• Title/Summary/Keyword: width of thickness

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Clasp arm의 형상과 재료 탄성에 따른 단위 변위에 대한 힘 (Force per unit Displacement according to the Shape of a Clasp Arm and Flexibility of the Material)

  • 임동천
    • 대한치과기공학회지
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    • 제23권2호
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    • pp.171-177
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    • 2002
  • The purpose of this study is to evaluate force per unit displacements according to the shape of a clasp arm and flexibility of the material. Effect of four shape parameters of a clasp, base width and thickness and tip width and thickness, on tip displacement and force per unit displacement was investigated to get the fact that displacement and force per unit displacement at the tip increase as thickness and width of clasp arm increase just as expected. But force per unit displacement is much more affected by the change in thickness than by change in width. So it is effective to increase the thickness rather than width in order to increase the force at the tip using the same amount of the material.

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Double-Sided Deep-Ridge 도파관 구조 수직 방향성 결합기의 날개구조부 폭과 두께가 편광 특성에 미치는 영향 (Effect of wing width and thickness on the polarization characteristics of vertical directional couplers using the Double-Sided Deep-Ridge waveguide structure)

  • 정병민;윤정현;김부균
    • 한국광학회지
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    • 제15권4호
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    • pp.293-298
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    • 2004
  • Double-Sided Deep-Ridge(DSDR) 수직 방향성 결합기의 날개구조부 폭과 두께가 편광에 따른 결합길이에 미치는 영향에 관하여 연구하였다. 날개구조부가 존재하지 않는 DSDR 수직 방향성 결합기는 편광에 무관한 결합길이를 가질 수 없음을 볼 수 있었다. 일정한 날개구조부 두께에 대하여 날개구조부 폭이 특정 길이 이상이 되면 TE 모드와 TM 모드의 결합길이의 변화는 거의 없으며 또한 두 모드의 결합길이의 차이도 거의 발생하지 않음을 볼 수 있었다. 따라서 편광에 무관한 결합길이를 가지는 DSDR 수직 방향성 결합기를 구현하기 위한 최소 날개구조부 폭이 존재함을 볼 수 있었다. 이러한 최소 날개구조부 폭은-같은 코어 두께에 대해서는 날개구조부 두께가 증가할수록, 같은 날개구조부 두께에 대해서는 코어 두께가 감소할수록-증가함을 볼 수 있었다. 또한 최소 날개구조부 두께는 코어의 두께에 의하여 결정됨을 볼 수 있었고 코어의 두께가 증가할수록 최소 날개구조부 두께는 감소함을 볼 수 있었다.

Micro-computed tomography evaluation of general trends in aligner thickness and gap width after thermoforming procedures involving six commercial clear aligners: An in vitro study

  • Palone, Mario;Longo, Mattia;Arveda, Niki;Nacucchi, Michele;De Pascalis, Fabio;Spedicato, Giorgio Alfredo;Siciliani, Giuseppe;Lombardo, Luca
    • 대한치과교정학회지
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    • 제51권2호
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    • pp.135-141
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    • 2021
  • Objective: To assess the effects of thermoforming on aligner thickness and gap width in six aligner systems with the same nominal thickness. Methods: Six passive upper aligners of different brands were adapted to a single printed cast. Each sample was evaluated with high-resolution micro-computed tomography. To investigate aligner thickness and gap width, two-dimensional (2D) analysis was conducted assessing the effects of the following variables: tooth type (central incisor, canine, and first molar), 2D reference points, and aligner type. Data were analyzed and compared using analysis of variance and Tukey's post-hoc tests (p < 0.05). Results: Tooth type, dental region, and aligner type affected both the gap width and aligner thickness. The aligner thickness remained moderately stable across the arch only in the F22. Conclusions: All thermoformed samples displayed smaller aligner thickness and gap width at anterior teeth and both gingival and coronal centers than at posterior teeth and occlusal surfaces.

하악 절치 근원심폭경과 법랑질 두께의 관계 (Relationship between mesiodistal width and enamel thickness in mandibular incisors)

