• 한국염색가공학회지
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• 제33권2호
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• pp.72-78
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• 2021

The purpose of this study, the purpose of this study is to activate the antibacterial effect on the Chlorinated polyvinyl chloride film by using Octadecyldimethyl (3-triethoxy silylpropyl) ammonium chloride antibacterial agent with Chlorinated polyvinyl chloride polymer, which is inexpensive and has excellent properties such as heat resistance and chemical resistance. The Chlorinated polyvinyl chloride polymer was dissolved in a dimethylacetamide solvent, and film samples were prepared by varying the ratio of Octadecyldimethyl (3-triethoxy silylpropyl) ammonium chloride to study the antibacterial performance. A Scanning Electron Microscope-Energy Dispersive X-ray Spectrometer and X-ray photoelectron spectroscopy were employed to confirm the elements in the samples. According to the initial decomposition temperature of the Chlorinated polyvinyl chloride film and the Chlorinated polyvinyl chloride/Octadecyldimet hyl (3-triethoxy silylpropyl) ammonium chloride(10%) film using a Thermogravimetric analyzer(TA-DTA), it was confirmed that the initial decomposition temperature was lowered due to the influence of Octadecyldimethyl (3-triethoxy silylpropyl) ammonium chloride. In addition, in order to measure the mechanical properties, Universal testing machine was used and the result showed that a strength of Chlorinated polyvinyl chloride/Octadecyldimethyl (3-triethoxy silylpropyl) ammonium chloride(10%) was 36.8 MPa. The antimicrobial properties of the Chlorinated polyvinyl chloride/Octadecyldimethyl (3-triethoxy silylpropyl) ammonium chloride(10%) film showed 99.9% antimicrobial properties.

• 한국융합학회논문지
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• 제11권12호
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• pp.131-135
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• 2020

본 연구에서는 경비행기를 날게 하는 프로펠러인 3개 및 5개 또는 10개가 있는 날개의 모델들로서 공기 유동 해석을 하였다. Model A에 대해서는 5개의 날개들이 있는 유동 형상으로서 Model A가 가장 이상적인 공기의 흐름을 보이고 있다. 너무 많거나 적지도 않은 날개 수로 공기의 흐름이 가장 원활히 흐르는 형상을 나타내고 있다. 프로펠러 날개의 수가 적으면 적을수록 공기의 유동이 작아지는 것을 볼 수 있다. Model A는 공기 유동의 전면부에서 최대 0.5631 MPa의 압력을 받고 있다. 또한 Model B와 Model C는 0.5758 MPa 및 0.5589 MPa의 압력을 각각 받고 있다. 각 유동 모델들에 대한 압력 등고선들을 비교해 보면, Model B가 그 압력 분포가 제일 높은 것으로 볼 수 있다. 본 연구 결과를 활용하면 실제 시험을 하지 않고서도 공기 유동을 조사할 수 있다. 또한 경비행기 프로펠러의 미적인 융합 설계에 도움이 될 수 있다고 보인다.

• The Journal of Advanced Prosthodontics
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• 제12권6호
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• pp.376-382
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• 2020

PURPOSE. To determine the shear bond strengths of different denture base resins to different types of prefabricated teeth (acrylic, nanohybrid composite, and cross-linked) and denture teeth produced by computer-aided design/computer-aided manufacturing (CAD/CAM) technology. MATERIALS AND METHODS. Prefabricated teeth and CAD/CAM (milled) denture teeth were divided into 10 groups and bonded to different denture base materials. Groups 1-3 comprised of different types of prefabricated teeth and cold-polymerized denture base resin; groups 4-6 comprised of different types of prefabricated teeth and heat-polymerized denture base resin; groups 7-9 comprised of different types of prefabricated teeth and CAD/CAM (milled) denture base resin; and group 10 comprised of milled denture teeth produced by CAD/CAM technology and CAD/CAM (milled) denture base resin. A universal testing machine was used to evaluate the shear bond strength for all specimens. One-way ANOVA and Tukey post-hoc test were used for analyzing the data (α=.05). RESULTS. The shear bond strengths of different groups ranged from 3.37 ± 2.14 MPa to 18.10 ± 2.68 MPa. Statistical analysis showed significant differences among the tested groups (P<.0001). Among different polymerization methods, the lowest values were determined in cold-polymerized resin.There was no significant difference between the shear bond strength values of heat-polymerized and CAD/CAM (milled) denture base resins. CONCLUSION. Different combinations of materials for removable denture base and denture teeth can affect their bond strength. Cold-polymerized resin should be avoided for attaching prefabricated teeth to a denture base. CAD/CAM (milled) and heat-polymerized denture base resins bonded to different types of prefabricated teeth show similar shear bond strength values.

