• 제목/요약/키워드: pin-hole

검색결과 200건 처리시간 0.023초

직교이방성 적층판의 Hole단부의 3D 비선형 층간응력 해석 (3D Non-linear Analysis of Interlaminar Stress around the Hole Edge of Orthotropic Laminates)

  • 송관형
    • 한국해양공학회지
    • /
    • 제18권5호
    • /
    • pp.36-42
    • /
    • 2004
  • Orthotropic laminates, such as [$0^{\circ}6$/$90^{\circ}6$]s and [$90^{\circ}6$/$0^{\circ}6$]s, were performed, using a commercial nonlinear finite element method. Interlaminar stress distributions, around the hole curve free-edge, were calculated. The delamination bearing strengths of pin joints were predicted, using the modified delamination failure criterion. These stress distributions were presented along the radial lines and around the free-edge of the hole. Further, three-dimensional non-linear contact analysis of orthotropic laminates was conducted to investigate the effect of friction. In this paper, laminates with a circular hole were taken to study interlaminar stresses the curved edge. This study may assist in the design of a thick composite laminate with mechanically pin joints.

원공공차를 가진 볼트 조인트와 핀 조인트의 강도평가에 관한 연구 (A Study on the strength of the Bolted Joint & Pin Joint with Hole Clearance)

  • 정강우;최진호;권진회
    • Composites Research
    • /
    • 제25권6호
    • /
    • pp.186-190
    • /
    • 2012
  • 복합재료가 기계부품 및 항공기 구조물에 폭 넓게 적용됨에 따라, 복합재료 구조물에서 가장 취약한 복합재료 체결부의 설계는 매우 중요한 연구 분야로 대두되고 있다. 본 논문에서는 다양한 원공공차를 가지는 복합재료 볼트 조인트와 핀 조인트의 강도를 상호 비교하였다. 실험결과로부터 조인트의 원공공차가 $880{\mu}m$일 때 원공공차가 $0{\mu}m$ 보다 첫 번째 파손하중의 볼트 조인트는 24.2 %, 핀 조인트는 51.3 %의 강도저하가 발생되었다. 또한, 이에 대한 유한 요소 해석을 수행하여 파손지수를 계산하고 실험값과 상호 비교하였다.

중형 디젤 엔진 크랭크축 및 오일 홀에 대한 강도평가 (Strength Evaluation for Crankshaft and its Oil Hole of Medium Speed Diesel Engine)

  • 안성찬;손정호;김병주;김종석
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2003년도 추계학술대회
    • /
    • pp.1121-1126
    • /
    • 2003
  • Strength evaluation was carried out for the fillet and oil hole of crankshaft of medium speed diesel HiMSEN engine to verify initial concept design. Alternating torque obtained from torsional vibration analysis and radial force due to firing pressure were applied. It was assumed that the maximum alternating torque and radial force occur simultaneously. Weak points in view of fatigue are proceeding fillet and crank pin fillet area and the minimum normalized fatigue safety factor is 1.17 at crank pin fillet. The fatigue strength of the oil hole was evaluated to verify the effect of the surface roughness of the oil hole. As results, the specific level of the inner surface roughness and the polishing depth of the oil hole for sufficient fatigue strength was suggested. The maximum stress value and stress distribution at the inner surface of the oil hole can be easily estimated at initial design stage by the newly developed method.

  • PDF

일방향 CFRP 복합재료의 핀 베어링강도에 관한 시험편 치수의 영향 (Effect of Specimen Geometries on the Pin Bearing Strength of Unidirectional CFRP Composites)

  • 전진탁;김재동;고성위
    • 수산해양기술연구
    • /
    • 제33권4호
    • /
    • pp.346-351
    • /
    • 1997
  • The pin bearing strength is one of the most important design parameters for mechanical joints composed of fiber reinforced composites. Thus the effect of the edge distance and the width of specimen on the pin-bearing strength of unidirectional CFRP composites were experimentally investigated in this paper. As results, the failure modes and the pin bearing strength of mechanical joints turned out to depend on the edge distance and also the width of specimen. The failure of specimen with low ratio of width to hole diameter was caused by the net tension from the hole boundary, on the other hand, the failure of specimen with low ratio of edge distance to hole diameter was caused by the shear-out. The bearing strength in case of the failure by shear-out was quite lower than that in case of failure by net tension.

