• Title/Summary/Keyword: mechanical and thermal behavior

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Thermal Stability and Mechanical Interfacial Properties of DGEBA/PMR-15 Blend System Initiated by Cationic Latent Thermal Catalyst (잠재성 양이온 개시제를 이용한 DGEBA/PMR-15 블렌드계의 열안정성 및 기계적 계면 특성에 관한 연구)

  • Park, Soo-Jin;Lee, Hwa-Young;Han, Mijeong;Hong, Sung-Kwon
    • Journal of Adhesion and Interface
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    • v.5 no.1
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    • pp.3-11
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    • 2004
  • In this work, the cure behaviors of the DGEBA/PMR-15 blends initiated by N-benzylpyrazinium hexafluoroantimonate (BPH) as a cationic latent catalyst were performed in DSC and DMA analyses. And, the thermal stabilities were carried out by TGA analysis and their mechanical interfacial properties of blends were measured in the context of critical stress intensity factor ($K_{IC}$). As a result, the curing activation energy ($E_a$) determined from Ozawa's equation in DSC and the relaxation activation energy ($E_r$) from DMA were increased with increasing PMA-15 content. Also, the thermal stabilities obtained from the integral procedural decomposition temperature (IPDT) and the glass transition temperature ($T_g$) were highly improved with increasing the PMR-15 content, which were probably due to the high heat resistance. And, the $K_{IC}$ showed a similar behavior with $E_a$, which was attributed to the improving of the interfacial adhesion or hydrogen bondings between intermolecular chains.

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Assessment of Creep-Fatigue Crack Growth for a High Temperature Component (고온 기기의 크리프-피로 균열성장 평가)

  • Lee, Hyeong-Yeon;Kim, Jong-Bum;Lee, Jae-Han
    • Proceedings of the KSME Conference
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    • 2008.11a
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    • pp.264-268
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    • 2008
  • An assessment of creep-fatigue crack behavior is required to ensure the structural integrity for high temperature components such as fast breeder reactor structures or thermal power plant components operating at an elevated temperature. In this study, an evaluation of creep-fatigue crack growth has been carried out according to the French assessment guide of the RCC-MR A16 for austenitic stainless steel structures. The assessment procedures for creep-fatigue crack growth in the recent version of the A16 (2007 edition) have been changed considerably from the previous version (2002 edition) and the material properties (RCC-MR Appendix A3) have been changed as well. The impacts of those changes on creep-fatigue crack growth behavior are quantified from the assessments with a structural model. Finally the assessment results were compared with the observed images obtained from the structural tests of the same structural specimen.

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Thermal Stress Analysis of a Fuel Cell Stack using an Orthotropic Material Model (복합재료 연료전지 스택의 열응력 해석)

  • Jeon Ji Hoon;Hwang Woonbong;Um Sukkee;Kim Soowhan;Lim Tae Won
    • Proceedings of the Korean Society For Composite Materials Conference
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    • 2004.04a
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    • pp.206-209
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    • 2004
  • Mechanical behavior of a fuel stack was studied using an orthotropic material model. The fuel stack is essentially composed of a bipolar plate (BP), a gasket, an end plate, a membrane electrolyte assembly (MEA), and a gas diffusion layer (GDL). Each component is fastened with a suitable pressure. It is important to maintain a suitable contact pressure distribution of BP, because it influences the power efficiency of the fuel cell stack. When it is exposed to high temperature, its behavior must be stable. Hence, we performed stress analysis at high temperature as well as at room temperature. At high temperature, the contact pressure distribution becomes poor. Many patents have shown that using an elastomer can overcome this phenomena. Its effect was also studied. By using an elastomer, we found a good contact pressure distribution at high temperature as well as at room temperature.

