• 제목/요약/키워드: Circular Hole

검색결과 296건 처리시간 0.023초

원심분리기용 스크류의 블레이드 및 원공형상변화에 따른 응력 및 진동해석 (Stress and Vibration Analysis with respect to the change of the Shape of Screw Blade and the Hole for Centrifuge)

  • 한근조;이성욱;심재준;한동섭;안찬우;서용권;김태형
    • 한국정밀공학회지
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    • 제20권9호
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    • pp.118-125
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    • 2003
  • In this study, we carried out the finite element analysis for the screw of centrifuge that is the weakest part of the centrifuge for sewage management. Centrifugal force caused by rotation with velocity of 4000rpm was applied at the screw. Structural analysis was done with respect to the change of the ratio of blade pitch($R_P$), shaft diameter($R_D$) and extended hole($R_E$). When the area of circular hole is equal to that of extended holes, maximum equivalent stresses in the screw with circular and extended circular hole were compared. And then natural frequency analysis was executed for the same model. Three mode shapes were used to explain the vibration characteristics of each screw. Convergence study was accomplished fur more accurate results.

Stress analysis of an infinite rectangular plate perforated by two unequal circular holes under bi-axial uniform stresses

  • Yang, Yeong-Bin;Kang, Jae-Hoon
    • Structural Engineering and Mechanics
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    • 제61권6호
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    • pp.747-754
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    • 2017
  • Exact solutions for stresses for an infinite rectangular plate perforated by two circular holes of different radii subjected to uni-axial or bi-axial uniform loads are investigated using the Airy stress function. The hoop stresses occurring at the edge of the circular hole are computed and plotted. Comparisons are made for the stress concentration factors for several types of loading conditions.

화포에 의해 손상된 날개의 공력특성에 관한 연구 (A Study on the Aerodynamic Characteristic of Gunfire Damaged Airfoil)

  • 이기영;정형석;김시태
    • 한국군사과학기술학회지
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    • 제11권2호
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    • pp.144-151
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    • 2008
  • An experimental study has been conducted to investigate the effects of circular damage hole on the characteristics of airfoil performance. The damage on a wing created from a hit by anti-air artillery was modeled as a circular hole. Force balance measurements and static pressure measurements on the wing surface were carried out for the cases of having damage holes of 10% chord size at quarter chord and/or half chord positions. All experiments were conducted at Reynolds number of $2.85\times10^5$ based on the chord length. The surface pressure data show big pressure alterations near the circular damage holes. This abnormal surface pressure distribution produces shear stress that could lead to the acceleration of the structural degradation of the wing around the circular damage hole. However, in spite of the existence of circular damage holes, the measured force data indicated the only a slight decrease in lift accompanied by increase in drag compared to the results of undamaged one. The influence of damage hole on the aerodynamic performance was increased as the location of damage moved to the leading edge. The effect on the control force was insignificant when the damaged size was not large.

독립좌표연성법을 이용한 여러 개의 원형 구멍을 갖는 직사각형 평판의 자유진동해석 (Free Vibration Analysis of Rectangular Plate with Multiple Circular Cutouts by Independent Coordinate Coupling Method)

  • 곽문규;송명호
    • 한국소음진동공학회논문집
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    • 제17권11호
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    • pp.1086-1092
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    • 2007
  • This paper is concerned with the vibration analysis of a rectangular plate with multiple circular holes. On the contrary to the case of rectangular plate with multiple rectangular holes, it is very difficult to perform qualitative analysis on natural vibration characteristics because of geometrical inconsistency. In this paper, we applied the Independent Coordinate Coupling Method(ICCM) to the addressed problem, which was developed to compute natural vibration characteristics of the rectangular plate with a circular hole and proven to be computationally effective. The ICCM is based on Rayleigh-Ritz method but utilizes independent coordinates for each hole domain. By matching the deflection conditions for each hole imposed on the expressions, we can easily derive the reduced mass and stiffness matrices. The resulting equation is then used for the calculation of the eigenvalue problem. The numerical results show the efficacy of the Independent Coordinate Coupling Method.

핀이 부착된 금속곡관 제품의 열간압출 굽힘가공에 관한 연구 (A Study on the Bending Process for the Circular Curved Tube and Rectangular Curved Tube with Fins)

  • 김민규;박중원;진인태
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2001년도 추계학술대회 논문집
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    • pp.204-207
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    • 2001
  • The bending process for the circular curved tube and rectangular curved tube with fins can be developed by the hot metal extrusion machine with the multiple punches moving in the different velocity. The bending phenomenon can be controlled by the two variables. The one of them is the difference of velocity at the die exit section by the different velocity of billets through the multi-hole container. The other is the one by the different hole diameter. The results of the experiment show that the circular curved tube with fins and rectangular curved tube with pins can be formed by the extrusion process and that the curveture of the product can be controlled by the velocity of punch and diameter of container hole and that the defects such as the distortion of section and the thickness change of the wall of tube the folding and wrinkling of thin tube and fins did not happen after the bending processing by the extrusion bending machine.

