• Title/Summary/Keyword: 열기계응력

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A Study of Thermo-Mechanical Behavior and Its Simulation of Silicon Nitride Substrate on EV (Electronic Vehicle)'s Power Module (전기자동차 파워모듈용 질화규소 기판의 열기계적 특성 및 열응력 해석에 대한 연구)

  • Seo, Won;Jung, Cheong-Ha;Ko, Jae-Woong;Kim, Gu-Sung
    • Journal of the Semiconductor & Display Technology
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    • v.18 no.4
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    • pp.149-153
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    • 2019
  • The technology of electronic packaging among semiconductor technologies is evolving as an axis of the market in its own field beyond the simple assembly process of the past. In the field of electronic packaging technology, the packaging of power modules plays an important role for green electric vehicles. In this power module packaging, the thermal reliability is an important factor, and silicon nitride plays an important part of package substrates, Silicon nitride is a compound that is not found in nature and is made by chemical reaction between silicon and nitrogen. In this study, this core material, silicon nitride, was fabricated by reaction bonded silicon nitride. The fabricated silicon nitride was studied for thermo-mechanical properties, and through this, the structure of power module packaging was made using reaction bonded silicon nitride. And the characteristics of stress were evaluated using finite element analysis conditions. Through this, it was confirmed that reaction bonded silicon nitride could replace the silicon nitride as a package substrate.

Cure Shrinkage Behavior of Polymer Matrix Composite according to Degree of Cure (경화도에 따른 고분자 기지 복합재의 경화 수축률 거동)

  • Kwon, Hyuk;Hwang, Seong-Soon;Choi, Won-Jong;Lee, Jae-Hwan;Kim, Jae-Hak
    • Composites Research
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    • v.27 no.3
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    • pp.90-95
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    • 2014
  • Cure shrinkage during cure process of polymer matrix composites develope residual stress that cause some structural deformation, such as spring-in, spring-out and warpage. The carbon/epoxy prepreg used in this study is Hexply M21EV/34%/UD268NFS/IMA-12K supplied by Hexcel corp. Cure shrinkage and degree of cure measured by TMA(thermomechanical analyzer) and DSC(differential scanning calorimetry). Cure shrinkages are measured by TMA within a temperature range of $140{\sim}240^{\circ}C$ in a nitrogen atmosphere, and degree of cure determined by the heat of reaction using dynamic and isothermal DSC runs in argon atmosphere. As a result, the cure shrinkage is increased dramatically in a degree of cure range between 27~80%. the higher the cure temperature, the lower the degree of cure occurring to begin cure shrinkage.

Study on the Thermomechanical Properties of Epoxy-Silica Nanocomposites by FTIR Molecular Structure Analyses (FTIR 분자구조 해석을 통한 에폭시-실리카 나노복합소재의 열기계적 물성 연구)

  • Jang, SeoHyun;Han, Yusu;Hwang, DoSoon;Jung, Juwon;Kim, YeongKook
    • Journal of the Microelectronics and Packaging Society
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    • v.28 no.2
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    • pp.51-57
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    • 2021
  • This paper analyzed the effects of the concentration of nano-silica particles contained in epoxy resin on the thermomechanical properties of the composite materials. The 12nm sized nanoparticles were mixed with epoxy polymer by 5 different weight ratios for the test samples. The glass transition temperature, stress relaxation, and thermal expansion behaviors were measured using dymanic mechanical analyzer (DMA) and thermomechanical analyzer (TMA). It was shown that the nano particle mixing ratios had significant influences on the viscoelastic behaviors of the materials. As the content of the silica particles was increased, the elastic modulus was also increased, while the glass transition temperatures were decreased. Fourier Transform Infrared Spectroscopy (FTIR) results played an important role in determining the causes of the property changes by the filler contents in terms of the molecular structures, enabling the interpretations on the material behaviors based on the chemical structure changes.