• 제목/요약/키워드: 2-D shape

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소프트 로봇용 4D 프린팅 소재 (4D Printing Materials for Soft Robots)

  • 이선희
    • 한국의류산업학회지
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    • 제24권6호
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    • pp.667-685
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    • 2022
  • 본 원고는 소프트 로봇용 4D 프린팅 소재와 어그제틱 구조체에 대한 연구 동향을 정리한 것이다. 먼저 4D 프린팅 소재의 형상 변화 거동을 형상 변화와 형상기억 소재, 이중, 삼중, 다중 형상기억 효과, 접힘과 굽힘, 표면지형별로 구분하여 알아보았다. 형상 변화와 형상기억 소재 등 열이나 수분의 자극에 가역적/비가역적 혹은 규칙적/불규칙적 형상 변형이 가능할 수 있다. 다음으로, 차원별 형상이동 유형에 따른 특성과 물성에 대해 알아본 바, 1차원에서 다차원으로의 형상이동을 1D-1D 팽창/수축, 1D-2D 접힘/굽힘, 1D-3D 접힘 (1D-to-3D folding)으로 구분할 수 있다. 2차원에서 형상이동은 2D-2D 굽힙, 2D3D 굽힘/접힘/꼬임/표면말림/표면지형변화/굽힘과 꼬임, 3차원에서 다차원으로의 형상이동은 3D-3D 굽힙과 3D-3D 선형/비선형 거동으로 구분할 수 있다. 마지막으로 4D 프린팅 메타구조체 중 힌지 구조체를 적용한 KinetiX는 단일단위 터셀레이션과 다중단위 터셀레이션으로 모델링할 수 있고, 평면 및 공간 변환이 용이하고, 컨포머블 헬멧에 적용할 수 있다. 키리가미 구조체를 기본으로 한 공압형 어그제틱 구조체는 역설계 기반 구조체로써 굽힘각도를 제어하는 알고리즘으로 설계할 수 있다. 설계 후 3D 프린팅하여 TPU 멤브레인으로 프로토 타입을 제조하였고, 압력을 낮추면서 원하는 3차원 형상으로 완성될 수 있음을 확인하였다. 온도나 습도 등의 외부자극요소에 따라 형상이나 물성을 변화할 수 있는 재료를 사용하여 변형가능한 3차원 구조체로 성형한 4D 프린팅 소재를 이용하여 상지, 하지, 손, 발 등 소프트 로봇의 외골격(exoskeleton) 소재에 적용할 수 있을 것이다. 즉 자세제어, 상황인식, 동작신호 생성 등 다양한 환경에 대응하여 착용자의 움직임에 고하중, 고기동성, 운동지속성을 지원하는 기능을 갖는 소프트 로봇용 4D 프린팅 소재는 헬스케어 웨어러블 의류 제품화 개발로의 용도 전개가 가능할 것이다. 특히 4D 프린팅 소프트 소재 및 공정개발 분야는 일상 생할 보조용이나 재활치료용 의류를 개발하기 위한 3D 프린팅 소재 및 공정의 원천 기술에 해당하므로 이와 관련한 연구의 기초 자료로서 활용되기를 기대한다.

컴퓨터 시뮬레이션을 이용한 임플란트 상부 티타늄 구조물의 주조방안 (CONFUTER-AIDED CASTING DESIGN FOR IMPLANT TITANIUM SUPERSTRUCTURES)