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Thermo-mechanical Behavior of Wire Bonding PBGA Packages with Different Solder Ball Grid Patterns (Wire Bonding PBGA 패키지의 솔더볼 그리드 패턴에 따른 열-기계적 거동)

  • Joo, Jin-Won
    • Journal of the Microelectronics and Packaging Society
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    • v.16 no.2
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    • pp.11-19
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    • 2009
  • Thermo-mechanical behaviors of wire-bond plastic ball grid array (WB-PBGA) package assemblies are characterized by high-sensitivity moire interferometry. Using the real-time moire setup, fringe patterns are recorded and analyzed for several temperatures. Experiments are conducted for three types of WB-PBGA package that have full grid pattern and perimeter pattern with/without central connections. Bending deformations of the assemblies and average strains of the solder balls are investigated, with an emphasis on the effect of solder interconnection grid patterns, Thermal strain distributions and the location of the critical solder ball in package assemblies are quite different with the form of solder ball grid pattern. For the WB-PBGA-PC, The largest of effective strain occurred in the inner solder ball of perimeter closest to the chip solder balls. The critical solder ball is located at the edge of the chip for the WB-PBGA-FG, at the most outer solder ball of central connections for the WB-PBGA-P/C, and at the inner solder ball closest to the chip for the WB-PBGA-P.

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Study on Behavior Characteristics of Embedded PCB for FCCSP Using Numerical Analysis (수치해석을 이용한 FCCSP용 Embedded PCB의 Cavity 구조에 따른 거동특성 연구)

  • Cho, Seunghyun;Lee, Sangsoo
    • Journal of the Microelectronics and Packaging Society
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    • v.27 no.1
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    • pp.67-73
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    • 2020
  • In this paper, we used FEM technique to perform warpage and von Mises stress analysis on PCB according to the cavity structures of embedded PCB for FCCSP and the types of prepreg material. One-half substrate model and static analysis are applied to the FEM. According to the analysis results of the warpage, as the gap between the cavity and the chip increased, warpage increased and warpage increased when prepreg material with higher modularity and thermal expansion coefficient was applied. The analysis results of the von Mises stress show that the effect of the gap between the cavity and the chip varies depending on prepreg material. In other words, when material whose coefficient of thermal expansion is significantly higher than that of core material, the stress increased as the gap between the cavity and the chip increased. When the prepreg with the coefficient of thermal expansion lower than the core material is applied, the result of stress is opposite. These results indicate that from a reliability perspective, there is a correlation between the structure of the cavity where embedded chips are loaded and prepreg material.

Mechanical and Thermal Analysis of Oxide Fuel Rods

  • Ilsoon Hwang;Lee, Byungho;Lee, Changkun
    • Nuclear Engineering and Technology
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    • v.9 no.4
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    • pp.223-236
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    • 1977
  • An integral computer code has been developed for a mechanical and thermal design and performance analysis of an oxide fuel rod in a pressurized water reactor. The code designated as FROD 1.0 takes into account the phenomena of radial power depression within the pellet, cracking, densification and swelling of the pellet, fission gas release, clad creep, pellet-clad contact, heat transfer to coolant and buildup of corrosion layers on the clad surface. The FROD 1.0 code yields two-dimensional temperature distributions, dimensional changes, stresses, and internal pressure of a fuel rod as a function of irradiation time within a reasonable computation time. The code may also be used for the analyses of oxide fuel rods in other thermal reactors. As an application of FROD 1.0 the behavior of fuel rod loaded in the first core of Go-ri Nuclear Power Plant Unit 1 is predicted for the two power histories corresponding to steady state operation and Codition II of the ANS Classification. The results are compared with the design criteria described in the Final Safety Analysis Report and a discrepancy between these two values is discussed herein.

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Temporal Brittleness of the Mod.9Cr-1Mo Steel (Mod.9Cr1Mo강에서 발생되는 일시적 취성현상)

  • Hur, Sung-Kang;Gu, Ji-Ho;Shin, Kee-Sam;He, Yincheng;Shin, Jong-Ho
    • Korean Journal of Materials Research
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    • v.21 no.11
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    • pp.592-595
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    • 2011
  • It is well known that modified 9Cr-1Mo steel has a low thermal expansion and high thermal conductivity with excellent high temperature properties compared to austenitic stainless steel. For these advantages, the steel is very popular for the boiler tube of thermal power plants. Normalizing is commonly utilized to obtain martensite in this steel, which shows an unusual toughness for martensite. However, some accidents related to this steel have been reported recently, opening the necessity for further study. As a particular behavior of the steel, an abrupt drop of the impact value has been identified upon tempering at 750$^{\circ}C$ for about 1 hour. It is well known that $Fe_3C$ forms during autotempering and turns to $Cr_2C$ at an early stage and then transforms to $Cr_{23}C_6$. In this study, the cause of the abrupt drop of the impact value was investigated with an impact test, microstructural observation, nanodiffraction and phase analyses using instruments such as optical and transmission electron microscopes (TEM) with an extraction carbon replica of the carbides. The analyses revealed that the $M_2C$ that formed when retained for about 1 hour at 750$^{\circ}C$ causes a drastic decrease in the mechanical properties. The sharp drop in mechanical properties, however, disappeared as the $M_2C$ transformed into $M_{23}C_6$ with longer retention.

