• 제목/요약/키워드: Hole shape

검색결과 525건 처리시간 0.025초

평판에서 타원공의 형상에 따른 피로도지수 해석 (The Analysis of Fatigue Quality Index for Shape of Elliptical Hole in Plate)

  • 송준혁;노홍길;강희용;양성모
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2003년도 춘계학술대회 논문집
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    • pp.130-136
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    • 2003
  • A FQI(fatigue quality index) analysis using the concept of SF(severity factor) is performed to various shape of elliptical hole. FQI is fatigue quality index to estimate the dynamic SF from static SF by finite element analysis. Since the SF is affected by the location of cutout in plate and radius ratio, static SF is analyzed with finite element method and forms the equation of FQI for predicting a dynamic SF. To examine the validity, dynamic SF is measured by photoelastics and thermalelastics for an epoxy resin plate with various elliptical holes under dynamic load.

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결함이 있는 점집합 곡면의 형상 및 외관 수정 (Shape and Appearance Repair for Incomplete Point Surfaces)

  • 박세연;;신하용
    • 한국CDE학회논문집
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    • 제12권5호
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    • pp.330-343
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    • 2007
  • In this paper, we present a new surface content completion system that can effectively repair both shape and appearance from scanned, incomplete point set inputs. First, geometric holes can be robustly identified from noisy and defective data sets without the need for any normal or orientation information. The geometry and texture information of the holes can then be determined either automatically from the models' context, or manually from users' selection. After identifying the patch that most resembles each hole region, the geometry and texture information can be completed by warping the candidate region and gluing it onto the hole area. The displacement vector field for the exact alignment process is computed by solving a Poisson equation with boundary conditions. Out experiments show that the unified framework, founded upon the techniques of deformable models and PDE modeling, can provide a robust and elegant solution for content completion of defective, complex point surfaces.

크리깅 기법을 이용한 원통형 막냉각 홀의 최적설계 (Shape Optimization of Cylindrical Film-Cooling Hole Using Kriging Method)

  • 이기돈;김광용
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회B
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    • pp.2729-2732
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    • 2008
  • Cylindrical film-cooling hole is formulated numerically and optimized to enhance film-cooling effectiveness. The Kriging method is used an optimization technique with Reynolds-averaged Navier-Stokes analysis of fluid and heat transfer with shear stress transport model. The hole length-to-diameter ratio and injection angle are chosen as design variables and spatially averaged film-cooling effectiveness is considered as objective function which is to be maximized. Twelve training points obtained by Latin Hypercube Sampling for two design variables. Optimum shape shows the film-cooling effectiveness increased.

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알루미늄 사형주조에서 기공 결함 감소를 위한 연구 (A study on the reduction of blow hole defects in aluminum sand casting)

  • 이동연;이춘규
    • Design & Manufacturing
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    • 제14권4호
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    • pp.52-57
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    • 2020
  • In this study attempted to prevent defects due to blow holes among defects of sand casting products. It was intended to reduce the defect rate by reducing the blow hole of the inner surface. Currently, expectations and requirements for the quality level of non-ferrous aluminum casting in the casting industry are increasing. In addition, the shape is complex and the shrinkage precision is required. Among them, the test prototype is expensive to manufacture the mold, and the production time is also long, and the product is manufactured by sand casting. At this time, the highest defect rates are defects caused by shrinkage defects, surface defects, and blow holes.. At this study, the manufacturing time was shortened by using the shape of the fluid movement path in advance. Also, it is possible to reduce defects due to blow holes.

플라즈마 용사된 세라믹 코팅층의 레이저 홈가공 (Laser Engraving of Plasma Sprayed Ceramic Coatings)

  • 방세윤
    • 한국정밀공학회지
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    • 제14권1호
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    • pp.142-149
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    • 1997
  • Ceramic-coated anilox roll for printing is resistant to corrosion and wear, and hence has enhanced life and quality. Laser engraving is used typically for machining holes to store ink in this roll. Since engraved hole size and shape are directly related to laser processing parameters, it is necessary to know the rela- tionships among these parameters. In this study, the parameters for engraving of ;oasma sprayed ceramic coatings with Nd:YAG laser were studied. Relationships between hole shape and processing parameters were analyzed. Cr$_{2}$O$_{3}$ceramic was found to be most suitable for Nd:YAG laser engraving. It was found that hole depth can be increased by using higher energy pulses. Effect of using different assistant gases was small to the final results. For better results, it was suggested to use a very stable laser with shorter pulses and higher pulse energy.