  • PDF

Performance Comparison of CuPc, Tetracene, Pentacene-based Photovoltaic Cells with PIN Structures

  • Hwang, Jong-Won;Kang, Yong-Su;Park, Seong-Hui;Lee, Hye-Hyun;Jo, Young-Ran;Choe, Young-Son
    • 한국진공학회:학술대회논문집
    • /
    • 한국진공학회 2010년도 제39회 하계학술대회 초록집
    • /
    • pp.311-312
    • /
    • 2010
  • The fabricated photovoltaic cells based on PIN heterojunctions, in this study, have a structure of ITO/poly(3, 4-ethylenedioxythiophene)-poly(styrenesulfonate)(PEDOT:PSS)/donor/donor:C60(10nm)/C60(35nm)/2, 9-dimethyl-4, 7-diphenyl-1, 10-phenanthroline(8nm)/Al(100nm). The thicknesses of an active layer(donor:C60), an electron transport layer(C60), and hole/exciton blocking layer(BCP) were fixed in the organic photovoltaic cells. We investigated the performance characteristics of the PIN organic photovoltaic cells with copper phthalocyanine(CuPc), tetracene and pentacene as a hole transport layer. Discussion on the photovoltaic cells with CuPc, tetracene and pentacene as a hole transport layer is focussed on the dependency of the power conversion efficiency on the deposition rate and thickness of hole transport layer. The device performance characteristics are elucidated from open-circuit-voltage(Voc), short-circuit-current(Jsc), fill factor(FF), and power conversion efficiency($\eta$). As the deposition rate of donor is reduced, the power conversion efficiency is enhanced by increased short-circuit-current(Jsc). The CuPc-based PIN photovoltaic cell has the limited dependency of power conversion efficiency on the thickness of hole transport layer because of relatively short exciton diffusion length. The photovoltaic cell using tetracene as a hole transport layer, which has relatively long diffusion length, has low efficiency. The maximum power conversion efficiencies of CuPc, tetracene, and pentacene-based photovoltaic cells with optimized deposition rate and thickness of hole transport layer have been achieved to 1.63%, 1.33% and 2.15%, respectively. The photovoltaic cell using pentacene as a hole transport layer showed the highest efficiency because of dramatically enhanced Jsc due to long diffusion length and strong thickness dependence.

  • PDF

제트홀이 설치된 핀-휜 및 핀-휜/딤플 복합 배열을 사용한 내부유로에서의 열전달 향상 (Enhancement of Heat Transfer in Internal Passage using Pin-Fin with Jet Hole and Complex Pin-Fin-Dimple Array)

  • 박준수
    • 융복합기술연구소 논문집
    • /
    • 제5권1호
    • /
    • pp.27-31
    • /
    • 2015
  • A Pin-fin array is widely used to enhance the heat transfer in the internal cooling passage. The heat transfer distribution around the pin-fin is varied by the horseshoe vortex and flow separation. The difference of heat transfer coefficient induces the large thermal stress, which is one of the major reasons to break of hot components. So, it is required to enhance the heat transfer on the back side of pin-fin to solve the thermal stress problem. This study suggests the pin-fin with inclined jet hole and complex pin-fin/dimple array to enhance the heat transfer on the back side of pin-fin. The heat transfer coefficient is predicted by the numerical analysis, which is performed by CFX 14.0. The numerical results are obtained at Reynolds number, 10,000. The results show that the heat transfer on the back side of pin-fin is increased in both cases. Beside, the wake, which comes from dimple and jet, helps to develop the horseshoe vortex and increase the heat transfer on the next row pin-fin.

유한요소해석에 의한 플라스틱 스퍼기어의 내구성 향상방안 연구 (On a Method for the Durability Enhancement of Plastic Spur Gear Using Finite Element Analysis)

  • 김충현;안효석;정태형
    • 대한기계학회논문집A
    • /
    • 제27권2호
    • /
    • pp.223-230
    • /
    • 2003
  • Stress patterns are created in the plastic spur gear tooth body by introducing a hole or a steel pin to improve stress distribution. Static analysis using finite element method is carried out to show the effect. The result shows that maximum stress as well as tooth tip displacement is dependent on the size and location of a hole or a steel pin. When a hole located on the tooth center line, the maximum static stress level and the tooth tip deflection is always higher than that of a solid gear. But, a considerable reduction in the maximum stress and tooth tip displacement is achieved by insertion of steel pin.

