• 한국강구조학회 논문집
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• 제16권6호통권73호
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• pp.737-745
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• 2004

최근 구조물의 정확한 해석을 위하여 접합부의 강성에 반강접 개념이 도입되고 있다. 우리나라의 경우 반강접 접합부의 실험과 이론해석에 대한 연구가 산발적으로 진행되고 있으며, 체계적인 강구조설계를 진행할 정도의 연구성과를 내지는 못 한 상태이다. 그래서 스플릿-티(Split-Tee)를 이용한 접합부의 설계는 국내의 강종과 하중특성을 고려되지 못한 선진국의 연구자료에 의존하고 있는 실정이다. 본 논문은 F10T 고력볼트를 사용한 스플릿-티 접합부의 반강접 특성을 파악하고자, 기둥-보 접합부에 대한 반강접 연구 이전 단계로서 스플릿-티 인장접합부의 구조성능과 변형특성에 대해 실험을 통하여 규명하고자 한다. 플랜지 두께, 도장, 초기도입축력 및 하중가력패턴을 실험변수로 하였으며, 총 20개의 실험체를 제작하여 300ton UTM으로 인장실험을 수행하였다. 각 변수에 따른 스플릿-티 인장 접합부의 구조성능과 거동을 평가하였다.

• 대한치과보철학회지
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• 제34권2호
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• pp.385-402
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• 1996

The purpose of this study was to analyze how the stability of the implant prostheses and the loosening of the fastening screw was affected when the various types of Hex structure provided for the effect of anti-rotation of the single prostheses were given. Three dimensional finite element model was designed with which the implants with the external hex type of 0.75mm, 1.5mm and the implant with the internal hex type of 0.75mm, 1.5mm and the implant with the external hex type of $15^{\circ}$ tapered shape of 0.75mm were supposed to completely osseointegrate to the mandible. After fininshing the finite element model, the preload of 10N at the fastening screw was applied and then the vertical and $30^{\circ}$ lateral load of 200N was applied respectively at the cusp tips of the prostheses. The following results were obtained : 1. In case of displacement, the amount of displacement was increased at the internal hex type(model C, D) than at the external hex type(model A, B, E) when the vertical and lateral load was applied. 2. Less equivalent stress was represented at the model B with increased external hex height than at the model A when the vertical and lateral load was applied. 3. Much stress was represented at the model E with increased hex angle than at the model A in case of the stress happened to the implant body and the fastening screw when the vertical and lateral load was applied. 4. Much equivalent stress was represented at the model D with deepened internal hex height than at the model C when vertical and lateral load was applied. 5. The least stress was taken at the model B and the most stress was taken at the model D in case of the stress happened to the implant when the vertical and lateral load was applied. 6. The least stress was taken at the model C at the vertical load. And the least stress was taken at the model B at lateral load in case of the stress happened to the fastening screw. As a results of this study, the good lateral stability of prostheses and less stress of the component of implant was taken when the external hex height was increased, and the risk of neck fracture of implant and fastening screw was increased when the internal hex height was deepned because of long screw neck portion and thin implant neck portion.

• 대한치과보철학회지
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• 제45권2호
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• pp.240-249
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• 2007

Statement of problem: A phenomenon of screw-loosening in implant abutment is frequently occurred in a single and multiple implant restoration. Purpose: This study was performed to evaluate an effect of abutment material on screw-loosening before and after a cyclic loading. In a single-tooth implant, different materials of abutment, Type III Gold alloy and Zirconium composite$(ZrO_2/Al_2O_3)$ were used. Material and method: The Gold alloy(Type III) and Zirconium composite$(ZrO_2/Al_2O_3)$ were used to make a superstructure of implant, the one of types of UCLA, Each group was constituted of 5 sample with a 30-degree offset angulated loading platform. The external hexagonal fixture was rigidly hel d in a special holding zig to ensure solid fixation without rotation during the tightening and a cyclic loading. A Titanium-alloy screw was used to connect and controlled to be tighten in 20Ncm torque by a digital torque gauge. A 20 times of consecutive closing/opening cycle were performed to evaluate the immediate torque loss. In 5 sample of each material group, an initial opening torque was recorded during 3 closing/opening cycle, then 2Hz, 200N, 1,000,000 cyclic loadings were performed, then a opening torque was evaluated. Result & Conclusion: 1. In this limited study, titanium alloy screw tightened in 20Ncm, a cold-welding phenomen on was not observed during the 20 times of closing/opening cycle(p=0.11, p=0.18). 2. In titanium alloy abutment screw, repeated opening and closing of the screw caused to progressive decrease of opening torque(p=0.014). 3. The difference in preload of screw between gold alloy abutment and ceramic$(ZrO_2/Al_2O_3)$ abutment was not significant(p=0.78). 4. The difference in torque loss of screw between gold alloy abutment and ceramic$(ZrO_2/Al_2O_3)$ abutment was not significant after 2Hz,200N, 1,000,000 cyclic loading(p=0.92). 5. In titanium alloy abutment screw tightened by 20Ncm, the screw loosening was not significant on each group after 2Hz, 200Ncm, 1,000,000 cyclic loading(p=0.59).