• 한국산학기술학회논문지
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• 제22권1호
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• pp.87-93
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• 2021

현대 무기체계는 전자장비 탑재의 비중이 늘어나고 있으며, 그에 따른 소프트웨어 탑재비중도 늘어나고 있다. 소프트웨어 비중이 높아감에 따라 그 품질관리와 개발방법에 대한 관심도 높아졌다. 물리적으로 가시화 된 기계체계와 달리 논리적으로 비가시화 된 소프트웨어는 결함에 노출될 경우 복구의 어려움, 재사용의 어려움, 자원의 낭비와 같은 위험에 놓여 질 수 있다. 미국의 경우 국방 소프트웨어의 개발과 품질관리를 위한 별도의 프로세스를 연구하고 적용하는 노력을 통해 CMM(Capability Maturity Model)을 만드는 성과도 거두었다. 우리나라 또한 국제표준을 바탕으로 국방 소프트웨어 개발 및 품질관리에 대한 기준을 만들어 활용하고 있다. 그러나 소프트웨어의 발전 속도에 맞추어 기준을 변경해야 함에도 아직 기초수준에 머무르고 있다는 지적이 있다. 소프트웨어 발전 속도에 비해 기준이 낮다면, 자원 재사용 비용 및 복구비용이 기하급수적으로 늘어난다. 본 논문에서는 CMM의 소프트웨어 테스트 파생형인 TMMi(Test Maturity Model-integration)을 통해 국방 소프트웨어 테스트 절차 발전 방안에 대해 논의하고, 국방 소프트웨어 품질관리에 대한 청사진을 제시하고자 한다.

• 대한금속재료학회지
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• 제47권3호
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• pp.202-208
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• 2009

The effects of aging time on the microstructure and shear strength of the Low Temperature Co-fired Ceramic (LTCC)/Ag pad/Electroless Nickel Immersion Gold (ENIG)/BGA solder joints were investigated through isothermal aging at $150^{\circ}C$ for 1000 h with conventional Sn-37Pb and Sn-3Ag-0.5Cu. $Ni_3Sn_4$ intermetallic compound (IMC) layers was formed at the interface between Sn-37Pb solder and LTCC substrate as-reflowed state, while $(Ni,Cu)_3Sn_4$ IMC layer was formed between Sn-3Ag-0.5Cu solder and LTCC substrate. Additional $(Cu,Ni)_6Sn_5$ layer was found at the interface between the $(Ni,Cu)_3Sn_4$ layer and Sn-3Ag-0.5Cu solder after aging at $150^{\circ}C$ for 500 h. Thickness of the IMC layers increased and coarsened with increasing aging time. Shear strength of both solder joints increased with increasing aging time. Failure mode of BGA solder joints with LTCC substrate after shear testing revealed that shear strength of the joints depended on the adhesion between Ag metallization and LTCC. Fracture mechanism of Sn-37Pb solder joint was a mixture of ductile and pad lift, while that of Sn-3Ag-0.5Cu solder joint was a mixture of ductile and brittle $(Ni,Cu)_3Sn_4$ IMC fracture morphology. Failure mechanisms of LTCC/Ag pad/ENIG/BGA solder joints were also interpreted by finite element analyses.

• 한국산학기술학회논문지
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• 제22권1호
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• pp.327-332
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• 2021

패키지레벨에서 반도체의 신뢰성 검사는 테스트 소켓에 반도체 칩 패키지를 탑재시킨 상태에서 테스트가 진행되며, 테스트 소켓은 기본적으로 반도체 칩 패키지의 형태에 따라서 그 모양이 결정되는 것이 일반적이다. 또한, 반도체 칩 패키지의 리드와 소켓 리드의 기계적인 접촉에 의해 테스트 장비와 연결하는 매개체의 역할을 하며, 신호전달 과정에서 신호의 손실을 최소화하여 반도체에 검사신호를 잘 전달할 수 있도록 하는 기능이 핵심이다. 본 연구에서는 이웃하고 있는 전기 전달 경로의 상호 영향성을 검사 할 수 있는 기술을 적용함으로써 수명 검사와 정밀 측정뿐만 아니라 이웃하고 있는 전기 전달 경로의 구조를 포함하여 단 한 번의 접촉을 통해 100개미만의 실리콘 테스트 소켓의 합선 테스트가 가능하도록 개발하였다. 개발된 장치의 테스트 결과 99%이상의 테스트 정밀도와 0.66이하의 동시 검사속도 특성을 나타내었다.