  • 오세욱;이호용;이근우;심준성
    • 대한치과보철학회지
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    • 제41권4호
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    • pp.421-439
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    • 2003
  • Statement of problem : It is difficult to obtain a good titanium casting body using the traditional sprue design because of high melting point of Ti, and the low fluidity and high reactivity of molten Ti. Purpose : A new sprue design for titanium casting bodies needs more trial and error. In order to decrease the number of trial and error, computer simulation(MAGMASOFT, Magmasoft Giessereitechnologie GmbH, Achen, Germany) was used to optimize sprue design in U-shaped implant superstructures. Material and method : Five kinds of sprue were examined for the design of the sprue former for titanium casting: Sprue design A(sprue length 4 mm, rectangular shape, 4 sprues), Sprue design B(sprue length 4 mm. round shape. radius 2 mm, 7 sprues), Sprue design C (sprue length 2 mm, round shape, radius 2 mm, 7 sprues). Sprue design D (sprue length 2 mm, cone shape, large radius 3mm. small radius 2mm, 7 sprues), and Sprue design E( sprue length 2 mm. one unit channel shape). Sprue design F(sprue length 2mm, one unit channel shape) was also examined for the design of the customized sprue former in the Biotan system(Schutz Dental Gmbh, Germany). The casting bodies were taken in Sprue design A, Sprue design D, Sprue design E, and Sprue design F in the Biotan casting system. The numerically predicted defects were compared with the experimental dental castings by the radiographic and sectional view observations. Results : 1. According to the result of computer simulation, turbulence during mold filling was decreased in the sequence of Sprue design F, Sprue design E, Sprue design D, Sprue design C, Sprue design B, and Sprue design A. 2. The calculated solidification time contours indicate that hot spot was moved from the casting body to the sprue button in the sequence of Sprue design A, Sprue design B, Sprue design C, Sprue design D, and Sprue design E. The filling pattern of Sprue design F was similar to that of Sprue design E. 3 The predicted filling pattern shows that less turbulence was found in the customized sprue former than in the standard sprue former. 4. According to the results of the radiographic and cross sectional observations, casting defects less than 1mm were found at the center of a casting body with Sprue design E and Sprue design F. However, larger casting defects of 4mm were found in a casting with Sprue design A. 5. The predicted casting porosity was similar to that of the real casting. Conclusion : One unit channel-type and customized sprue former can be recommended. Further research and developement of various sprue designs using computer simulation in necessary to optimize casting design, in order to reduce the formation of casting defects in implant titanuim super-structures.

3차원 인체모델을 이용한 엉덩이의 형태적 특징과 패턴과의 관계 (Relationship between Hip Shape and Pattern Using 3D Body Model)

  • 조영숙
    • 한국의류학회지
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    • 제33권2호
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    • pp.266-275
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    • 2009
  • Variations of individual hip shapes are a major obstacle in pattern making for fitness. The drafting method is used for pattern making in today's apparel industry. Whilst catering to a limited number of information such as waist and hip sizes, this method does not cater to variations in hip shape. This paper describes the analysis of hip shapes using 3D body model and tries to make sure the relationship between hip shape and pattern by calculating hip angle and dart amount. We achieved results in analyzing various hip shapes by extracting hip angle. Moreover, various hip shapes can be divided into three types(A, B and C) by the hip angle value($K_{sh}-K_{wsh}$). When we use computerized draping method to make a personalized pattern for a tigth skirt, we easily create complex dart lines automatically. Therefore we achieve the result of individual dart amount such as distance between dart lines and dart areas. C type of hip shape had short dart length, long distance between dart lines and a large amount of dart area. On the other hand, A type had long dart length, short distance between dart lines and small amount of dart area. B type had long length and long distance between dart lines and large amount of dart area. In traditional pattern making, distance between dart lines is usually proportional to amount of dart area because of similarity in dart line shape. In our pattern, there is no proportional relationship between dart line distance and dart area. This means that variations in hip shapes result in a wide variety of dart line curvature resulting in a wide range of dart area. By ensuring an accurate relationship between hip shape and pattern, it is possible to make patterns which result in clothing that not only fits well, but also exhibits other desirable properties.

3D 동체 모형을 이용한 2D 전개 패턴 연구 (2D Flat Pattern Development Using Simplified 3D Torso Model)

  • 김명수;홍경희
    • 대한인간공학회지
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    • 제24권2호
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    • pp.85-91
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    • 2005
  • To understand the basic relationship between 3D curved surface model and 2D pattern, simplified torso model was generated by commercial CAD program (IDEAS). 3D torso model was then divided into different blocks and unfolded into a flat pattern as in ordinary works of clothing item design. As results, 2D pattern development of different part of 3D torso model was attempted and analyzed mathematically. It was found that different height, radius and tangent slope of 3D blocks resulted in different 2D pattern. The relationships between the shape parameters of 3D torso blocks and those of 2D patterns were analyzed using regression equations. Direct way of drawing a 2D pattern of corresponding 3D torso block was also illustrated for the convenience of pattern making using conventional measurements of upper/ lower radii and height of 3D torso block.

단조공정에서 민감도법을 이용한 예비 성형체 설계 (Preform Design for Forging by the Sensitivity Method)

  • 심현보;노현철;손기찬
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2001년도 춘계학술대회 논문집
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    • pp.180-185
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    • 2001
  • The sensitivity method has been applied to find perform shape that results in the desired shape after forging. As a 2D example, initial shape of specimen for the cylinder shape without barrelling after forging has been found. The method is then applied to various shapes of 3D free forging and initial shapes of the corresponding specimens after forging have been found successfully. The sensitivity method is proven to be an effective and accurate tool for the preform design.

