• 제목/요약/키워드: Pressure Correction Method

검색결과 159건 처리시간 0.02초

평발교정용 형상기억합금 초탄성 인솔 설계 연구 (A Study on Design Factor of Insole using Shape Memory Alloy for Pes Planus Correction)

  • 양미경;이상욱
    • 한국산학기술학회논문지
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    • 제18권5호
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    • pp.79-85
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    • 2017
  • 발 질환으로 어려움을 겪는 환자들이 증가하면서 이에 대응할 수 있는 교정용 인솔에 대한 연구가 점점 요구되고 있다. 이에 따라 본 논문에서는 형상기억합금의 특성 중 하나인 초탄성 효과를 이용하여 평발교정용 인솔 설계에 관한 연구를 진행하였다. 신발에 인솔을 부착하는 방식을 도입하여 설치된 인솔이 발 구조 중 가장 중요한 근육인 족저근막을 자극할 수 있도록 유도하였다. 족저근막에서 인솔에 의해 유발되는 접촉압을 유한요소법으로 예측하는 방법을 통해 교정 효과를 기대할 수 있는 평발교정용 인솔을 설계하고자 하였다. 이를 위해 인솔의 형상을 결정하는 설계 인자로 세 가지 즉, 인솔의 두께, 최고높이, 앞뒤의 비대칭률을 채택하였다. 세 가지 설계 인자의 영향도를 평가하기 위해 다구찌 최적화 기법을 도입하여 각 인자 간 조합에 따른 족저근막에서의 최대 접촉압을 계산하고 이를 분석하였다. 분석 결과 접촉압을 결정하는데 영향을 많이 주는 설계인자를 순서대로 나열하면 최고높이, 두께, 비대칭률의 순으로 나타났다. 또한, 접촉압을 실제 사람이 느낄 수 있는 인지압으로 변환한 후 교정 효과를 기대할 수 있으면서도 족저근막에 무리를 주지 않는 안전 교정 범위를 설정하였다. 이를 통해 안전 교정 범위에 드는 가장 좋은 설계안을 제안하였다. 본 연구를 통해 확립한 중요인자를 고려한 설계방법은 향후 개인별 맞춤형 교정 인솔을 설계하는 기반이 될 수 있다.

비영위법에 의한 5공 프로브의 교정에 관한 연구 (A Study on the Five - hole Probe Calibration with Non-nulling Method)

  • 정양범;신영호;박호동
    • Journal of Advanced Marine Engineering and Technology
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    • 제20권2호
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    • pp.116-116
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    • 1996
  • This paper is concerned with a method for calibrating five-hole probes of both angle-tube and prismatic geometries to measure local total and static pressures and the magnitude and direction of the mean velocity vector. Descriptions of the calibration technique, the typical calibration data, and an accompanying discussion of the interpolation procedure are included. The flow properties are determined explicitly from measured probe pressures using calibration data. Flow angles are obtained within the deviation angle of 1.0 degree and dynamic pressures within 0.03 with 95% certainty. The variations in the calibration data due to Reynolds number are also discussed. For the range of Reynolds number employed, no effect was detected on the pitch, yaw and total pressure coefficients. However, the static pressure coefficient showed change to cause minor variations in the magnitude of the calculated velocity vector. To account for these variations, average correction factors need to be incorporated into the static pressure coefficient.

비영위법에 의한 5공 프로브의 교정에 관한 연구 (A Study on the Five-hole Probe Calibration with Non-nulling Method)

  • 정양범;신영호;박호동
    • Journal of Advanced Marine Engineering and Technology
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    • 제20권2호
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    • pp.48-56
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    • 1996
  • This paper is concerned with a method for calibrating five-hole probes of both angle-tube and prismatic geometries to measure local total and static pressures and the magnitude and direction of the mean velocity vector. Descriptions of the calibration technique, the typical calibration data, and an accompanying discussion of the interpolation procedure are included. The flow properties are determined explicitly from measured probe pressures using calibration data. Flow angles are obtained within the deviation angle of 1.0 degree and dynamic pressures within 0.03 with 95% certainty. The variations in the calibration data due to Reynolds number are also discussed. For the range of Reynolds number employed, no effect was detected on the pitch, yaw abd total pressure coefficients. However, the static pressure coefficient showed change to cause minor variations in the magnitude of the calculated velocity vector. To account for these variations, average correction factors need to be incorporated into the static pressure coefficient.

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배기 압력 상승률에 의한 실화 검출 (The Misfire Detection by the Exhaust Pressure Ascent Rate)

  • 김세웅;최미호;심국상
    • 한국자동차공학회논문집
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    • 제11권2호
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    • pp.1-7
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    • 2003
  • This paper proposes a method to detect misfired cylinders by the exhaust pressure ascent rate. The misfire is generated by faults of electric system or faults of fuel delivery system. It is one of the abnormal combustions. Therefore, it increases the unburned hydrocarbon and the carbon monoxide and affects a bad influence to the 3-way catalyst. The misfire causes to decrease the power of the engine and increase the consumption of the fuel. Early detection and correction of the misfired cylinders can prevent these unusual phenomena. The misfired cylinders can be detected by the comparison of exhaust pressure ascent rate during each cycle. The exhaust pressure ascent rate is defined as pressure rise per time. Our experimental results showed that the proposed method is effective in the detection of the misfired cylinders on a gasoline engine regardless loads and revolutions of the engine.

