• 한국수소및신에너지학회논문집
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• 제23권6호
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• pp.612-618
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• 2012

In this paper, in order to prevent electric shock of high voltage system of HFCV after crash test, insulation performance measurement methods were studied. Under conditions of in-use, insulation performance tests can be divided into measurement method using the vehicle's own RESS as DC voltage source and measurement method using DC voltage from off-vehicle sources. However, these tests can not be applied after a post-crash because parts of high voltage system cover should be removed, and insulation performance can be influenced during these tests. Therefore, we proposed post-crash insulation performance test methods for preventing electric shock through problem analysis of previous post-crash insulation performance tests. Also, test equipment which can measure voltage absence and total energy was developed. We verified performance of the equipment through experiments with vehicle test.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 춘계학술대회논문집
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• pp.957-961
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• 2005

A satellite component must withstand vibration caused when launch vehicle acoustics and engine rumble transfer to it through its structural mount. Components shall be subjected to environmental tests after manufacturing process thus the environmental test conditions are needed for component level test including vibration and shock. This paper deals with derivation of component-level environmental test specifications, especially for solar panels of STSAT-2(Science & Technology SATellite-2). Sine sweep random vibration, and shock test conditions were generated for solar panels by assuming the satellite as single-degree-of-freedom system with a base excitation.

• International Journal of Reliability and Applications
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• 제15권1호
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• pp.11-22
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• 2014

New classes of life distributions called new better (worse) than used at age $t_0$ in Laplace transform order, NBUL- $t_0$(NWUL - $t_0$) are introduced. For the classes NBUL - $t_0$(NWUL - $t_0$), preservation under convolution, mixture, mixing and the homogeneous Poisson shock model are studied. In the sequel, we obtain a test for $H_0$ : F is exponential versus $H_1$ : F is NBUL - $t_0$ and not exponential. The critical values and the powers of this test are calculated to assess the performance of the test. It is shown that the proposed test has high efficiencies for some commonly used distributions in reliability. Sets of real data are used as examples to elucidate the use of the proposed test for practical problems.

• Journal of Welding and Joining
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• 제7권2호
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• pp.25-34
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• 1989

The purpose of this work is to coat ZrO$_{2}$ - 8Y$_{2}$O$_{3}$ ceramic on the Al cast alloy(AC-8A) by using the plasma spray method. Two types of coatings which were composed of two and three layer coating were examined. Each coating powder was analyzed for shape and size distribution and X-ray diffraction pattern. For the coated layers, microstructural analysis and performance estimation which was composed of static thermal test, thermal cyclic test and thermal shock test were conducted.

• 한국음향학회지
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• 제41권5호
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• pp.589-600
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• 2022

탄도형 체외 충격파 치료기의 출력 에너지를 측정하는 Dry Test Bench(DTB)의 신뢰성을 검증하기 위해, 상용 탄도형 충격파 치료기에 대해 Laser Doppler Vibrometer(LDV)로 측정된 충격파의 음향 에너지와 비교했다. 실험 결과, DTB로 측정된 역학적 에너지는, 동일한 출력 설정에서, 5 % 이내의 변동성을 보이며, 치료기의 전 출력 설정 범위에서 LDV로 측정된 충격파의 음향 에너지와 선형적인 상관성(adj. R² = 0.991)을 확인했다. 두 측정 방법의 상관성과, LDV을 이용하여 공기 및 수중에서 측정된 충격파 음향 에너지의 상관성(adj. R² = 0.995)을 통합하면, DTB 측정으로부터 수중에서 발생된 충격파의 energy flux density를 평균 7.85 % 오차로 추정된다. DTB는 치료기의 출력에너지에 대한 정보만 제공하기 때문에, IEC61846 및 IEC63045에서 요구하는 다양한 충격파의 음향 출력을 시험하는 도구로 적합하지 않다. 그러나 측정 원리가 단순하고 사용이 용이한 DTB는 제조사 및 사용자가 탄도형 Extracorporeal Shock Wave Therapy(ESWT) 치료기의 성능을 관리하는 목적으로 유용하게 사용될 수 있을 것으로 기대된다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2010년도 춘계학술대회 논문집
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• pp.857-858
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• 2010

