• Journal of the Korean Society of Propulsion Engineers
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• v.23 no.2
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• pp.111-117
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• 2019

An experimental study on the welding part of a heat transfer plate that constitutes the lightweight and high efficiency recuperator is presented in this paper. In particular, to find out the service life of the welded part, fatigue characteristics were determined through experiments. Experiments were carried out on two materials (STS347, AL20-25 + nb), which are selected as the material of the recuperator; further, the specimens were manufactured through the methods used for actual fabrication and the standards recommended by ASTM. To evaluate the mechanical properties of the specimens at room and high temperature, MTS-810 was used in a high-temperature furnace. The tensile test was carried out at room and high temperatures for each specimen. The fatigue test was carried out by setting the load ratio corresponding to 50%, 40%, 30%, 20%, and 10% of the tensile strength at the stress ratio of 0.1. Finally, the fatigue life characteristics obtained by the experiment were compared with the stresses owing to the load generated in the operating conditions of the recuperator, and the lifetime of the welds was evaluated to prepare for the operation time required by the UAV.

• Transactions of the Korean Society of Mechanical Engineers
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• v.12 no.2
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• pp.185-192
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• 1988

Computation of the elasto-plastic solution of ball indentation was carried out by the quadratic programming method. The problem was formulated as an elasto-plastic contact problem under the assumption of small displacement and small deformation and then transformed into a minimization problem. Finite element approximation resulted in a quadratic programming problem. Numerical and experimental study were done with aluminium Al 2024-T351 and commercially pure copper. The computed load-displacement curves were in good agrement with those obtained from experiments. Tabor's relationship for representative strains was also examined. Stress distributions were found to resemble closely those results available in the literature.

• Transactions of the Korean Society of Mechanical Engineers
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• v.6 no.3
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• pp.271-281
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• 1982

이 연구는 테이퍼진 가공물이 동적 절삭상태에서 가지는 한계절삭깊이의 예측을 위한 이론 및 실험적 방법을 논하였다. 절삭 모델은 Usui-Hirota(1)가 제안한 것을, 가공물의 형상은 MTIRA (2)가 제안한 공작기계 동적성능시험용 표준시편을 다소 수정하여 사용하였다. 칩유동각은 Usui-Hirota의 에너지 방법에 의하여 구하였고, Inamura-Sata(6)의 원통형 가공물에 대한 절 삭동력학 이론을 일반화시켜 테이퍼진 가공물에 적용하여 절삭의 안정한계를 구한 후 채터시험 결과와 비교하여 이론의 타당성을 검증하였다.

• Proceedings of the KIEE Conference
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• 2009.07a
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• pp.377_378
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• 2009

HVDC 케이블은 장거리 전력전송, 국가간 계통연계, 비동기 전력계통연계, 전력의 시장화에 따른 전력공급 제어 필요에 따라 세계적으로 널리 사용되고 있다. 국내에서는 현재 유일하게 제주-해남간 180kV HVDC 해저케이블이 운영 중에 있으며, 향후 제주도의 안정적인 전력공급을 위하여 2011년에 제주-육지간 250kV HVDC 해저케이블이 추가로 건설될 예정이다. 그래서 HVDC 해저케이블의 신속 정확하게 안정적이고 신뢰성 있는 운영을 위해서 국내에서 자체 개발한 HVDC 해저케이블에 대한 장기과통전 시험에 대한 평가 및 절차가 필요하게 되었다. 본 논문에서는 HVDC 해저케이블의 장기과통전 시험평가를 위하여 전기적 시험은 CIGRE에서 권고하고 있는 Electra 189, 219에 근거하고 기계적 시험은 IEC 60055-1, Elecrta 171에 근거하여 기술하고자 한다.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.35 no.3
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• pp.223-233
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• 2011

A ceramic monolithic catalyst is a honeycomb structure that consists of two layers. The honeycomb structure is regarded as a continuum in structure and heat-flow analysis. The equivalent mechanical properties of the honeycomb structure were determined by performing finite element analysis (FEA) for a test specimen. Bending strength experiments and FEA of the test specimen used in ASTM C1674-08 standard test were performed individually. The bonding coefficient between the cordierite ceramic layer and the washcoat layer was almost zero. The FEA test specimen was modeled on the basis of the bonding coefficient. The elastic modulus, Poisson's ratio, and the thermal properties of the ceramic monolithic substrate were determined by performing the FEA of the test specimen.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.36 no.6
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• pp.617-622
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• 2012

Structures are often subjected to various types of loading such as static, dynamic, or impact loading. Therefore, experimental and numerical methods have been employed to find adequate material properties according to the conditions. The Split-Hopkinson pressure bar (SHPB) test has frequently been used to test engineering materials, particularly those used under high strain rates. In this study, the compressive deformation behaviors of aluminum alloy under impact conditions have been investigated by means of the SHPB test. The experimental results were then compared with those of finite element analyses. It was shown that reasonably good agreement with the true stress-strain curves was obtained at strain rates ranging from 1000 $s^{-1}$ to 2000 $s^{-1}$. When the strain rate increased by 30%, the peak stress in particular increased by 17%, and the strain also increased by 20%.