전 속도영역 유동을 위한 비정렬격자 압력기반해법 (Unstructured Pressure Based Method for All Speed Flows)

  • 최형일;이도형;맹주성
    • 대한기계학회논문집B
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    • 제26권11호
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    • pp.1521-1530
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    • 2002
  • This article proposes a pressure based method for predicting flows at all speeds. The compressible SIMPLE algorithm is extended to unstructured grid framework. Convection terms are discretized using second-order scheme with deferred correction approach. Diffusion term discretization is based on structured grid analogy that can be easily adopted to hybrid unstructured grid solver. This method also uses node centered scheme with edge based data structure for memory and computing time efficiency of arbitrary grid types. Both incompressible and compressible benchmark problems are solved using the above methodology. The demonstration of this method is extended to slip flow problem that has low Reynolds number but compressibility effect. It is shown that the proposed method can improve efficiency in memory usage and computing time without losing any accuracy.

병렬 연산을 이용한 축류 블레이드의 역설계 (The Inverse Design Technique of Axial Blade Using the Parallel Calculation)

  • 조장근;안재성;박원규
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 1999년도 유체기계 연구개발 발표회 논문집
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    • pp.200-207
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    • 1999
  • An efficient inverse design technique based on the MGM (Modified Garabedian-McFadden) method has been developed. The 2-D Navier-Stokes equations are solved for obtaining the surface pressure distributions and coupled with the MGM method to perform the inverse design. The solver is parallelized by using the domain decomposition method and the standard MPI library for communications between the processors. The MGM method is a residual-correction technique, in which the residuals are the difference between the desired and the computed pressure distribution. The developed code was applied to several airfoil shapes and the axial blade. It has been found that they are well converged to their target pressure distribution.

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수정된 방사 에너지법과 단파장 영역 보정법을 이용한 파랑 중 부가저항 추정에 관한 연구 (A Study on Estimation of Added Resistance in Waves Using Modified Radiated Energy Method and Short Wave Correction Method)

  • 오승훈;양진호
    • 대한조선학회논문집
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    • 제53권1호
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    • pp.62-68
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    • 2016
  • A simple calculation tool for added resistance in waves is developed to utilize for initial design or embedded module for navigation support system. In order to select an appropriate calculation method for added resistance in waves, three methods (drift method, integrated pressure method, radiated energy method) based on strip method are applied to Wigley I and KVLCC2. The methods for added resistance in waves give the underestimated results because it is difficult to consider nonlinear effects due to reflected wave. We apply asymptotic (Faltinsen's method) and empirical formula (NMRI's method) to improve the accuracy for short wave length region. In comparison with experimental results, the combination of radiated energy method and short wave correction method of NMRI is the most reasonable. However, a simple sum of results calculated by two methods gives rise to the overestimation of added resistance for short wave length region because added resistance of radiated energy method exits in total reflection region. To overcome this problem, modified radiated energy method is proposed using correction coefficient defined by reflection coefficient of NMRI's method. Finally, added resistance in regular waves is composed of added resistance of modified radiated energy method and that of short wave correction method of NMRI. Estimated added resistance in regular waves is validated by comparison with experimental results of other research groups.

적분방정식을 이용한 초음속 날개의 역설계법 (Inverse Design Method of Supersonic wings Using Intergral Equations)

  • 정신규;김경훈
    • 한국항공우주학회지
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    • 제31권4호
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    • pp.8-15
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    • 2003
  • 본 연구는 적분 방정식과 반복 "오차-수정" 개념을 이용하는 Takanashi의 이론에 기초한 초음속 실용적인 설계방법의 개발 결과로서, 형상의 수정량은 목표 압력분포와 설계대상의 압력분포와의 차를 경계조건으로 이용해 LSP 방정식을 풀므로써 계산되어진다. 이 연구에서는 Green의 정리를 이용하여 편미방정식 형태의 LSP 방정식을 적분방정식으로 변환하여 계산하는 방법을 이용하고 있다. 여기서는 Isolated wing과 wign-nacelles 두가지 경우의 설계를 예로 들었다.

배기계 압력 변동을 이용한 가솔린 기관의 실화 검출 -단수 실린더 실화- (Fluctuations in the Exhaust System -Single Cylinder Misfire-)

  • 심국상;복중혁;김세웅
    • 한국자동차공학회논문집
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    • 제6권6호
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    • pp.210-217
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    • 1998
  • This paper describes the method for detection of the misfired cylinder using the pressure fluctuations occurred in the exhaust system on an MPI gasoline engine. If misfire is occurred in the cylinder of the gasoline engine, the power of engine gets lost, the fuel consumption and the exhaust emission are increased and the vibration is caused by unsteady torque. Therefore early detection and correction of misfire play a very important role in the proper performance and the exhaust emission. This paper suggests method of misfire detection which affect engine performance. The method is a comparison of average pressure index during the displacement period. Experimental results showed that the method using the pressure fluctuations in the exhaust system is proven to be effective in the detection of misfire on gasoline engine regardless loads and revolutions of the engine. In addition, this method, using the pressure fluctuations in exhaust system is easier than other methods and is not a need of additional reconstruction of engine.

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Cavity Design Method for Injection-Molded Spur Gears

  • Kim, Choong-Hyun;Lee, Sung-Chul;Ahn, Hyo-Sok;Chong, Tae-Hyong
    • Journal of Mechanical Science and Technology
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    • 제14권1호
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    • pp.65-71
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    • 2000
  • Mold cavities of gears should be made larger than the product specification since plastics shrink when changing from a molten to a solid state. For injection molded spur gears, two design methods for the compensation of shrinkage are widely used. One is the module correction method and the other is the pressure angle correction method. Both methods are based on the assumption that shrinkage occurs toward the center of a molded gear. This paper deals with the shrinkage rate and proposes a method of designing gear cavity derived from the measured shrinkage rates which govern the outside diameter, the tooth depth and the tooth thickness of a molded gear. The proposed method imposes no restriction on the shrinkage direction and provides a cavity with all of the fundamental gear design parameters.

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