• 제목/요약/키워드: optimal shapes

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Shape Optimization of Damaged Columns Subjected to Conservative and Non-Conservative Forces

  • Jatav, S.K.;Datta, P.K.
    • International Journal of Aeronautical and Space Sciences
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    • 제15권1호
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    • pp.20-31
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    • 2014
  • This paper deals with the development of a realistic shape optimization of damaged columns that are subjected to conservative and non-conservative forces, using the Genetic Algorithm (GA). The analysis is based on the design of the most optimized shape of the column under the constraint of constant weight, considering the Static, Vibrational, and Flutter characteristics. Under the action of conservative and non-conservative longitudinal forces, an elastic column loses its stability. A numerical analysis based on FEM has been performed on a uniform damaged column, to compute the fundamental buckling load, vibration frequency, and flutter load, under various end restraints. An optimization search based on the Genetic Algorithm is then executed, to find the optimal shape design of the column. The optimized column references the one having the highest buckling load, highest vibration frequency, and highest flutter load, among all the possible shapes of the column, for a given volume. A comparison is then made between the values obtained for the optimized damaged column, and those obtained for the optimized undamaged column. The comparison reveals that the incorporation of damage in the column alters its optimal shape to only a certain extent. Also, the critical load and frequency values for the optimized damaged column are comparatively low, compared with those obtained for the optimized undamaged column. However, these results hold true only for moderate-intensity damage cases. For high intensity damage, the optimal shape may not remain the same, and may vary, according to the severity of damage.

태양광 무인기 복합재 윙 리브 최적 제작 연구 (Optimal Manufacturing of Composite Wing Ribs in Solar-Powered UAVs: A Study)

  • 양용만;김명준;김진성;이수용
    • 항공우주시스템공학회지
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    • 제10권4호
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    • pp.50-58
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    • 2016
  • 선행 연구 개발을 통하여 장기 체공 태양광 무인기 복합재 날개의 경량화는 매우 중요한 요소임을 확인하였다. 날개 외피의 좌굴 방지와 비틀림 방지 역할을 하는 구조물인 리브는 날개의 구성 요소 중에 필수적이다. 본 연구는 최적의 복합재 리브를 설계, 제작하기 위하여 복합소재의 이방성 특성을 고려한 다양한 적층 패턴 적용 및 형상에 대하여 리브를 제작하였고. MSC. Patran/Nastran을 이용한 유한요소 해석을 통하여 최대 하중 및 변위 형상을 확인하였으며, 구조 시험을 통하여 측정된 시험 결과를 바탕으로 최적의 리브를 제시하였다.

미세스탬핑 공정에서 블랭크 형상의 영향에 관한 연구 (A Study on the Effect of Blank Shape on the Miniature Stamping)

  • 심현보
    • 소성∙가공
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    • 제15권4호
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    • pp.304-310
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    • 2006
  • Due to a recent growth of the area of MEMS and a trend moving toward smaller scale, a micro manufacturing that is usually related with lithography is now emerging. Differently from traditional manufacturing processes, the micro or miniature manufacturing usually requires expensive sophisticated equipments and its characteristics are of high cost and of low productivity. However, a miniature stamping, which makes small sized product with a thin metal usually in the range of meso-scale, can be realized in a low cost and in a high productivity with relatively inexpensive equipments. For a successful development of miniature stamping, lots of obstacles, including material properties related with formability, have to be overcome. Since the thin metal shows distinctive characteristics, e.g., size effect and statistically scattered material properties, the formability of miniature stamping is not good in general and the possible shape with the miniature stamping is limited relatively simple shapes. Since the optimal blank improves formability and the improved formability can make up for problems of material properties, the possibility of success can be increased. This study is carried out to show the possibility of miniature stamping and to verify the effect of optimal blank for the miniature stamping.

