• 제목/요약/키워드: hole 형상

검색결과 312건 처리시간 0.032초

마이크로 전자기판의 미세 피치 블라인드 비아홀의 충진 거동 (Via Filling in Fine Pitched Blind Via Hole of Microelectronic Substrate)

  • 이민수;이효수
    • 마이크로전자및패키징학회지
    • /
    • 제13권1호통권38호
    • /
    • pp.43-49
    • /
    • 2006
  • 새로운 잔류 기공 추출 공정을 적용하여 Blind via hole(BVH)의 형상에 따라 발생되는 잔류기공 특성, 거동 및 신뢰성평가를 수행하였다. 잔류 기공 추출 공정을 적용한 시편에서는 잔류기공이 완전히 제거 되었으며, 기존 공정으로 제조된 시편에 비하여 40% 수준의 향상된 결과를 나타내었다. BVH의 형상에 관계없이 1.5기압수준으로 약 30초 이상 동안 추출하면 BVH내부의 잔류기공은 제거 되어지며 JEDEC 기준의 신뢰성으로 평가한 결과 BVH내부에 잔류기공은 존재하지 않았다.

  • PDF

회전원판에 존재하는 구멍의 형상변화가 강도에 미치는 영향 (The effect of shape change of holes in rotating disc on disc strength)

  • 김병진;심재준;한동섭;이성욱;한근조;안찬우;안성찬
    • 한국정밀공학회:학술대회논문집
    • /
    • 한국정밀공학회 2002년도 추계학술대회 논문집
    • /
    • pp.796-799
    • /
    • 2002
  • The stress of the rotating disc with several types of hole was investigated in detail in this paper. Maximum circumferential stress of rotating disc by changing hole shape with same area, were studied using FEM. The results obtained were as follows: 1. The disc which rotates at high speed is subjected to circumferential stress remarkably. 2. When the number of circular holes in rotating disc is four, stress reduction effect is maximum. 3. When shape of holes in rotating disc is cylindrical elongated hole, maximum circumferential stress of the rotating disc decreased most.

  • PDF

브레이크 디스크 형상에 따른 대류열전달에 의한 방열성능 연구 (STUDY ON COOLING PERFORMANCE BY CONVECTIVE HEAT TRANSFER WITH DIFFERENT DISK BRAKE SHAPES)

  • 박찬우;이동렬
    • 한국전산유체공학회지
    • /
    • 제21권1호
    • /
    • pp.64-71
    • /
    • 2016
  • This research is to numerically investigate the convective cooling performance in the Disk brake. Research concentrates on the heat transfer coefficient and cooling performance which are selected with cooling local locations. Cooling performance of the Hole disk has been compared by Ventilated Disk. According to the results of heat transfer on the disk brake, activated velocity distributions more appear in the Hole disk. This is due to the fact that a number of hole units have exactly 120 on the surface of the hole disk. Therefore, velocity distributions of hole disk brake is better activated than Ventilated disk. According to the calculations of Nusselt number between surface and atmosphere in the interested cooling area, average value of cooling effect has been increased 13.5% by the hole disk at driving of speed 65 km/h situation and grown 18% by the hole disk at driving speed of 100 km/h. Due to the flow of air through the hole route, cooling performance of the hole disk was very excellent. In addition, cooling effect on edge of the bottom is better than the vicinity of center.

고강도 열연재의 홀 플랜징시 립 형상이 플랜정성에 미치는 효과 (Effect of Lip Shape on the Hole Flangeability of High Strength Steel Sheets)

  • 김정운;김봉준;문영훈
    • 대한기계학회논문집A
    • /
    • 제26권1호
    • /
    • pp.147-152
    • /
    • 2002
  • Effect of lip shape on the hole flangeability of high strength steel sheets is investigated. Circular plates of various hole sizes are tested and the variation of lip length as well as the variation of thickness on the sectional views of the finished lip were studied. The conventional hole flanging process is limited to a certain limit hole diameter below which failure will ensue during the hole expansion. The intention of this work is to examine the effect of lip shape on the flangeability of TRIP steel and Ferrite-Bainite duplex steel and find out major parameters which can affect flanging shape of high strength hot rolled steels. Over the ranges of conditions investigated, the minimum hole diameter of F+B steel is better than TRIP steel. while, the lip-shape accuracy of TRIP steel is better than that of F+B steel. although the tensile strength and elongation of %P steel are superior than those of Ferrite-Bainite duplex steel, the flangeability is found to be not so strongly sensitive to the tensile properties but sensitive to displacement on the circumferential direction of hole edge.

노즐 형상 변경이 소형 CRDI 엔진의 성능에 미치는 영향에 대한 수치 해석적 연구 (Numerical Study on the Effect of Nozzle Geometry on the Small CRDI Engine Performance)

  • 민세훈;서현규
    • 한국분무공학회지
    • /
    • 제20권4호
    • /
    • pp.254-260
    • /
    • 2015
  • The objective of this study is to investigate the effect of multi-hole nozzle on the performance of small CRDI engine. Combustion and exhaust emission characteristics of engine were studied by using CFD simulation with ECFM-3Z combustion model. The conditions of simulation were varied with nozzle geometry, injection timing and injection quantity. In addition, the results were compared in terms of combustion pressure, rate of heat release, $NO_x$ and soot emissions. It was found that combustion pressure was increased when injection timing was advanced. The rate of heat release of 6 hole nozzle was higher than that of 12 hole nozzle since the quantity of fuel impinged at the bottom of piston rim was different under different injection timing conditions. In the case of $NO_x$ emission, 6 hole nozzle generated more $NO_x$ emission than 12 hole nozzle. On the other hand, in the case of soot emission, 12 hole nozzle showed higher value than 6 hole nozzle because injected fuel droplets from multi-hole nozzle were coalesced.

