• 제목/요약/키워드: Thermal cycles

검색결과 494건 처리시간 0.029초

Thermal cycle하에서의 OSP 표면 처리된 BGA 패키지의 신뢰성 연구 (Reliability of BGA Package with OSP Surface Finish under Thermal Cycle)

  • 이종범;노보인;이영호;정승부
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2006년도 춘계 학술대회 개요집
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    • pp.206-208
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    • 2006
  • The reliability of BGA (ball grid array) package with OSP (organic surface preservative) surface finish under thermal cycle was investigated by using SEM (scanning electron microscopy), EDS(energy dispersive spectroscopy), image tool and ball shear test. The IMCs (intermetallic compounds) were increased with increasing number of thermal cycles. However, the shear strengths of solder ball were decreased with increasing number of thermal cycles. The order of solders which had the highest shear strength as follow: Sn-3.5wt%Ag-0.7wt%Cu, Sn-0.7wt%Cu, Sn-37wt%Pb.

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열충격에 의한 열차폐 코팅재의 기계적 거동 변화 (Changes in the Mechanical Behavior of Thermal Barrier Coatings Caused by Thermal Shock)

  • 장빈;이기성;김태우;김철
    • 한국재료학회지
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    • 제27권1호
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    • pp.25-31
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    • 2017
  • This study investigates changes in the mechanical behaviors, especially hardness and indentation load-displacement curves, of thermal barrier coatings (TBCs) brought about by thermal shock. The TBCs on the Nickel-based bondcoat/superalloy was prepared with diameters of 25.4 mm and $600{\mu}m$ thickness. The results of thermal shock cycling test from $1100^{\circ}C$ of the highest temperature indicate that the thermal shock do not influence on the mechanical behavior, but a continuous decrease in porosity and increase in hardness were observed after 1200 thermal shock cycles; these changes are believed to be due to sintering of thermal barrier coating materials. The results that no degradation in the indentation load-displacement curves indicate that the coating shows good thermal shock resistance up to 1200 cycles at $1100^{\circ}C$ in air.

Darveaux 모델에 의한 플립칩 패키지 솔더 접합부의 열피로 해석 및 수명 평가 (The Thermal Fatigue Analysis and Life Evaluation of Solder Joint for Flip Chip Package using Darveaux Model)

  • 신영의;김연성;김종민;최명기
    • Journal of Welding and Joining
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    • 제22권6호
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    • pp.36-42
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    • 2004
  • Experimental and numerical approaches on the thermal fatigue for the solder joint of flip chip package are discussed. However, it is one of the most difficult problems to choose the proper fatigue model. It was found that viscoplstic FE model with Darveaux method was very desirable and useful to predict the thermal fatigue life of solder joint for flip chip package under $208{\~}423K$ thermal cycling condition such as steep slope of temperature(JEDEC standard condition C). Thermal fatigue life was 1075 cycles as a result of viscoplatic model. It was a good agreement compared to the experimental. And also, it was found from the experimental that probability of the thermal fatigue life was $60{\%}$ at 1500 cycles.

An evaluation of power conversion systems for land-based nuclear microreactors: Can aeroderivative engines facilitate near-term deployment?

  • Guillen, D.P.;McDaniel, P.J.
    • Nuclear Engineering and Technology
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    • 제54권4호
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    • pp.1482-1494
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    • 2022
  • Power conversion cycles (Subcritical Steam, Supercritical Steam, Open Air Brayton, Recuperated Air Brayton, Combined Cycle, Closed Brayton Supercritical CO2 (sCO2), and Stirling) are evaluated for land-based nuclear microreactors based on technical maturity, system efficiency, size, cost and maintainability, safety implications, and siting considerations. Based upon these criteria, Air Brayton systems were selected for further evaluation. A brief history of the development and applications of Brayton power systems is given, followed by a description of how these thermal-to-electrical energy conversion systems might be integrated with a nuclear microreactor. Modeling is performed for optimized cycles operating at 3 MW(e) with turbine inlet temperatures of 500 ℃, 650 ℃ and 850 ℃, corresponding to: a) sodium fast, b) molten salt or heat pipe, and c) helium or sodium thermal reactors, coupled with three types of Brayton power conversion units (PCUs): 1) simple open-cycle gas turbine, 2) recuperated open-cycle gas turbine, and 3) recuperated and intercooled open-cycle gas turbine. Aeroderivative turboshaft engines employing the simple Brayton cycle and two industrial gas turbine engines employing recuperated air Brayton cycles are also analyzed. These engines offer mature technology that can facilitate near-term deployment with a modest improvement in efficiency.