  • 한욱;강성남;임성훈
    • 대한치과교정학회지
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    • 제41권3호
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    • pp.184-190
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    • 2011
  • 하악 절치부에서 보이는 총생은 하악 절치의 큰 MD/FL (mesiodistal/faciolingual) 인덱스와 관련이 있음이 보고되었다. 큰 MD/FL 인덱스를 보이는 절치에서 치간 삭제를 통해 근원심폭경을 줄여 MD/FL 인덱스를 줄이고 공간을 확보하는 방법이 정당화되기 위해서는 MD/FL 인덱스가 클수록 인접면 법랑질 두께가 더 두꺼워야 할 것이다. 본 연구의 목적은 하악 절치의 MD/FL 인덱스, 근원심폭경, 최대풍융부/치경부폭경비와 같은 치아의 형태적 요인과 인접면 법랑질 두께 사이에 상관관계가 있는지를 조사하는 것이었다. 발거된 하악 절치 40개에서 MD/FL 인덱스, 근원심폭경, 최대풍융부/치경부폭경비를 구하였으며, 근원심폭경을 구한 선상까지 순면을 연마하여 그 단면에서 법랑질 두께를 측정하였다. 치경부근원심폭경은 순면을 연마한 단면에서의 좌우측 백악법랑경계 사이의 폭경을 측정하였다. 이후 법랑질 두께와 MD/FL 인덱스, 근원심폭경, 최대풍융부/치경부폭경비의 상관관계를 조사하였다. 연구결과 하악 절치의 법랑질 두께는 편측에서 $0.75{\pm}0.07mm$였고, 근원심폭경은 $5.56{\pm}0.40mm$였다. 법랑질 두께와 근원심폭경 간에는 유의한 상관관계가 있었지만(R = 0.68), 법랑질 두께와 MD/FL 인덱스, 법랑질 두께와 최대풍융부/치경부폭경비 간에는 상관관계가 없었다. 이는 근원심폭경이 큰 치아에서는 치간 삭제를 더 많이 할 수 있지만, 동일한 근원심폭경을 갖는 절치들의 경우 MD/FL 인덱스가 큰 하악 절치 또는 최대풍융부/치경부폭경비가 커서 삼각형의 형태를 갖는 하악절치에서 치간 삭제를 더 많이 할 수는 없다는 것을 나타낸다.

콘크리트 강도 및 강관 폭두께비에 따른 각형 CFT 단주의 내력평가 (Strength Evaluation of Rectangular CFT Stub Columns varing with Concrete Strength and Width-to-Thickness Ratio of Steel Tubes)

  • 심종석;한덕전
    • 한국디지털건축인테리어학회논문집
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    • 제11권2호
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    • pp.31-39
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    • 2011
  • Concrete-filled steel tube(CFT) columns have become popular for building construction due to not only composite effect of steel tube and infilled concrete, but also more economical. The purpose of this paper is to propose the applicable boundary formula of width-to-thickness ratio for rectangular steel tube as using CFT column. A parametric study was performed taking width-to-thickness ratio of rectangular steel tube and compressive strength of concrete as the main parameter. The strength of concrete are selected to 30, 60, 90MPa. The non-linear analysis was adopted in order to take into account the effect of concrete strength. Finally, from the test and analysis results, the effect of increasing strength according to concrete strength and width-to-thickness of steel tube and plastic behavior of specimens were verified distinctly.

항공기 박판 구조의 가공가능 폭과 두께에 관한 실험 연구 (An Experiment of Machineable Width and Thickness of Airframe Thin Plate Structure)

  • 신용보;김수진
    • 한국생산제조학회지
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    • 제22권1호
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    • pp.162-167
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    • 2013
  • The most important factor in an aircraft manufacturing is stability and weight reduction. Most of aircraft components are designed with thin plate type to satisfy weight reduction needs. The thin plate is difficult to be machined because it is apt to be vibrated by dynamic force generated in milling process. The most critical factor in machining of aluminum thin plate is width and thickness between stiffeners. So we tested many cases to find out the machinable minimum thickness at different width between stiffeners. And with the data obtained from many tests, this papers suggested the standard width thickness relation that is machinable without vacuum fixture. Machinist will be able to reduce the cost of aircraft thin plate parts by reducing the number of vacuum fixture used by the help of this standard.

Ultimate capacity of welded box section columns with slender plate elements

  • Shen, Hong-Xia
    • Steel and Composite Structures
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    • 제13권1호
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    • pp.15-33
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    • 2012
  • For an axially loaded box-shaped member, the width-to-thickness ratio of the plate elements preferably should not be greater than 40 for Q235 steel grades in accordance with the Chinese code GB50017-2003. However, in practical engineering the plate width-to-thickness ratio is up to 120, much more than the limiting value. In this paper, a 3D nonlinear finite element model is developed that accounts for both geometrical imperfections and residual stresses and the ultimate capacity of welded built-up box columns, with larger width-to-thickness ratios of 60, 70, 80, and 100, is simulated. At the same time, the interaction buckling strength of these members is determined using the effective width method recommended in the Chinese code GB50018-2002, Eurocode 3 EN1993-1 and American standard ANSI/AISC 360-10 and the direct strength method developed in recent years. The studies show that the finite element model proposed can simulate the behavior of nonlinear buckling of axially loaded box-shaped members very well. The width-to-thickness ratio of the plate elements in welded box section columns can be enlarged up to 100 for Q235 steel grades. Good agreements are observed between the results obtained from the FEM and direct strength method. The modified direct strength method provides a better estimation of the column strength compared to the direct strength method over the full range of plate width-to-thickness ratio. The Chinese code and Eurocode 3 are overly conservative prediction of column capacity while the American standard provides a better prediction and is slightly conservative for b/t = 60. Therefore, it is suggested that the modified direct strength method should be adopted when revising the Chinese code.