페로브스카이트 반도체 물질에 원형 패턴을 형성하기 위한 상압플라즈마 식각 기술 (Atmospheric Pressure Plasma Etching Technology for Forming Circular Holes in Perovskite Semiconductor Materials)

  • 김무진
    • 융합정보논문지
    • /
    • 제11권2호
    • /
    • pp.10-15
    • /
    • 2021
  • 본 논문에서는 먼저 습식 코팅 방법으로 페로브스카이트 (CH3NH3PbI3) 박막을 글라스 상에 형성하고, 다양한 분석 기법을 이용하여 막의 두께, 표면거칠기, 결정성, 구성성분 및 가시광 영역에서의 이 물질의 반응에 대해 논한다. 완성된 반도체 물질은 막내부에 결함(defect)이 없고 균일하며, 표면거칠기는 매우 작으며, 가시광영역에서 높은 흡수율이 관찰되었다. 다음으로 이와 같이 형성된 유무기 층에 hole 형상을 구현하기 위하여, 구멍이 일정한 간격으로 있는 메탈마스크, 페로브스카이트 물질이 코팅되어 있는 유리, 자석 순서로 되어있는 구조의 샘플을 상압플라즈마 공법을 이용하여 시간에 따른 물질에 형성되는 hole 형태의 변화를 분석하였다. 시간이 길어짐에 따라 더 많이 식각되는 것을 알 수 있으며, 이 중에서 공정 시간을 가장 오래한 샘플에 대해서는 보다 자세하게 살펴보았고, 플라즈마의 위치에 따른 차이에 의해 7영역으로 분류할 수 있었다.

가스터빈 블레이드의 얇은 벽에서의 팬 형상 홀 최적화 (Optimization of Fan-Shaped Hole for Gas Turbine Blade on Thin Wall)

  • 현민주;박희승;김태현;송호섭;이희재;조형희
    • 한국추진공학회지
    • /
    • 제25권4호
    • /
    • pp.71-77
    • /
    • 2021
  • 가스터빈 블레이드를 고온의 주유동으로부터 보호하기 위해 다양한 냉각 기법이 연구되었고, 팬 형상 홀을 포함한 다양한 막냉각 홀 형상에 대해서도 연구가 수행되어왔다. 하지만, 소형 가스터빈에 대한 수요가 증가함에 따라 얇은 벽에 적용할 수 있는 막냉각 홀에 대한 연구가 필요하다. 이에 따라 본 연구에서는 수치해석을 통하여 분사율 1과 2에서 팬 형상 홀의 형상 변수의 영향을 연구하였다. 또한, 원형부 길이와 전방향 및 횡방향 확장각, 세 가지 변수에 대하여 최적화를 수행하였다. 각 분사율에서 최적화된 두 형상은 유사한 형상 변수와 냉각 성능을 갖는 것으로 나타났다.

PCB드릴링용 공기베어링 스핀들의 런아웃(RunOut)에 따른 가공 홀의 형상변화 (Drilled Hole Variation of Air Bearing Spindle for PCB according to RUNOUT)

  • 배명일;김상진;김형철;김기수
    • 한국정밀공학회:학술대회논문집
    • /
    • 한국정밀공학회 2005년도 춘계학술대회 논문집
    • /
    • pp.1555-1558
    • /
    • 2005
  • In this study, we measured cylindricity and Runout of the air bearing spindle, and tested PCB(printed circuit boards) drilling with 0.4mm micro drill at 90,000rpm and 110,000rpm in order to obtain drilling hole error. Results are as follows; The air bearing spindle's Runout was not so high within $10\mu{m}$ from 20,000rpm to 80,000rpm but it grew after 80,000rpm. Drilling hole size error was 9% at 80,000rpm and 12% at 110,000rpm because of spindle's Run out. Drilled hole shape falsified more 110,000rpm than 90,000rpm.

  • PDF

홴형상 막냉각홀의 신경회로망 기법을 이용한 최적설계 (Design Optimization of a Fan-Shaped Film-Cooling Hole Using a Radial Basis Neural Network Technique)

  • 이기돈;김광용
    • 한국유체기계학회 논문집
    • /
    • 제12권4호
    • /
    • pp.44-53
    • /
    • 2009
  • Numerical design optimization of a fan-shaped hole for film-cooling has been carried out to improve film-cooling effectiveness by combining a three-dimensional Reynolds-averaged Navier-Stokes analysis with the radial basis neural network method, a well known surrogate modeling technique for optimization. The injection angle of hole, lateral expansion angle of hole and ratio of length-to-diameter of the hole are chosen as design variables and spatially averaged film-cooling effectiveness is considered as an objective function which is to be maximized. Twenty training points are obtained by Latin Hypercube sampling for three design variables. Sequential quadratic programming is used to search for the optimal point from the constructed surrogate. The film-cooling effectiveness has been successfully improved by the optimization with increased value of all design variables as compared to the reference geometry.