• 제목/요약/키워드: room temperature bonding

검색결과 153건 처리시간 0.022초

Determination of Trace Elements of Ge and P in a Gold Bonding Wire by Inductively Coupled Plasma Atomic Emission Spectrometry

  • Choi, Sung-Min;Lee, Gae-Ho;Han, Jae-Kil
    • Bulletin of the Korean Chemical Society
    • /
    • 제29권2호
    • /
    • pp.393-397
    • /
    • 2008
  • Inductively coupled plasma atomic emission spectrometry (ICP-AES) was used to determine the presence of germanium and phosphorus in a pure gold bonding wire. The samples were dissolved with hydrobromic acid and nitric acid at room temperature. The quantitation limits were 0.012 mg L-1 at 265.118 nm for Ge and 0.009 mg L-1 at 177.495 nm for P. Using the mixed acid digestion formula of DIW+HBr+HNO3, the recoveries were in the range of 98-100% and the relative standard deviation was within 1.1-2.3%. On the other hand, the amount of Ge decreased by about 16.2% using DIW+HCl+HNO3, due to the formation of a volatile compound. The Ge contents determined using the external method and the standard addition method were 9.45 mg kg-1 and 9.24 mg kg-1, respectively, and the P contents, using the same methods, were 22.49 mg kg-1 and 23.09 mg kg-1, respectively. Both methods were successfully used to determine the trace amounts of P and Ge in the pure gold bonding wire samples.

Mg-Zn-RE/Al1050 클래드재의 제조 및 기계적 특성 (Fabrication and Mechanical Characterization of the Mg-Zn-RE/Al1050 Clad Sheet)

  • 신범수;윤석연;하창성;윤승관;배동현
    • 대한금속재료학회지
    • /
    • 제48권2호
    • /
    • pp.116-121
    • /
    • 2010
  • The Mg-Zn-RE alloy cladded with the thin Al1050 sheet was fabricated by means of a roll bonding process at $280^{\circ}C$.Microstructures and mechanical properties of the clad sheets were investigated. After heat treatment at $230^{\circ}C$ for 30 min, an Mg-rich diffusion layer with about $2{\mu}m$ in thickness was developed at the Mg and Al interface. Tensile tests were carried out in a temperature range up to $300^{\circ}C$. The clad sheet exhibits superior elongation to failure not only at room temperature but also at elevated temperatures compared with those of the Mg alloy sheet. For the deformed specimens, interface debonding does not occur and the diffusion layer shows only a few cracks.

카올린-인산염-물계의 저온 특성에 관한 연구 (A Study on Low Temperature Properties of Kaolin-Phosphate-Water Systems)

  • 박금길;박근원
    • 한국세라믹학회지
    • /
    • 제18권3호
    • /
    • pp.192-200
    • /
    • 1981
  • This study deals with the low temperature ($25^{\circ}C$-$600^{\circ}C$) properties of Kaolin-Phosphate-water systems. Phosphoric acid, mono aluminum phosphate, mono ammonium phosphate, the mixture of phosphoric acid and mono aluminum phosphate, and the mixture of phosphoric acid and mono ammonium phosphate were used to characterize the M.O.R. of the systems with to quantity of phosphates, curing time, and firing temperature. Firing shrinkage, viscosity, surface tension, DTA, TGA, and X-ray diffraction patterns were also measured in order to investigated the factors of strengthening. The results of this study were summarized as follows: 1. The M.O.R. of kaolin-phosphate systems were stronger than that of Kaolin-water system at room temperature or low temperature($25^{\circ}C$-$600^{\circ}C$). Though it was increased according to the longer curing time, the higher temperature, and the more addition of phosphate, the M.O.R. were decreased in the case of 10 wt% phosphate addition in the system of phosphoric acid, mono aluminum phosphate and phosphoric acid-mono aluminum phosphate. 2. When the concentration of Phosphate was at 4 wt%, the M.O.R. of specimen cured at $25^{\circ}C$ and added to the phosphoric acid was strongest among the specimens in added to the others phosphates. Whereas, when the concentration of phosphate was above 6wt%, the M.O.R. of specimen cured at $25^{\circ}C$ and added to the phosphoric acid mono ammonium phosphate system cured at $25^{\circ}C$ was the strongest. 3. The M.O.R. of the specimen heated, in the temperature range of 15$0^{\circ}C$-1$600^{\circ}C$, and added to the mixture of phosphoric acid-mono aluminum phosphate system or phosphoric acid-mono ammonium phosphate system was stronger than that of specimen added to Phosphoric acid, mono-aluminum Phosphate or mono-ammonium phosphate alone. 4. The bonding force of phosphate binders was more closely related to surface tension than viscosity and it tended to be inversely proportional to surface tension. The bonding force after heating treatment seemed to be caused by the change of structure of phosphate according to heating.