Catastrophe analysis of active-passive mechanisms for shallow tunnels with settlement

  • Yang, X.L.;Wang, H.Y.
    • Geomechanics and Engineering
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    • 제15권1호
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    • pp.621-630
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    • 2018
  • In the note a comprehensive and optimal passive-active mode for describing the limit failure of circular shallow tunnel with settlement is put forward to predict the catastrophic stability during the geotechnical construction. Since the surrounding soil mass around tunnel roof is not homogeneous, with tools of variation calculus, several different curve functions which depict several failure shapes in different soil layers are obtained using virtual work formulae. By making reference to the simple-form of Power-law failure criteria based on numerous experiments, a numerical procedure with consideration of combination of upper bound theorem and stochastic medium theory is applied to the optimal analysis of shallow-buried tunnel failure. With help of functional catastrophe theory, this work presented a more accurate and optimal failure profile compared with previous work. Lastly the note discusses different effects of parameters in new yield rule and soil mechanical coefficients on failure mechanisms. The scope of failure block becomes smaller with increase of the parameter A and the range of failure soil mass tends to decrease with decrease of unit weight of the soil and tunnel radius, which verifies the geomechanics and practical case in engineering.

복합소재 교량용 방호울타리의 최적 적층 단면 도출을 위한 낙하 충돌시험 (The Fall Impact test for Extraction of Optimal Stacking Section of Composite Safety Barrier for Bridge)

  • 홍갑의;전신열;김기승;김승억
    • 복합신소재구조학회 논문집
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    • 제2권1호
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    • pp.1-7
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    • 2011
  • 본 논문에서는 복합소재 방호울타리의 6가지 적층 단면에 대한 충돌시뮬레이션을 실시하여 최적 적층 단면을 결정하였다. 먼저 6가지 단면 형상에 대하여 설문 조사를 통하여 형상을 결정하였다. 결정된 보 단면에 대하여 6가지 적층설계를 하였다. 적층에는 CSM, DB, DBT, Roving 섬유를 사용하였다. LS-DYNA를 사용하여 수평 및 3:1 경사에 대한 복합소재 보를 모델링하였다. 직육면체 추 및 원통형 추를 사용하여 낙하 충돌 시뮬레이션을 실시하였다. 시뮬레이션결과를 비교 분석하여 최적 적층 단면을 도출하였다.

염색체 마디 추출을 위한 최적타원 추정기법 (The Optimal Ellipse Estimation Method for Chromosome Bands Extraction)

  • 이상렬;이권순;전계록;장용훈;엄상희
    • 대한의용생체공학회:학술대회논문집
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    • 대한의용생체공학회 1995년도 춘계학술대회
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    • pp.227-229
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    • 1995
  • This paper attempts to examine an optimal method for the chromosome specific vector extraction. Usually, represented method are used with a line segmentation on a chromosome Image. It is not Inaccurate but also needs a long time for the analysis. This paper purpose to aquire specific vector in the image with a using optimal ellipse estimation method. Normally, shapes of chromosomes are curved and too difficult to analyze automatically. A chromosome has a lot of band which looks like an ellipse. If we can estimate their bands with an ellipse, we can reconstruct the sample Which Is straight and can be analyzed easily. We have rearranged a chromosome Image with above proposed. Result shows a reconstructed sample which Is simple for chromosome analysis.

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3/8" 유압 퀵 커플러의 피스톤형상을 고려한 최적설계에 관한 연구 (A Study on the Optimal Design According to the Piston Shape of the 3/8 Hydraulic Quick Coupler)

  • 김남용;우위팅;진진;조용민;류성기
    • 한국기계가공학회지
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    • 제20권2호
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    • pp.66-71
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    • 2021
  • A hydraulic quick coupler is a component used to easily connect or disconnect pipes or hoses that transfer high pressure fluid without leakage in various mechanical devices. In this study, to obtain an optimal design of a 3/8" hydraulic quick coupler, the effect of different shapes of the internal piston on the internal flow characteristics of the coupler was analyzed and evaluated through numerical analysis based on computational fluid dynamics. Subsequently, the optimal shape design of the internal piston was obtained by comparing the flow characteristics results such as velocity distribution, temperature distribution, and the pressure drop of the hydraulic quick coupler.