열화학싸이클 수소를 제조를 위한 (Cu0.5Mn0.5)Fe2O4의 열적 거동 (Thermal Behaviors of (Cu0.5Mn0.5)Fe2O4 for H2 production by thermochemical cycles)

  • 김진웅;최승철;주오심;정광덕
    • 한국수소및신에너지학회논문집
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    • 제15권1호
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    • pp.32-38
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    • 2004
  • Thermal behaviors of $(Cu_{0.5}Mn_{0.5})Fe_2O_4$, prepared by a solid method, were investigated for $H_2$ production by a thermochemical cycle. The thermal reduction of $(Cu_{0.5}Mn_{0.5})Fe_2O_4$ started from $300^\circ{C}$ and the weight loss was 1.3 wt% up to 1200. XRD shows the prepared ferrite has the spinel structure with a lattice constant of $8.414{\AA}$ and changed to the oxygen deficient structure by thermal reduction. Oxygen and hydrogen can be separately produced by the cycles of thermal reduction and water oxidation of the oxygen deficient ferrite.

Repair bond strength of composite resin to zirconia restorations after different thermal cycles

  • Cinar, Serkan;Kirmali, Omer
    • The Journal of Advanced Prosthodontics
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    • 제11권5호
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    • pp.297-304
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    • 2019
  • PURPOSE. This in vitro study investigated the repair bond strength of the zirconia ceramic after different aging conditions. MATERIALS AND METHODS. In order to imitate the failure modes of veneered zirconia restorations, veneer ceramic, zirconia, and veneer ceramic-zirconia specimens were prepared and were divided into 4 subgroups as: control ($37^{\circ}C$ distilled water for 24 hours ) and 3000, 6000, 12000 thermal cycling groups (n=15). Then, specimens were bonded to composite resin using a porcelain repair kit according to the manufacturer recommendation. The repair bond strength (RBS) test was performed using a universal testing machine (0.5 mm/min). Failure types were analyzed under a stereomicroscope. Two-way ANOVA and Bonferroni test were used for statistical analysis. RESULTS. The RBS values of zirconia specimens were statistically significant and higher than veneer ceramic and veneer ceramic-zirconia specimens in control, 3000 and 6000 thermal cycling groups (P<.05). When 12000 thermal cycles were applied, the highest value was found in zirconia specimens but there was no statistically significant difference between veneer ceramic and veneer ceramic-zirconia specimens (P>.05). Veneer ceramic specimens exhibited cohesive failure types, zirconia specimens exhibited adhesive failure types, and veneer ceramic-zirconia specimens exhibited predominately mixed failure types. CONCLUSION. Thermal cycling can adversely affect RBS of composite resin binded to level of fractured zirconia ceramics.

저온 열원 활용을 위한 암모니아-물 혼합물을 작동유체로 하는 칼리나 사이클의 성능 해석 (Performance Analysis of Kalina Cycle using Ammonia-Water Mixture as Working Fluid for Use of Low-Temperature Energy Source)

  • 김경훈;고형종;김세웅
    • 한국수소및신에너지학회논문집
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    • 제22권1호
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    • pp.109-117
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    • 2011
  • Since the thermal performance of cycles for use of low-temperature source is low if a pure working fluid is used, the cycles using ammonia-water binary mixture as a working fluid has attracted much attention over past two decades. Recently, several commercial power plants using Kalina cycles have been built and being operated successfully. In this work thermodynamic performance of Kalina cycles using ammonia-water mixture as a working fluid is investigated for the purpose of extracting maximum power from low-temperature energy source. Special attention is paid to the effect of system parameters such as concentration of ammonia and turbine inlet pressure on the characteristics of the system. Results show that the system performance is influenced sensitively by the ammonia concentration, and the role of the performance of heat exchangers is crucial.