  • PDF

규사(硅砂)의 입도(粒度)에 따른 주물사(鑄物砂)의 상온성질(常溫性質)에 관(關)한 연구(硏究) (A Study on the Room Temperature Properties of Molding Sand with different Sand Grain Size)

  • 최동수;이계완
    • 한국주조공학회지
    • /
    • 제3권3호
    • /
    • pp.167-173
    • /
    • 1983
  • The effect of sand grain size on the various properties of mold is not only basic but important interest which we have to deal with.And the relation among the various properties of mold (strength, permeability, flowability, compactability, hardness, deformation, toughness etc.) is very complicated and inaccurate, so we can delineate the behavior of mixture (sand+water+bentonite) with experience only. Within recent years a so-called rigid-water theory has been accepted as a means of advancing logical explanations for the research aimed at delineating sand-clay-water relationships. By changing grain size or mesh no. of grain, specimens have been subjected to green compressive strength, permeability, deformation, flowability, compactablity, toughness at room temperature. Under constant mulling energy and ratio of water/bentonite, the results obtained were as follows: 1. With decreasing grain size green compressive strength of the specimen increased. 2. With decreasing grain size permeability decreased. 3. With decreasing grain size flowability and bulk density decreased but compactability increased. 4. With decreasing grain size deformation decreased but toughness increased. 5. At 60 mesh no., the properties of specimen are conspicuously changed. The reason is that the total surface area of sand grain which affects the type of bonding between sand grains is more changed at 60 mesh number.

  • PDF

금형주조법을 이용한 TiNi/6061Al 지적복합재료의 제조 및 기계적 특성 (Fabrication and Mechanical Properties of TiNi/6061Al Smart Composite by Permanent Mold Casting)

  • 김순국;이준희;윤두표;박영철;이규창;김영희
    • 한국주조공학회지
    • /
    • 제18권6호
    • /
    • pp.534-540
    • /
    • 1998
  • 6061Al-matrix composite with TiNi shape memory fiber as reinforcement has been fabricated by Permanent Mold Casting to investigate the mechanical properties of the smart composites. The composites have showed good interface bonding as a result of the analysis of SEM and EDX. The smartness of composite is given due to the shape memory effect of the TiNi fiber which generates compressive residual stresses in the matrix material when heated after being prestrained. The tensile strength of the composites was tested at temperatures between $90^{\circ}C$ and room temperature with increasing amount of pre-strain, and it showed that the tensile strength at $90^{\circ}C$ was higher than that of the room temperature. Especially, the tensile strength of the composite increases with increasing pre-strain. It showed that hardness of matrix was higher than that of common 6061Al alloy.

  • PDF

핫프레스법에 의한 TiNi/Al6061 형상기억복합재료의 제조 및 기계적 특성에 관한 연구 (Fabrication and Characterization of TiNi Shape Memory Alloy Fiber Reinforced 6061 Aluminum Matrix Composite by Using Hot Press)

  • 박동성;이준희;이규창;박영철
    • 대한기계학회논문집A
    • /
    • 제26권7호
    • /
    • pp.1223-1231
    • /
    • 2002
  • Al alloy matrix composite with TiNi shape memory fiber as reinforcement has been fabricated by hot pressing to investigate microstructures and mechanical properties. The analysis of SEM and EDS showed that the composites have shown good interface bonding. The stress-strain behavior of the composites was evaluated at temperatures between 363K and room temperature as a function of prestrain, and it showed that the yield stress at 363K was higher than that of the room temperature. Especially, the yield stress of this composite increases with increasing the amount of prestrain, and it also depends on the volume fraction of fiber and heat treatment. The smartness of the composite is given due to the shape memory effect of the TiNi fiber which generates compressive residual stress in the matrix material when heated after being prestrained. Microstructural observation has revealed that interfacial reactions occur between the matrix and fiber, creating two intermetallic layers.

