명시험을 통해 배기파이프 용접부의 수명평가에 관해 다루고 있다. 배기파이프 용접부는 실차 상태에서 열과 진동이 많이 가는 부분으로 내구에 많이 취약하다. 배기 파이프에 주기적인 하중을 가하여 가속시험하여, 배기파이프 용접부에 대한 신뢰성관련 수명특성을 빠른시간 내에 산출하기 위한 것이다. 적절한 수명분포 및 고장데이터를 수집분석하고 시험방법 과 시험결과를 활용하여 신뢰성 보증 시험시간을 단축하고 제품의 개발단계 및 일정 축소와 시험비용 감소 및 제품의 보증수명증대에 기여할 것이다.

• Aerospace Engineering and Technology
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• v.13 no.1
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• pp.76-85
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• 2014

In this paper, the equivalent coefficient of thermal expansion (CTE) of fiber reinforced plastic composite material is investigated with various CTE prediction schemes. Although there are several methods for predicting the equivalent CTEs, most of them have some limitations of are not much accurate when comparing prediction results with test results. In the framework of computational homogenization, a representative volume element is taken from the predefined fiber-volume ratio, and modelled with finite element mesh. Finally, the equivalent CTEs are obtained by applying periodic boundary condition. To verify the performance of the proposed method, the results obtained are compared with those by the existing methods and test results. Additionally, the thermal pointing error analysis for star tracker support structure is conducted and its accuracy is estimated according to CTE prediction schemes.

• Journal of Aerospace System Engineering
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• v.16 no.6
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• pp.90-98
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• 2022

The output of an infrared (IR) sensor mounted on an EO/IR payload is known to change during a mission period in an orbital environment. As it is required to calibrate the output of the IR sensor periodically to obtain high-quality images, an on-board black body system is mounted on the payload. All systems operating in the space environment require performance tests on ground to verify the target performance in the orbital environment. Therefore, it is also required to test the black body system to verify the performance of the surface temperature uniformity and the estimated representative temperature error within the target temperature range in the operating environment. In this study, calibration of the estimated representative temperature error and verification of the thermal performance of the black body system were conducted by performed a performance test in the thermal vacuum chamber applying deep space radiation cooling effect of an orbital environment.