경사화 두께를 갖는 열차폐 코팅의 열적 내구성 평가 (Evaluation of Thermal Durability for Thermal Barrier Coatings with Gradient Coating Thickness)

  • 이승수;김준성;정연길
    • 한국산학기술학회논문지
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    • 제21권8호
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    • pp.248-255
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    • 2020
  • 경사화 두께를 갖는 열차폐 코팅의 열적 내구성과 열적 안정성에 대한 코팅층 두께의 영향을 화염 열피로 시험과 열충격 시험을 통해서 조사하였다. Bond 층과 top 층은 각각 Ni-Cr계 상용 MCrAlY 분말과 상용 이트리아 안정화 지르코니아 (YSZ) 분말을 사용하여 니켈기지의 초내열합금 모재 (GTD-111)에 대기 플라즈마 용사법 (APS)으로 코팅층을 형성하였다. 1100 ℃의 화염으로 1429회 열피로 시험 후 bond 층이 일부 산화되고 top 층과 bond 층 계면에서 열화에 의한 산화층 (TGO)이 관찰되었으나, 코팅층 부위와 관계없이 균열이나 박리현상 없는 양호한 미세구조를 나타내었다. 1100 ℃ 열충격 시험결과, 37회 열충격 테스트 후 코팅층의 얇은 부위에서 박리가 시작되어 98회 시험 후 코팅층의 50% 이상이 박리되었으며, 코팅층의 두께가 얇게 형성된 부위는 코팅층이 두껍게 형성된 부위에 비해, top 층의 박리와 함께 bond 층의 산화가 많이 진행되었으며, 코팅층 두께가 상대적으로 두껍게 형성된 부위에서 열차폐 효과의 증가로 인해 bond 층의 내산화성과 열적 안정성이 우수한 것으로 나타났다.

수치시뮬레이션에 의한 박판 용접 변형 예측에 관한 기초적 연구 (A Fundamental Study on Forecast of the Thin Plate Welding Deformation by Numerical Simulation)

  • 김종명;박창수;김영표;방한서
    • Journal of Welding and Joining
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    • 제21권1호
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    • pp.93-98
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    • 2003
  • For construction of steel structures, thin steel plates have been often used and welding is the main manufacturing process. However, welding processes cause some problems(welding residual stresses, welding deformations, etc.). In these problems, welding deformation is extremely harmful to the safety of structures especially. Therefore, in this study, a numerical analysis program based on large deformation plate theory has been developed to analyze and predict the welding deformation in thin plates. From the result of numerical analyse, we can find two parameters, thermal cycles and mechanical restraints affecting the welding deformation of structures. It is considered that large difference of thermal cycles and mechanical restraints in the width direction bring about welding deformation. Results of simulation have the same tendency of deformation distribution in width direction as experimental formulas.

복합재료의 열충격 특성 평가 (A Study on Thermal Shock Characterization of Composite)

  • 이진경;박영철;이준현;이상필
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2004년도 추계학술발표대회 논문집
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    • pp.246-249
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    • 2004
  • A smart material is used as spectacle frames and brassiere frames, and partly in medical supplies because of its shape memory effect. The smart composite can be used on the wing of an airplane instead of the existing aluminium to control crack propagation. In this study, the smart composite was fabricated by a hot press method. TiNi alloy as reinforcement and A16061 as matrix were used, respectively. The mechanical properties of the smart composite under thermal shock cycles were evaluated. In addition, Acoustic Emission techniques were also used to clarify the damage behavior of the smart composite under thermal shock cycles nondestructive.

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