Evaluation of Structural Safety of Linear Actuator for Flap Control of Aircraft (항공기 플랩 제어를 위한 선형 구동기의 구조 안전성 평가)

  • Kim, Dong-Hyeop;Kim, Sang-Woo
    • Journal of Aerospace System Engineering
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    • v.13 no.4
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    • pp.66-73
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    • 2019
  • The objective of this study was to evaluate the structural safety of the basic design for the linear actuator for the flap control of aircrafts. The kinetic behavior of the linear actuator was determined using the multi-body dynamics (MBD) analysis, and the contact force was calculated to be used as input data for the structural analysis based on the finite element analysis. In the structural analysis, the thermal and static behaviors of the linear actuator satisfying the designed velocity were examined, and the structural safety of the linear actuator evaluated. Moreover, the dynamic behaviors of the key components of the linear actuator were investigated by the modal analysis. The actuation rod linearly moved with about 5 mm/s when the motor operated at 225 rpm and the maximum contact force of 32.83 N occurred between two driving gears. Meanwhile, the structural analysis revealed that the maximum thermal and static stresses were 1.57% and 78% of the yield strength of steel, respectively, and they were in a safe range of the structure. In addition, the linear actuator for the basic design is stable to the resonance by avoiding the natural frequencies of the components.

A Study on the 43$0^{\circ}C$ Degradation Behavior of Cast Stainless Steel(CF8M)(II)-Evaluation of Low Cycle Fatigue Characteristics- (주조 스테인리스강 CF8M의 43$0^{\circ}C$ 열화거동에 관한 연구 (II) -저사이클 피로특성 평가-)

  • Gwon, Jae-Do;U, Seung-Wan;Park, Jung-Cheol;Lee, Yong-Seon;Park, Yun-Won
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.24 no.9 s.180
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    • pp.2183-2190
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    • 2000
  • A thermal aging is observed in a primary reactor cooling system(RCS) made of a casting stainless steel when the RCS is exposed for long period at the reactor operating temperature, 290~3300C An investigation of effects of thermal aging on a low cycle fatigue characteristics included a stress variations caused by a reactor operation and trip, is required. The purpose of the present investigation is to find an effect of a thermal aging of the CF8M on a low cycle fatigue life. The specimen of CF8M are prepared by an artificially accelerated aging technique holding 300 and 1800hr at 4300C respectively. The low cycle fatigue tests for the virgin and two aged specimens are performed at the room temperature for various strain amplitudes($\varepsilon$ta), 0.3, 0.5, 0.8, 1.0, 1.2 and 1.5% strain. Through the experiment, it is found that the fatigue life is rapidly reduced with an creasing of the aging time. The experimental fatigue life estimation formulas between the virgin and two aged specimen are obtained and are proposed to a analysis purpose.

Numerical Analysis of 1-D Ablation and Charring of a Composite Heat Insulator Using Finite Analytic Method (유한해석법을 이용한 조합 내열부품의 1차원 삭마 및 숯층 형성 해석)

  • 함희철;배주찬;이태호;전광민;이진호
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.16 no.5
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    • pp.943-951
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    • 1992
  • The objectives of this study are to analyse the thermal response behavior occurring in the charring ablative material more realistically by considering ablation and char phenomena occurring in several material layers, and to increase the reliability of thermal analysis by being able to get stable solutions through using the finite analytic method. A program has been developed to predict the temperature distribution, ablation thickness, char thickness, ablation velocity and char velocity by solving non-linear one-dimensional heat conduction equation. Results of calculation were compared with results of published papers. From this compariosn this program was proved to be a very good tool for thermal design and analysis of charring ablative materials used in the rocket propulsion system.