• 대한조선학회논문집
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• 제57권6호
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• pp.322-330
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• 2020

This study deals with underwater explosion (UNDEX) characteristics of various non-explosive underwater shock sources for the development of non-explosive underwater shock testing devices. UNDEX can neutralize ships' structure and the equipment onboard causing serious damage to combat and survivability. The shock proof performance of naval ships has been for a long time studied through simulations, but full-scale Live Fire Test and Evaluation (LFT&E) using real explosives have been limited due to the high risk and cost. For this reason, many researches have been tried to develop full scale ship shock tests without using actual explosives. In this study, experiments were conducted to find the characteristics of the underwater shock waves from actual explosive and non-explosive shock sources such as the airbag inflators and Vaporizing Foil Actuator (VFA). In order to derive the empirical equation for the maximum pressure value of the underwater shock wave generated by the non-explosive impact source, repeated experiments were conducted according to the number and distance. In addition, a Shock Response Spectrum (SRS) technique, which is a frequency-based function, was used to compare the response of floating bodies generated by underwater shock waves from each explosion source. In order to compare the magnitude of the underwater shock waves generated by each explosion source, Keel Shock Factor (KSF), which is a measure for estimating the amount of shock experienced by a naval ship from an underwater explosionan, was used.

• 한국염색가공학회지
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• 제34권1호
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• pp.58-67
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• 2022

In this study, self-reinforced composite(SRC) was prepared using HDPE(High density polyethylene) fabric(2×2 plain) and LDPE(Low density polyethylene) film. The optimal conditions were derived by manufacturing specimens according to the temperature of 100 ~ 140℃ using a hot stamping at a pressure of 100bar for 10 minutes in order to find the optimal conditions for the SRC. The manufactured SRC was analyzed for tensile properties, compressive strength and shear strength through a universal testing machine(UTM). As a result of the measurement, the P3 specimen prepared by hot stamping at a temperature of 130℃ and a pressure of 100bar for 10 minutes was found to be higher than other specimens with tensile strength and tensile modulus of 210MPa and 19GPa, compressive strength 69MPa and shear strength 13MPa and it was considered to be optimal condition. Finally, the composite material according to the fabric structure was modeled using experimental values and the physical properties of the composite material according to the fabric structure were predicted using GeoDict and Digimat.

• 대한조선학회논문집
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• 제59권4호
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• pp.200-206
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• 2022

This study is to develop database by an experimental method for the development of condition based maintenance for auxiliary equipment in marine engine systems. Existing ships have been performing regular maintenance, so the actual measurement data development is very incomplete. Therefore, it is best to develop a database on land tests. In this paper, a database developed by an experimental method is presented. First, failure case analysis and reliability analysis were performed to select a failure mode. For the failure simulation test, a test bed for land testing was developed. The failure simulation test was performed based on the failure simulation scenario in which the failure simulation test plan was defined. A 1.5TB failure simulation database has been developed, and it is expected to serve as a basis for ship failure diagnosis and prediction algorithm model development.

• Structural Engineering and Mechanics
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• 제81권3호
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• pp.349-365
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• 2022

Steel fibre-reinforced concrete (SFRC) is an emerging class of composite for construction. However, a reliable method to assess the flexural behaviour of SFRC structural member is in lack. An analytical technique is proposed for determining the moment-curvature response of concrete beams reinforced with steel fibres and longitudinal bars (R/SFRC members). The behaviour of the tensile zone of such members is highly complex due to the interaction between the residual (tension softening) stresses of SFRC and the tension stiffening stresses. The current study suggests a transparent and mechanically sound method to combine these two stress concepts. Tension stiffening is modelled by the reinforcement-related approach assuming that the corresponding stresses act in the area of tensile reinforcement. The effect is quantified based on the analogy between the R/SFRC member and the equivalent RC member having identical geometry and materials except fibres. It is assumed that the resultant tension stiffening force for the R/SFRC member can be calculated as for the equivalent RC member providing that the reinforcement strain in the cracked section of these members is the same. The resultant tension stiffening force can be defined from the moment-curvature relation of the equivalent RC member using an inverse technique. The residual stress is calculated using an existing model that eliminates the need for dedicated mechanical testing. The proposed analytical technique was validated against test data of R/SFRC beams and slabs.