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U-groove가 있는 평판재 끝 Hole의 안정성 문제 (A Study on the Hole Stability in the U-Grooved Plates)

  • 김시영
    • 수산해양기술연구
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    • 제19권1호
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    • pp.51-56
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    • 1983
  • 경계요소법에 의하여 U자형 홈(groove)을 가진 평판이 측면 분포하중을 받을 때 끝부에 위치할 원형 Hole의 최적 위치의 해석을 행하고 동일한 모델(model)에 대하여 실험결과를 비교하여 다음과 같은 결론을 얻게 되었다. 1. 원형 Hole이 U자형 홈(groove)에 가까이 접근하게 됨에 따라 초기의 원형 Hole은 c.-c.선에 수직방향이 그 장축이 되는 타원형으로 변화됨을 알 수 있다. 2. 원형 Hole이 U-groove에 접근함에 따라 Hole 과 Groove 사이의 Neck부는 그 횡단면응력이 인장 및 압축이 동시에 존재하다가 점점 전체가 인장역이 됨을 알 수 있다. 3. 원형 Hole이 Groove에 접근함에 따라 판재경계와 Hole 사이의 목(neck)부분은 계속적인 압축상태를 유지한다. 4. U-groove쪽의 Neck area의 응력분포는 그 최대응력치가 Hole로 접근함에 따라 가속적으로 증가하고 Hole의 찌그러짐(distortion)의 방지를 위한 Hole의 최적중심의 위치는 Neck부의 Hole 측면의 압축응력치가 0이 되지 않는 범위가 한계임을 알 수 있다.

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항공재료 리벳홀에 인접한 원공결함의 위치에 따른 응력집중계수의 변화와 균열발생거동 (The Variation of Stress Concentration Factor and Crack Initiation Behavior on the Hole Defects Around the Rivet Hole in a Aircraft Materials)

  • 송삼홍;김철웅;김태수;황진우
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 춘계학술대회
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    • pp.381-388
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    • 2003
  • The material deficiencies in the form of pre-existing defects can initiated cracks and fractures. The stress distribution and fatigue crack initiation life of engineering materials may be associated with the size, the shape and the relative location of defects contained in the component. The objective of this study is to investigate the effect of arbitrarily located hole defect around the rivet hole of a wing section in monolithic aluminum and Al/GFRP laminates under cyclic bending moment during a service load. The stress distribution and the fatigue crack initiation behavior near a rivet hole of on the relationships between stress concentration factor ($K_t$) and relative position of defects were considered. The test results indicated the features of different stress field. Therefore, the stress concentration factor ($K_t$) and the fatigue crack initiation behavior was illustrated different behavior according to each position of hole defect around the rivet hole in monolithic aluminum and Al/GFRP laminates.

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AJM을 이용한 HDM에 의한 잔류응력 계측에 관한 연구 1

  • 이택순
    • Journal of Welding and Joining
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    • 제6권3호
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    • pp.37-42
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    • 1988
  • The Hole Drilling Method(HDM) is widely used to measure residual stresses in the welded structures. The purpose of this study is to evaluate the accuracy fo measuring residual stresses when drilling the hole by Air-abrasive Jet machine(AJM). Simulated residual stresses wre introduced by applying known stresses to steel bars. These known streses were then compared with measured stresses relaxed from hole drilling. the obtained results are summarized as follows; 1) It was possible to obtain well defined holes with the nozzle designed for this study. 2) If the hole shape is not cylindrical, critical may occur. 3) In the uniaxial strain field, the measurement error of the maximum principal stress was within .+-.10 percent. The orientation angle of the maximum principal stress was within 8.deg. from the given directioin. 4) meausrements were made varying hole depths. Little or no change of stresses occurs since holse were drilled more than the depth of the 0.6 times diameter. 5) The air-abrasive jet machining for drilling holse does not cause appreciable apparent stresses which si critical to measure residual stresses.

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INVESTIGATION OF THE CNS HOLE SHAPE AND A PROPOSED INSTALLATION METHOD FOR A VACUUM CHAMBER FOR THE HANARO REACTOR

  • Cho Yeong-Garp;Kim Young-Ki;Lee Kye-Hong;Choung Yun-Hang
    • Nuclear Engineering and Technology
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    • 제38권5호
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    • pp.455-458
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    • 2006
  • The HANARO reactor has a vertical hole for a cold neutron source (CNS) in the heavy-water reflector tank, i.e., the CNS hole, which was considerably deformed during its welding to the horizontal cold neutron (CN) beam tube. This paper presents an investigation of the form of the CNS hole for the optimal design of the a vacuum chamber for the CNS. In addition, the installation method of the vacuum chamber into the CNS hole for minimizing the water thickness between the vacuum chamber and the nose of the CN beam tube is proposed.

고강도 열연판재의 홀 플랜정시 파단특성연구 (Fracture Analysis of Hole Flanging Process for High Strength Steel Sheets)

  • 김정운;김봉준;문영훈
    • 소성∙가공
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    • 제10권6호
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    • pp.465-470
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    • 2001
  • Hole flanging experiments are performed on flat circular plates with a hole in the center and the flangeability and fracture behaviors of TRIP steels and ferrite-Bainite duplex steels were examined. In the hole flanging, deformation by lip and petalling occurs when plates are struck by punches of various shapes and high circumferential strains induced in the target material cause radial cracking and the subsequent rotation of the affected plate material in a number of symmetric petals. In all cases, failure of the plate was due to lip fracture that results from multiple localized neckings that take place around the hole periphery where straining is most severe and a somewhat regular pattern was observed in a fracture shape. The neck characteristics in flange formation and the transition from the lip to petal mode at which fracture occurs were compared with two materials.

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