• International Journal of Automotive Technology
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• 제5권4호
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• pp.297-302
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• 2004

This paper presents the low cycle thermal fatigue of the engine exhaust manifold subject to thermo-mechanical cyclic loading. As a failure of the exhaust manifold is mainly caused by geometric constraints of the less expanded inlet flange and cylinder head, the analysis is based on the exhaust system model with three-dimensional temperature distribution and temperature dependent material properties. The result show that large compressive plastic deformations are generated at an elevated temperature of the exhaust manifold and tensile stresses are remained in several critical zones at a cold condition. From the repetition of these thermal shock cycles, maximum plastic strain range (0.454%) could be estimated by the stabilized stress-strain hysteresis loops. It is used to predict the low cycle thermal fatigue life of the exhaust manifold for the thermal shock test.

• Journal of Mechanical Science and Technology
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• 제14권3호
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• pp.298-305
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• 2000

The functionally graded material (FGM) is the new concept for a heat resisting material. FGM consists of ceramics on one side and metal on the other. A composition and microstructure of an intermediate layer change continuously from ceramics to metal at the micron level. This study is carried out to analyze the thermal shock characteristics of functionally graded PSZ/ metal composites. Heat-resistant property was evaluated by gas burner heating test using $C_2H_2/O_2$ combustion flame. The ceramic surface was heated with burner flame and the bottom surface cooled with water flow. Also, the composition profile and the thickness of the graded layer were varied to study the thermo mechanical response. Furthermore, this study carried out the thermal stress analysis to investigate the thermal characteristics by the finite element method. Acoustic emission (AE) monitoring was performed to detect the microfracture process in a thermal shock test.

• Journal of Welding and Joining
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• 제24권6호
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• pp.21-27
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• 2006

This study was focused on the evaluation of the thermo-mechanical board-level reliability of Pb-bearing and Pb-free surface mount assemblies. The composition of Pb-bearing solder was a typical Sn-37Pb and that of Pb-free solder used in this study was a representative Sn-3.0Ag-0.5Cu in mass %. Thermal shock test was chosen for the reliability evaluation of the solder joints. Typical $Cu_6Sn_5$ intermetallic compound (IMC) layer was formed between both solders and Cu lead frame at the as-reflowed state, while a layer of $Cu_3Sn$ was additionally formed between the $Cu_6Sn_5$ and Cu lead frame during the thermal shock testing. Thickness of the IMC layers increased with increasing thermal shock cycles, and this is very similar result with that of isothermal aging study of solder joints. Shear test of the multi layer ceramic capacitor(MLCC) joints was also performed to investigate the degradation of mechanical bonding strength of solder joints during the thermal shock testing. Failure mode of the joints after shear testing revealed that the degradation was mainly due to the excessive growth of the IMC layers during the thermal shock testing.

• 한국항공우주학회지
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• 제36권12호
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• pp.1229-1235
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• 2008

비상위치송신기(ELT)는 무수한 조난시의 응급구조에 큰 역할을 해왔다. 비행사, 항해사 그리고 지상 사용자들은 세상 어디에서든지 비상시에 조난신호를 위성에 송신이 가능한 장치를 갖추고 있는 것이다. 이 논문에서는 비상위치송신기의 본체를 낙하충격에 대하여 MSC/Dytran을 이용하여 해석하였다. 그리고 그 결과를 Karas' Example 이론 결과에 비교하였다. 또한, 추락생존성 시험에 대해 MSC/Nastran을 이용해 해석하였다. 비상위치송신기의 충격조건하에 과도응답해석을 하였다.