브레이드 복합재료의 원공의 크기와 분포가 재료강도에 미치는 영향 (The Effect of Circulat Hole Size and Distribution on Strength of Braided Composite)

  • 이경우;강태진
    • 한국재료학회지
    • /
    • 제4권3호
    • /
    • pp.253-258
    • /
    • 1994
  • S2-유리 섬유/폴리에스터 브레이드 복합재료에서 원공의 크기 및 원공간 거리 변화가 인장성질, 핀하중 인장성질, 굽힘성질에 미치는 영향을 연구하였다. 원공의 크기에 따른 복합재료의 인장강도의 저하는 Whitney와 Nuismer에 의해 제시된 이론값과 대체로 일치함을 보여주었으며 이때의 특성길이($d_o$)는 브레이드 복합재료는 약 1.6mm, 직물 적층 복합재료는 약 1.8mm가 되었다. 브레이드 복합재료의 원공간 거리 변화에 따른 인장강도의 변화는 두 원공 중심 사이의 거리가 원공 지름의 4배 이상이면 원공간 상호작용이 없었다. 원공의 중심과 측면간 거리에 따른 인장강도의 변화는 원공의중심과 측면간 거리가 원공 지름의 3배 이상일 때 상호작용이 없었다. 핀하중 인장실험에서 브레이드 복합재료와 직물 적층 복합재료 모두 핀의 지름이 증가함에 따라 Bearing Stength는 감소하였다.

  • PDF

브라운관용 플런저 냉각표면의 온도분포 개선을 위한 연구 (A Study for Improvement of Temperature Distribution in Plunger Surface Cooling)

  • 곽경민;박지열;배철호
    • 한국정밀공학회지
    • /
    • 제25권3호
    • /
    • pp.126-133
    • /
    • 2008
  • The main objective of the present study is to achieve linear temperature distribution of cooling surface of plunger. K type thermocouples are attached at the surface of plunger to measure temperature. Nozzle and insulating material are inserted in the pin hole of the plunger for this study. Cooling water flow enters at one nozzle and leaves at three nozzles. Flow through nozzle can be activated in the pin hole, temperature of hot point around hole is decreased. Meanwhile, insulating material blocks off heat transfer, temperature of cold point around hole is increased. By combination of nozzle and insulation, heat transfer of hole is controlled effectively, as result its, temperature of plunger surface shows linear temperature distribution.

터빈 블레이드 냉각시스템에 관한 수치해석적 연구 (NUMERICAL STUDY OF TURBINE BLADE COOLING TECHNIQUES)

  • 김광용;이기돈;문미애;허만웅;김현민;김진혁
    • 한국전산유체공학회:학술대회논문집
    • /
    • 한국전산유체공학회 2010년 춘계학술대회논문집
    • /
    • pp.530-533
    • /
    • 2010
  • This paper presents numerical analysis and design optimization of various turbine blade cooling techniques with three-dimensional Reynolds-averaged Navier-Stokes(RANS) analysis. The fluid flow and heat transfer have been performed using ANSYS-CFX 11.0. A fan-shaped hole for film-cooling has been carried out to improve film-cooling effectiveness with the radial basis neural network method. 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. The impingement jet cooling has been performed to investigate heat transfer characteristic with geometry variables. Distance between jet nozzle exit and impingement plate, inclination of nozzle and aspect ratio of nozzle hole are considered as geometry variables. The area averaged Nusselt number is evaluated each geometry variables. A rotating rectangular channel with staggered array pin-fins has been investigated to increase heat transfer performance ad to decrease friction loss using KRG modeling. Two non-dimensional variables, the ratio of the eight diameter of the pin-fins and ratio of the spacing between the pin-fins to diameter of the pin-fins selected as design variables. A rotating rectangular channel with staggered dimples on opposite walls are formulated numerically to enhance heat transfer performance. The ratio of the dimple depth and dimple diameter are selected as geometry variables.

  • PDF