• 제목/요약/키워드: bonding force test

검색결과 79건 처리시간 0.029초

Flip-chip 본딩 장비 제작 및 공정조건 최적화 (Bonding process parameter optimization of flip-chip bonder)

  • 심형섭;강희석;정훈;조영준;김완수;강신일
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2005년도 추계학술대회 논문집
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    • pp.763-768
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    • 2005
  • Bare-chip packaging becomes more popular along with the miniaturization of IT components. In this paper, we have studied flip-chip process, and developed automated bonding system. Among the several bonding method, NCP bonding is chosen and batch-type equipment is manufactured. The dual optics and vision system aligns the chip with the substrate. The bonding head equipped with temperature and force controllers bonds the chip. The system can be easily modified for other bonding methods such as ACF In bonding process, the bonding forte and temperature are known as the most dominant bonding parameters. A parametric study is performed for these two parameters. For the test sample, we used standard flip-chip test kit which consists of FR4 boards and dummy flip-chips. The bonding test was performed fur two types of flip-chips with different chip size and lead pitch. The bonding temperatures are chosen between $25^{\circ}C\;to\;300^{\circ}C$. The bonding forces are chosen between 5N and 300N. The bonding strength is checked using bonding force tester. After the bonding force test, the samples are examined by microscope to determine the failure mode. The relations between the bonding strength and the bonding parameters are analyzed and compared with bonding models. Finally, the most suitable bonding condition is suggested in terms of temperature and force.

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이종결합 고속회전 발사 탄의 비행 안정성에 결합력이 미치는 영향성 분석 (Analysis of How the Bonding Force between Two Assemblies Affects the Flight Stability of a High-speed Rotating Projectile)

  • 이상봉;최낙선;이종현;김상민;강병덕
    • 품질경영학회지
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    • 제49권3호
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    • pp.255-268
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    • 2021
  • Purpose: We sought to understand why a high-speed rotating projectile featuring a fuze-and-body assembly sometimes exhibited airburst, and we intended to improve the flight stability by eliminating airburst. Methods: We performed characteristic factor analysis, structural mechanics modeling, and dynamic modeling and simulation; and we scheduled firing tests to discover the cause of airburst. We used a step-by-step procedure to analyze the reliability function for selecting the bonding force standard that prevents airburst. Results: The 00MM high-speed rotating projectile features a fuze bonded to a body assembly; the bonding sometimes can break on firing. The resulting contact force, vibration and roll damping during flight generated yaw. Flight became unstable; fuze operation triggered an airburst. Our reliability test improved the bonding force standard (the force was increased). When the bonding force was at least the minimum required, a firing test revealed that airburst/flight instability disappeared. Conclusion: Analysis and identification of the causes of flight instability and airburst render military training safer and enhance combat power. Ammunition must perform as designed. Our method can be used to set standards that improve the performances of similar types of ammunition.

형상기억합금 선재가 삽입된 폴리머기지 능동복합재료의 회복력에 미치는 계면 접합강도의 영향 (Effect of interface bonding strength on the recovery force of SMA reinforced polymer matrix smart composites)

  • 김희연;김경섭;홍순형
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2003년도 춘계학술발표대회 논문집
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    • pp.18-21
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    • 2003
  • The effect of interface bonding strength on the recovery force of SMA wire reinforced polymer matrix composites was investigated by pullout test. Firstly, the recovery forces and transformation temperatures of various prestrained SMA wires were measured and 5% prestrained SMA wires were prepared for the reinforcements of composites. EPDM incorporated with 20vol% silicon carbide particles(SiCp) of 6, 12, $60{mutextrm{m}}$ size were used as matrix. Pullout test results showed that the interface bonding strength increased when the SiCp size decreased due to the increase of elastic modulus of matrix. Cyclic test of composites was performed through control of DC current at the constant displacement mode. The abrupt decrease of recovery force during cycle test at high current was occurred by thermal degradation of matrix. This was in good agreement with temperature related in the thermal degradation of matrix. The hysteresis of recovery force with respect to the temperature was compared between wire and composite and the hysterisis of composites was smaller than the wire due to less thermal conduction.