• Journal of the Korean Society for Nondestructive Testing
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• v.21 no.3
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• pp.307-312
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• 2001

Ultrasonic signals from Charpy impact test specimen have been analyzed in order to evaluate the integrity of reactor pressure vessel. Base and weld metal that were extracted from reactor vessel doting plant outages according to the schedule of the surveillance test required by the related regulations have been used and the ultrasonic test parameters including velocity, attenuation, etc. showed a close correlations with the amount of neutron irradiation for base metal, relatively homogeneous materials. This result showed certain possibility where a nondestructive method could be used to predict the fluence of the Irradiation due to neutron in nuclear reactor vessel materials.

• Applied Chemistry for Engineering
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• v.21 no.2
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• pp.217-223
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• 2010

In general, fiber-reinforced plastics (FRP) wastes are simply buried or burned. Landfill brings about a permanent contamination of soil due to the inability of FRP to decompose and incineration causes an issue of generating toxic gases and dusts. There have been several ways to treat the FRP wastes such as landfill, incineration, chemical recycling, material recycling and the utilization of energy from combustion. Most methods excluding material recycling are known to have critical limitations in economic, technical and environmental manners. However it is known that material recycling is most desirable among the methods handling FRP wastes. In this study, to investigate the purpose of feasibility of material recycling, various bulk molding compound (BMC) specimens were prepared with the various contents of unsaturated polyester resin binder (25, 30, 35 wt%) and the various replacement ratios of FRP wastes powder (0, 25, 50, 75, 100 wt%) substituted for filler. To evaluate the physical properties BMC specimens, various tests such as tensile strength, flexural strength, impact strength, hot water resistance and SEM imaging were conducted. As a results, mechanical strengths decreased with an increase of replacement ratio of FRP waste powder and physical properties of BMC specimens were deteriorated in the hot water resistance. The fluidity of BMC with more than 50 wt% of the replacement ratio of FRP wastes powder decreased remarkably, causing a problem in the BMC composite.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.2
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• pp.165-170
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• 2012

This paper contains the test method to obtain aerodynamic hinge moments acting on the control surface of air vehicle wing. During the flight, hinge moments make difference between actual control surface angle and control angle which is measured by sensor of actuator. The hinge moments can be obtained by using this difference. Static ground load test and calibration test were conducted to obtain torsional stiffness of control surface actuation system. This results are used to calculate hinge moments. In addition, the mechanical errors of actuation system such as slip angle of mounting point and backlash could be estimated. Using flight test results, this experimental measurement method of hinge moment acting on control surface is conducted. The results of this method are similar to those of numerical simulation method, and the validity of this method is proved.

• Proceedings of the KWS Conference
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• 2009.11a
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• pp.80-80
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• 2009

패키징 구조의 발전이 점차 중요한 문제로 대두되어, 칩의 집적 기술의 발전에 따라 실장기술에서도 고속화, 소형화, 미세피치화, 고정밀화, 고밀도화가 요구되고있다. 최근 선진국을 중심으로 전자 전기기기 및 부품의 실장기술에서도 환경 친화적인 기술을 요구함에 따라, 저에너지 공정 및 무연 실장 기술에 대한 연구가 활발하게 진행되고 있다. 기존의 SOP(Small Out-line Package), QFP(Quad Flat Package) 등은 소형화, 다핀화, 고속화, 실장성에 한계가 있기 때문에, SMT(Surface Mount Technology) 형식으로 된 BGA(Ball Grid Array)가 휴대형 전화를 비롯한 기타 전자 부품 실장에 널리 사용되고 있다. BGA ball shear 법은 BGA 모듈의 생산 및 취급 중에 발생할지도 모르는 기판에 수평으로 작용하는 기계적인 전단력에 BGA solder ball이 견딜 수 있는 정도를 측정하기 위해 사용되는 시험법이다. 전단 시험에 의한 전단 강도의 측정 외에 전기전도도 측정, 파면 관찰, 이동거리(displacement), 유한요소 해석법 등을 병행하여 시험법의 신뢰성 향상에 대한 연구가 이루어지고 있다. 본 실험에서는 지름이 $500{\mu}m$인 Sn-3.5Ag 솔더볼을 이용하여 세라믹 기판을 접합하여 BGA 패키지를 완성하였다. 상부 기판에 솔더볼을 정렬시켜 리플로우 방법으로 접합 한 후 솔더볼이 접합된 상부 기판과 하부 기판을 접합 하여 시편을 제작하였다. 접합된 시편들은 $150^{\circ}C$에서 0~800시간 열처리를 실시하였고, 열처리를 하면서 각각 $3{\times}10^2A/cm^2,\;5{\times}10^3A/cm^2$의 전류를 인가하였다. 시편들을 전단 시험기를 이용하여 솔더볼의 기계적 특성 평가를 하였으며, 계면 반응을 관찰하였다.