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유전 알고리즘을 이용한 공력 형상 최적화 연구 (Study of Aerodynamic Design Optimization Using Genetic Algorithm)

  • 김수환;권장혁
    • 한국전산유체공학회지
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    • 제6권3호
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    • pp.10-18
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    • 2001
  • Genetic Algorithm(GA) is applied to aerodynamic shape optimization and demonstrated its merits in global searching ability and the independency of differentiability. However, applications of GA are limited due to slow convergence rate, premature termination, and high computing costs. The present aerodynamic designs such as wing shape optimizations using GA have seldom been applied because of high computing costs. This paper has two objects; improvement of the efficiency of GA and application of GA into aerodynamic shape optimization for 2D and 3D wings. The study indicates that GA can be applied to aerodynamic design and its performance is comparable to traditional design methods.

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형상기억합금을 이용한 지능형 고분자 복합재료의 설계 (Design of an Intelligent Polymer-Matrix-Composite Using Shape Memory Alloy)

  • 정태헌
    • 대한기계학회논문집A
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    • 제21권10호
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    • pp.1609-1618
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    • 1997
  • Thermo-mechanical behaviors of polymer matrix composite(PMC) with continuous TiNi fiber are studied using theoretical analysis with 1-D analytical model and numerical analysis with 2-D multi-fiber finite element(FE) model. It is found that both compressive stress in matrix and tensile stress in TiNi fiber are the source of strengthening mechanisms and thermo-mechanical coupling. Thermal expansion of continuous TiNi fiber reinforced PMC has been compared with various mechanical behaviors as a function of fiber volume fraction, degree of pre-strain and modulus ratio between TiNi fiber and polymer matrix. Based on the concept of so-called shape memory composite(SMC) with a permanent shape memory effect, the critical modulus ratio is determined to obtain a smart composite with no or minimum thermal deformation. The critical modulus ratio should be a major factor for design and manufacturing of SMC.

근거리 환경에서의 3차원 배열센서 형상 보정 기법 (3-Dimensional Sensor Array Shape Calibration in Near Field Environment)

  • 류창수;어수해;강현구;유상욱
    • 한국산업융합학회 논문집
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    • 제6권4호
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    • pp.361-366
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    • 2003
  • Most sensor array signal processing methods for multiple source localization require knowledge of the correct shape of array(the correct positions of sensors that consist array), because sensor position uncertainty can severely degrade the performance of array signal processing. In particular, it is assumed that the correct positions of the sensors are known, but the known positions may not represent the true sensor positions. Various algorithms have been proposed for 2-D sensor array shape calibration in far field environment. However, they are not available in near field. In this paper, 3-D sensor array shape calibration algorithm is proposed, which is available in near field.

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극간절연회복성능 향상을 위한 초고압GCB의 노즐형상설계 (Design of Nozzle Shape for UHV GCB to Improve the Dielectric Recovery Characteristics between Electrodes)

  • 송기동;박경엽;신영준;권기영;송원표
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1995년도 추계학술대회 논문집 학회본부
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    • pp.479-481
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    • 1995
  • This paper presents a method witch tan improve the dielectric recovery characteristics of UHV class gas circuit breakers by changing the nozzle shape. To calculate the dielectric recovery voltage between electrodes, the flow field and electric field analysis in a 362kV model interrupter has been performed with the commercial programs, RAMPANT and FLUX2D, respectively. As a result, we found that the nozzle shape affects the characteristics of dielectric recovery between electrodes and obtained great improvement of it by the changing the downstream nozzle shape.

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고차 형상함수를 이용한 가스 미케니컬 페이스 시일의 윤활해석 (A Lubrication Analysis of Gas Mechanical Face Seals using a High-Order Shape Function)

  • 이안성;양재훈;최동훈
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 2001년도 제34회 추계학술대회 개최
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    • pp.204-211
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    • 2001
  • For the treatment of high compressibility number in the Reynolds equation, a new class of exponential high-order shape functions has been recently introduced in the literatures. In this paper a FE lubrication analysis method of high speed gas mechanical face seals is developed, implementing these shape functions. Their validity and usefulness are presented using 1-D gas bearing models. And a validation of developed 2-D analysis code is shown with a gas flat and spiral groove face seal models.

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