Effect of cross-sectional vortex formation on magnetization reversal in rectangular shaped Permalloy nanowires

  • Khan, Imran;Hong, Jisang;Hwang, Chanyong
    • 한국자기학회:학술대회 개요집
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    • 한국자기학회 2013년도 자성 및 자성재료 국제학술대회
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    • pp.115-115
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    • 2013
  • In order to pinpoint the different factors responsible for magnetization reversal, we performed simulation using OOMMF micromagnetic package for rectangular shaped permalloy element having length of $1{\mu}m$, width 50-100 nm and thickness 15-80 nm with length to width ratio L/W>4. Interestingly an increase in coercivity with thickness is found for every width below a critical thickness. With increasing width and thickness, the distinct behavior of coercivity, hysteresis loops and reversal mechanism are presented. Vortex end domains are observed during the magnetization reversal beyond particular thickness, where the three dimension reversal mechanism is expected to begin, causing a sudden increase in coercivity.

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폭두께비가 큰 각형CFT 단주의 설계식 (Design Equation for Square CFT Columns with Large Width-to-Thickness Ratio)

  • 김선희;최영환;최성모
    • 한국강구조학회 논문집
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    • 제21권5호
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    • pp.537-544
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    • 2009
  • AISC(2005)나 KBC(2005)등의 기준에서는 콘크리트 충전 강관(Concrete Filled Steel Tube) 기둥의 내력산정에서 폭두께비의 제한을 두고 있으며 최대 폭두께비를 초과하는 기둥에 대해서는 설계식을 제시하지 않고 있다. 본 연구는 stiffened (양단지지) 플레이트에서는 좌굴이 발생하더라도 바로 내력저하가 발생하지 않고 상당한 양의 좌굴 후 강도를 발휘할 수 있어 폭두께비가 큰 강관을 사용하는 것이 경제적일 수 있다는 점을 착안, 유효폭 개념을 도입해서 폭두께비가 큰 각형 CFT의 강도를 계산할 수 있는 설계식을 제안하였다. AISC 2005, KBC 2005와 본 연구에서 제안한 식을, 폭두께비를 변수로 수행한 4개의 각형 CFT 기둥 실험결과와 비교하였며 제안된 설계식의 적용가능성을 확인하였다. 이에 Uy(2005), Dalin Liu(2005)는 폭두께비가 큰 단주 CFT에 한에서 선행 연구된 실험데이타를 근거로 제안 설계식을 단순적용 하였다. 폭두께비가 초과된 각형CFT 단주를 검토 대상기본으로 1. 용접 조립된 정사각형 단면 2. 모살용접된 정사각형 단면 (b/t 60mm. 80mm, 100mm) 3. 한 폭면의 폭두께비가 초과하는 직사각형단면의 (b/t 45.5) 실험체를 선정하여 제안식의 타당성을 검토해 보고자 한다.

Resonant Transmission through Slits in a Cavity inside a Thin Conducting Plane

  • Lee, Jong-Ig;Cho, Young-Ki
    • Journal of electromagnetic engineering and science
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    • 제10권3호
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    • pp.127-131
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    • 2010
  • In this paper, the problem of electromagnetic transmission via slits in a cavity inside a conducting screen of finite thickness has been considered in the case that the transverse electric(to the slit axis) polarized plane wave is incident on a slit. The problem is solved numerically by the method of moments and the results are compared with those obtained from an equivalent circuit suitable for a case in which the slit width is infinite and the structure is modified to the two partially overlapped conducting planes. It is observed that when the cavity is resonated, the effective slit width reaches its maximum value of $1/\pi$ wavelengths, irrespective of the actual slit width and the incidence angle. When the thickness of the conducting plane is much smaller than the wavelength, the numerical results for the effective slit width(or transmission width) agree well with those obtained from the equivalent circuit, even though the slit is as narrow as the thickness of the conducting plane.