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고강도 열연재의 Hole Flanging시 성형특성과 파단에 관한 연구 (Hole Flangeability and Fracture Behaviors of Circular Flanges of High Strength Hot Rolled Steels)

  • 김정운;공성락;김봉준;문영훈
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2000년도 추계학술대회 논문집
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    • pp.49-52
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    • 2000
  • The hole flanging experiments are performed on a flat circular plates with a hole in the center and the flangeability and fracture behavior of TRIP steel and ferrite-bainite duplex steel were examined. Over the ranges of conditions investigated, the flangeability of ferrite-bainite duplex steel is better than TRIP steel and the term 'hole flanging capacity' introduced in this study. Fracture behavior of TRIP steel and ferrite-bainite duplex steel was characterized by petal formation at the edge of flange. In case of crack propagation, crack tip diversion that is supposed to be responsible for flangeability occurs more severely on HSLA Steel.

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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
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    • 한국정밀공학회 2002년도 추계학술대회 논문집
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    • pp.796-799
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    • 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.

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원공을 가진 Glass/Epoxy 복합재료의 노치강도 및 파괴조건 (Notched Strength and Fracture Criterion of Glass/Epoxy Plain Woven Composites Containing Circular Holes)

  • 김정규;김도식
    • 대한기계학회논문집
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    • 제16권7호
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    • pp.1285-1293
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    • 1992
  • 본 연구에서는 glass/epoxy 직조된 복합재료에 있어서 원공 및 판폭의 크기가 노치강도에 미치는 영향을 명확히 하고, 또한 노치강도 및 파괴조건과 위에서 언급한 특성길이와의 관계를 검토하였다.

안내관 제트유동 억제시의 하나로 원형 조사공의 냉각특성 (The Cooling Characteristics for Circular Irradiation Hole under Suppressing Jet Flow at Guide Tube in HANARO)

  • 우상익;박용철
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2004년도 춘계 학술대회논문집
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    • pp.208-213
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    • 2004
  • The HANARO, multi-purpose research reactor, 30 MWth open-tank-in- pool type, is under normal operation since it reached the initial critical in February 1995. The HANARO is planning to produce a fission moly-99 of radio isotopes, a mother nuclide of Tc-99m, a medical isotope and is under developing a target handling tool for loading and unloading it in a circular flow tube (OR-5). A guide tube is extended from the reactor core to the top of the reactor chimney for easily un/loading a target under the reactor normal operation. But active coolant through the core can be quickly raised up to the top of the chimney through the guide tube by jet flow. This paper is described an analytical analysis to calculate the hole size of a orifice inserted in the circular irradiation hole and to study the flow characteristics through the guide tube under reactor normal operation and loading the target. As results, the results show that the hole size of orifice was 31 mm of the inner diameter to suppress the guide tube jet flow and the coolant safely cooled the target of fission moly after inserting the orifice to the flow tube.

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사각형 및 원형 출구 Synthetic Jet의 유동 특성에 대한 수치적 연구 (Numerical Study on Flow Characteristics of Synthetic Jet with Rectangular and Circular Slot Exit)

  • 김민희;김우례;김종암;정경진
    • 한국항공우주학회지
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    • 제39권7호
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    • pp.585-595
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    • 2011
  • 사각형 및 원형 출구 형상 synthetic jet의 수치적 연구를 통하여 유입류가 존재할 경우 평판에서의 유동 구조 및 유동 제어 효과를 분석하였다. 사각형 출구 형상의 경우, jet 직후에 강한 vortex가 생성되지만 주변에 적은 momentum을 공급하기 때문에 유입류 방향으로 갈수록 유동제어 효과가 감소하게 된다. 원형 출구 형상의 경우, 규칙적인 vortex의 형태가 slot 중앙부터 끝까지 나타나고 보다 멀리까지 jet vorticity의 영향이 미치게 된다. 유동제어 효과를 예상하기 위하여 위치 별 wall shear stress를 비교하였다. 이에 원형 출구 형상이 사각형 출구 형상보다 유동제어 효과가 더 클 것으로 판단된다. 또한 최적의 원형 출구 형상을 도출하기 위하여, hole gap과 diameter의 변화에 따른 유동 구조 및 유동 제어 효과를 비교 분석하였다. 그 결과, hole diameter와 gap를 고려하여 원형 출구 형상을 설계할 경우 유동제어 효과를 극대화 할 수 있음을 밝혔다.