Room Temperature Ferromagnetism on Co and Fe Doped Multi-wall Carbon Nano-tube

  • Chae, K.H.;Gautam, S.;Yu, B.Y.;Song, J.H.;Augustine, S.;Kang, J.K.;Asokan, K.
    • 한국진공학회:학술대회논문집
    • /
    • 한국진공학회 2011년도 제40회 동계학술대회 초록집
    • /
    • pp.171-171
    • /
    • 2011
  • Co and Fe doped multi-wall carbon nano-tubes (MWCNTs) synthesized by microwave plasma enhanced chemical vapor deposition (PECVD) technique are investigated with synchrotron radiations at Pohang Light Source (PAL) and European Synchrotron Radiation Facility (ESRF). Near edge x-ray absorption spectroscopy (NEXAFS) measurement at C K, Co $L_{3,2}$ and Fe $L_{3,2}$-edges, and x-ray magnetic circular dichroism (XMCD) at Co and Fe $L_{3,2}$-edges have been carried at 7B1 XAS KIST and 2A MS beamline, respectively, to understand the electronic structure and responsible magnetic interactions at room temperature. X-ray absorption spectroscopy (XAS) at C K-edge shows significant p-bonding and Co and Fe L-edges proves the presence of $Co^{2+}$ and $Fe^{2+}$ in octahedral symmetry. Co and Fe doped MWCNTs show good XMCD spectra at 300K. The effect on the magnetism is also studied through swift heavy ion (SHI) radiations and magnetism is found enhanced and change in the electronic structure in Co-CNTs is investigated.

  • PDF

상온접합 본딩이 있는 복합재 날개의 저온 구조시험 (Low Temperature Structural Tests of a Composite Wing with Room Temperature-Curing Adhesive Bond)

  • 하재석;박찬익;이기범
    • 한국항공우주학회지
    • /
    • 제43권10호
    • /
    • pp.928-935
    • /
    • 2015
  • 본 논문에서는 상온접합이 있는 무인기 복합재 날개의 저온 구조시험에 대하여 소개하였다. 본 시험에 사용된 날개구조는 탄소섬유 강화 복합재료로 구성되며, 내부 구조물과 스킨은 상온접착제로 접합되었다. 또한 날개구조의 손상허용성을 검증하기 위하여 육안으로 확인이 거의 불가능한 충격손상을 스킨의 주요 부위에 인위적으로 적용하였다. 무인기 운용 고도의 온도환경을 모사하기 위한 저온 챔버를 특별히 제작하였으며, 날개구조는 챔버내에 고정시키고 챔버 외부에 설치한 유압 작동기를 이용하여 하중을 부가하였다. 구조시험은 변형률 개관 시험 및 1배 수명 피로하중 스펙트럼에 대한 손상허용시험으로 구성된다. 변형률 게이지와 광섬유 센서를 이용하여 본딩영역 및 주요 부위의 변형률을 측정하였으며, 압전 구동기/센서를 이용하여 손상의 변화를 모니터링 하였다. 시험결과로부터 날개구조는 1배 수명에 대한 운용환경을 모사한 환경 하에서 구조적 건전성을 보유하고 있음을 확인하였다.

레이저 공정변수 변화에 따른 다이아몬드상 카본박막의 전계방출 특성분석 (Investigation on field emission properties of diamond-like carbon thin film by variation of laser processing parameters)

  • 심경석;이상렬
    • 대한전기학회:학술대회논문집
    • /
    • 대한전기학회 1999년도 하계학술대회 논문집 D
    • /
    • pp.1511-1513
    • /
    • 1999
  • In order to investigate the properties of diamond-like carbon(DLC) thin films depending on the deposition parameters, DLC thin films were systematically fabricated by pulsed laser deposition (PLD), DLC thin films have been shown advantageous field emission properties due to a negative electron affinity (NEA) and a low work function. At the atomic level. DLC is referred to the group of carbon materials with strong chemical bonding composition of $sp^2$ and $sp^3$ arrangements of atoms incorporated with an amorphous structure. The experiment was performed at substrate temperature in the range of room temperature to $600^{\circ}C$. The laser energy densiy was used to be in the range of $6J/cm^2$ to $20J/cm^2$, SEM, Raman, PL, XPS and field emission characteristics were used to investigate the DLC thin films.

  • PDF

자전고온반응에 의한 적층복합재료의 제조공정 (Fabrication Process of Laminated Composites by Self-propagating High-temperature Synthesis Reaction)

  • 김희연;정동석;홍순형
    • 한국복합재료학회:학술대회논문집
    • /
    • 한국복합재료학회 2002년도 춘계학술발표대회 논문집
    • /
    • pp.155-158
    • /
    • 2002
  • Fabrication process of metal/intermetallic laminated composites by using self-propagating high temperature synthesis(SHS) reactions between Ni and Al elemental metal foils have been investigated. Al foils were sandwiched between Ni foils and heated in a vacuum hot press to the melting point of aluminium. SHS reaction kinetics was thermodynamically analyzed through the final volume fraction of the unreacted Al related with the initial thickness ratio of Ni:Al and diffusion bonding stage before SHS reaction. Thermal aging of laminated composites resulted in the formation of functionally gradient series of intermetallic phases. Microstructure showed that the main phases of intermetallics were NiAl and $Ni_3Al$ having higher strength at room and high temperatures. The volume fractions of intermetallic phases were measured as 82.4, 58.6, 38.4% in 1:1, 2:1, 4:1 initial thickness ratio of Ni:Al.

  • PDF