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열압착 접합 조건에 따른 경·연성 인쇄회로기판 간 Sn-58Bi 무연솔더 접합부의 기계적 특성 (Effects of Bonding Conditions on Mechanical Strength of Sn-58Bi Lead-Free Solder Joint using Thermo-compression Bonding Method)

  • 최지나;고민관;이상민;정승부
    • 마이크로전자및패키징학회지
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    • 제20권2호
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    • pp.17-22
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    • 2013
  • 본 연구에서는 Sn-58Bi 솔더를 이용한 경성 인쇄 회로 기판 (Rigid printed circuit board, RPCB)과 연성 인쇄회로 기판 (Flexible printed circuit board, FPCB) 간의 열압착 접합 시, 접합 조건에 따른 기계적 특성에 대하여 연구하였다. 접합 온도와 접합 시간을 변수로 열압착 접합을 실시하여 $90^{\circ}$ 필 테스트(Peel test)를 통해 접합 강도를 측정하고, 단면과 파단면을 관찰하였다. 접합 온도가 증가할수록 접합 강도가 증가하였으며, 접합 시간에 따른 접합 강도의 변화 또한 관찰할 수 있었다. 접합 시간이 증가하면서 접합부의 파괴에 영향을 미치는 요인이 솔더 층에서 금속간 화합물(Intermetallic compound, IMC) 층으로 변화하는 것을 관찰할 수 있었다. 필 테스트 과정의 F-x(Force-distance) curve를 통해 파괴 에너지를 계산하여 금속간 화합물이 접합 강도에 미치는 영향을 평가하였으며, 본 연구에서 $195^{\circ}C$, 7초 조건이 접합 강도와 파괴 에너지가 가장 높게 나타나는 최적 접합 조건으로 도출되었다.

Dynamic ice force estimation on a conical structure by discrete element method

  • Jang, HaKun;Kim, MooHyun
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제13권1호
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    • pp.136-146
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    • 2021
  • This paper aims to numerically estimate the dynamic ice load on a conical structure. The Discrete Element Method (DEM) is employed to model the level ice as the assembly of numerous spherical particles. To mimic the realistic fracture mechanism of ice, the parallel bonding method is introduced. Cases with four different ice drifting velocities are considered in time domain. For validation, the statistics of time-varying ice forces and their frequencies obtained by numerical simulations are extensively compared against the physical model-test results. Ice properties are directly adopted from the targeted experimental test set up. The additional parameters for DEM simulations are systematically determined by a numerical three-point bending test. The findings reveal that the numerical simulation estimates the dynamic ice force in a reasonably acceptable range and its results agree well with experimental data.

반도체 패키징용 Gold Bonding Wire의 변형특성 및 해석 (Deformation Properties of Gold Bonding Wire for VLSI Packaging Applications)

  • 김경섭;홍순형
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2001년도 춘계학술대회 논문집
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    • pp.250-253
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    • 2001
  • Mechanical properties of gold bonding wire for VLSI packaging have been studied. The diameters of gold wires are about 20-30 micrometer and fracture loads are 8-20 gram force. The elastic modulus, yield strength, fracture strength and elongation properties have been evaluated by micro-tensile test method. This work discusses for an appropriate selection of micro-force testing system and grip design in mim testing. The best method to determine gauge length of wire and to measure tensile properties has been proposed. The mechanical properties such as strength and elastic modulus of current gold bonding wire are higher than pure those of gold wire.

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와이어 본딩시 본딩 패드 리프트 불량에 관한 연구 (Study on the Bonding Pad Lift Failure in Wire Bonding)

  • 김경섭;장의구;신영의
    • 한국전기전자재료학회논문지
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    • 제11권12호
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    • pp.1079-1083
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    • 1998
  • In this study, ultrasonic power of Aluminum wire bonder, bond time and bond force are investigated and valued in order to minimize failure of bonding pad lift. We also tried to control those 3 factors properly. We got the conclusion that if we turn down the ability of ultrasonic power or bond time, we can get a pad lift from a boundary between bond pad ad wire because pad metal and wire joining is unstable, but it is best condition when it ultrasonic power is 100∼130unit, bond time is 15∼20msec and bond force is 4∼6gf.