배나무 무인 방제기의 개발을 위한 살포 시스템 설계 (System Design for Developing the Remote Controlled Sprayer of Pear Trees)

  • 이봉기;민병로;이민영;화윤일;최동성;홍준택;이대원
    • 생물환경조절학회지
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    • 제22권4호
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    • pp.303-308
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    • 2013
  • 배나무 방제용 무인살포시스템 개발을 위하여 생력화를 위한 작업기기를 설계하였다. 또한, 노즐의 분무유형을 실험적으로 분석하여 적정 살포를 위한 노즐 각도, 노즐과의 거리, 수평방향 살포시 거리를 선정하였다. 본 연구를 수행하기 위하여 배의 과수 형태와 재배 환경을 사전 조사하였다. 살포시스템의 살포진행방향에 적합한 분사 노즐각도를 선정하였다. 배나무와 살포시스템 간의 수직거리에 따라 달라지는 살포 정도를 비교하기 위하여 노즐과의 높이에 따른 분포도를 측정하였다. 배나무와 살포 시스템과의 적정 측면 거리를 선정하기 위하여 측면 살포시 거리에 따라 달라지는 분무량을 측정하였다. 무인살포시스템의 약대는 배의 식재 간격에 적합하도록 좌우가 동일한 형태로 2.5m까지 펼쳐지도록 설계 및 제작 하였다. 또한 일정하지 않은 배나무의 높이에 따라 약대의 높이가 1.7m까지 조절되도록 하였다. 본 시스템에 적합한 노즐 각도는 $15^{\circ}$로 나타났다. 배나무와 살포시스템과의 수직거리는 0.7m에서 0.9m의 간격을 유지하여 약제를 살포해야 된다는 것을 알 수 있었다. 수평방향으로 살포하는 경우 좌우 -0.9m에서 0.9m까지의 분무량이 가장 많았다. 약대와의 거리가 0.9m에서 2.1m일 때 가장 많은 분무량을 나타냈다. 실험을 통하여 배 과수원에서의 무인살포시스템에 맞는 분무 환경을 확인 할 수 있었다. 배 과수와의 거리에 따라 적정 거리를 유지하는 시스템을 개발함으로써 효율적인 약액 살포가 가능하게 하였다. 하지만 본 연구에서 진행된 실험은 제한된 실내 환경에서 진행된 것이기 때문에 제작된 시스템의 실제 과수원 환경에서의 실험이 필요하다.

볼엔드밀 중삭가공시 커습에 의한 절삭특성과 공구마모 (Effect of Cusp on the Cutting Characteristics and Tool Wear of Semi-finishing in Ball End Milling)

  • 조철용;문상돈;류시형
    • 한국공작기계학회논문집
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    • 제15권5호
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    • pp.79-84
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    • 2006
  • In modem manufacturing, many products that have geometrically complicated features, including three-dimensional sculptured surfaces, are designed and produced. In the production of these complex-shaped mechanical components, e.g. automobile dies, molds, and various engineering applications, the ball-end milling process is one of the most widely used NC machining processes that consists of roughing, semi-finishing and finishing. In semi-finishing, cusps remained after roughing according to the used tools that have two patterns of stairs and wave shapes. These cusp shapes have air-cut in cutting and instability caused by high cutting speed that affects the cutting characteristics such as cutting force and tool wear. Cutting characteristics are measured and analyzed through cutting force, FFT analysis of cutting force and tool wear along cutting length according to low tool paths with same metal removal rate. As a results of the experiments, this study suggests the optimal conditions of tool path and cutting direction. This approach for the cutting characteristics of semi-finishing provides a useful aid for the productivity and efficiency improvements of NC machining processes.

유입부 형상이 저전압 전동기 냉각홴의 공력성능에 미치는 영향 (Effects of Inlet Vent Shape on Aerodynamic Performance of a Low-Voltage Electric Motor Cooling Fan)

  • 박재민;허만웅;김광용
    • 한국유체기계학회 논문집
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    • 제19권5호
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    • pp.42-49
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    • 2016
  • Aerodynamic analysis of a low-voltage electric motor has been performed with various inlet vent shapes. Effects of inlet vent shape on aerodynamic performance of a motor cooling fan have been investigated numerically using three-dimensional Reynolds-averaged Navier-Stokes equations. The k-${\varepsilon}$ turbulence model was used for the analysis of turbulence. The finite volume method and unstructured tetrahedral grids were used in the numerical analysis. Optimal grid system in the computational domain was selected through a grid-dependency test. From the results of the flow analysis, considerable energy loss by flow separation was observed in the flow passage. It was found that mass flow rate through the cooling fan in the low-voltage motor can be increased by modifying the inlet vent shape. And, some inlet vent shapes were suggested to improve the aerodynamic performance of the motor cooling fan.