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Cu-C$u_2$O의 공정반응에 의한 구리와 알루미나의 직접접합 (The Direct Bonding of Copper to Alumina by $Cu-Cu_2$O Eutectic Reaction)

  • 유환성;이임열
    • 한국재료학회지
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    • 제2권4호
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    • pp.241-247
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    • 1992
  • 본 연구에서는 $Cu-Cu_2$O의 공정반응에 의한 구리와 알루미나의 직접접합에 대하여 연구 하였다. $1.5{\times}10^{-1}$torr, $1015^{\circ}C$에서 산화시킨 후 $10_{-3}$torr, 107$5^{\circ}C$에서 접합시킨 시편의 접합력과 계면특성을 인장시험, SEM, EDS 및 XRD를 통하여 분석하였다. 3분 산화시켜 접합하면 우수한 접합강도를 보이며 산화시간이 이보다 짧거나 길면 결합력은 저하하였다. 과단은 알루미나 공정조직 계면에서 발생하였으며 파단후 $Al_2O_3$표면에는 Cu쪽에서 빠져나간 $Cu_2$O nodule의 존재하였는 바 접합력은 $Cu_2$O-A$l_2O_3$계면보다는 $Cu-Cu_2$O계면에 좌우됨을 보여주고 있다. 접합력은 접합시간에 따라 완만한 증가를 보였으며 CuA$l_2O_4$$CuAlO_2$의 반응생성물이 접합중 형성되었다.

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고온 시효 시험에 따른 Epoxy 솔더 접합부의 접합 특성 평가 (Evaluation of Bonding Properties of Epoxy Solder Joints by High Temperature Aging Test)

  • 강민수;김도석;신영의
    • 한국전기전자재료학회논문지
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    • 제32권1호
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    • pp.6-12
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    • 2019
  • Bonding properties of epoxy-containing solder joints were investigated by a high temperature aging test. Specimens were prepared by bonding an R3216 standard chip resistor to an OSP-finished PCB by a reflow process with two basic types of solder (SAC305 & Sn58Bi) pastes and two epoxy-solder (SAC305+epoxy & Sn58Bi+epoxy) pastes. In all epoxy solder joints, an epoxy fillet was formed in the hardened epoxy, lying around the outer edge of the solder joint, between the chip and the Cu pad. In order to analyze the bonding characteristics of solder joints at high temperatures, a high-temperature aging test at $150^{\circ}C$ was carried out for 14 days (336 h). After aging, the intermetallic compound $Cu_6Sn_5$ was found to have formed in the solder joint on the Cu pad, and the shear stress on the conventional solder joint was reduced by a significant amount. The reason that the shear force did not decrease much, even though in epoxy solder, was thatbecause epoxy hardened at the outer edge of the supported solder joints. Using epoxy solder, strong bonding behavior can be ensured due to this resistance to shear force, even in metallurgical changes such as those where intermetallic compounds form at solder joints.

탄소섬유판으로 보강된 RC보의 휨 거동 (Flexural Behavior of RC Beams Strengthened with CFRP Strips)

  • 최기선;유영찬;박영환;박종섭;김긍환
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 2005년도 봄학술 발표회 논문집(I)
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    • pp.287-290
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    • 2005
  • CFRP strips manufactured in factory are produced normally with smaller width and larger thickness than CFRP sheets. By this reason, bonding force between CFRP strips and concrete substrate is not sufficient to sustain tensile force in CFRP strips. Therefore premature debonding failure cannot be avoided when strengthening is done by simply bonding the CFRP strips. The flexural strength of RC beam strengthened with CFRP strips must be calculated based on the effective strain considering debonding failure. This paper presents test results of an experimental study conducted to evaluate the flexural strength on RC beams strengthened with CFRP strips. 7 specimens were tested with respect to bond length and amount of CFRP strips. From the test results, it was indicated that the strain of the CFRP strips achieved at debonding failure can be decreased less than 6,000$\mu$ depending on the amount of CFRP strips.

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