• 콘크리트학회논문집
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• 제20권5호
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• pp.583-592
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• 2008

최근 고강도콘크리트의 압축강도, 탄성계수 및 최대하중에서의 변형에 대한 고온의 영향이 실험적으로 연구되어지고 있다. 본 연구는 40, 60, 80 MPa 급 고강도콘크리트의 재료 역학적 특성에 있어서 $20{\sim}700^{\circ}C$ 범위로 상승되는 온도의 영향을 연구하는데 그 목적이 있다. 본 연구에서는 설계하중 사전재하 및 잔존강도시험 방법으로서 시험체를 가열하기 전에 상온 압축강도의 25% 하중을 사전재하한 후 가열을 실시하고, 가열하는 동안 하중을 유지하며, 목표온도에 도달한 후 고온상태 및 상온에서 24시간 냉각상태에서 시험체가 파괴될 때까지 재하를 실시하였다. 시험은 W/B 46%, 32% 및 25%로 이루어진 콘크리트 시험체에 대하여 $20{\sim}700^{\circ}C$의 다양한 온도하에서 실시하였다. 시험 결과 콘크리트 강도가 증가할수록 고온에서의 상대적인 압축강도와 탄성계수는 감소하였으며, 최대하중에서의 축방향 변형은 설계하중 사전재하와 상관성이 높은 것으로 나타났다. 또한 온도상승에 따른 콘크리트의 열팽창 변형은 압축강도 뿐만 아니라 하중 크기의 영향을 받는 것으로 나타났으며, 최종적으로 가열을 받은 고강도콘크리트의 압축강도 및 탄성계수에 대한 모델식을 제안하였다.

• 한국전기전자재료학회논문지
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• 제27권5호
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• pp.286-291
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• 2014

In this study, novel ultrasonic rotary motor of hexadecagon shape stator was proposed. Stator of the hexadecagon ultrasonic motor was composed of an elastic ring and ceramics. The elastic ring had sixteen sides and sixteen angular points. Eight ceramics were attached on the outer surface of the eight sides of the ring. When rotor of cylindrical shaft was inserted inside of the ring stator, central lines of the sixteen sides of the stator hold the shaft by the slight pressures(frictions). This slight pressure was a preload of the motor and it could be controlled by radius and thickness of the ring. When two sinusoidal voltages which have 90 degree phase difference were applied to each four ceramics, elliptical displacements of inner surface of the ring were obtained. These elliptical displacements of the inner surface rotated the shaft rotor through the frictions. The proposed hexadecagon ultrasonic motor was designed and analyzed by using the finite element method (FEM), depending on materials of the elastic ring. Based on the FEM results, one model of motor which showed maximum displacement at contact points was chosen and fabricated. And characteristics of the motor were compared with simulated results. When the motor was fabricated with these results, EL20ET0.5CT0.5CW2 model showed 115[rpm] speed about input voltage of 60[Vrms] at 65.6[kHz]. And the maximum torque of 6[gfcm] was obtained. From these results, the hexadecagon shaped ultrasonic motor can be used to actuator for optical device which needs detailed position control. Also it can be used to medical and portable device by reducing size and weight.

• 항공우주시스템공학회지
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• 제12권4호
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• pp.75-80
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• 2018

위성용 카메라의 경우 광학계의 초점을 제어하기 위한 포커싱 메커니즘이 필수적이다. 그러나 국내의 위성용 광학계 포커싱 메커니즘 관련 연구는 시작 단계이며, 관련 보유 기술 또한 열제어형에 국한되어있다. 따라서 본 논문에서는 소형위성용 광학계에 적용 가능한 모터 구동형 포커싱 메커니즘을 제안하였다. 제안된 메커니즘은 모터 구동에 의해 secondary mirror에 z축 변위를 발생시키도록 설계하였다. 또한 서포터에 flexure hinge를 설치하여 사전하중을 가하도록 하여 메커니즘내 부품간 제작공차 및 조립공차로 인한 정렬도 오차를 최소화하도록 하였다. 메커니즘 제작 후 LVDT 센서(linear variable differential transformer sensor)와 레이저 변위측정기로 정렬도(de-space, de-center, tilt)를 측정한 결과 소형위성광학계에 적용 가능한 수준의 정렬도를 갖는 것을 확인하였다.

• 한국전산구조공학회논문집
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• 제30권3호
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• pp.239-248
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• 2017

솔레노이드 밸브는 구조에 따라 스풀 밸브와 포핏 밸브로 구분된다. 구조가 단순하고 오염에 민감한 스풀 밸브에 대하여 연구가 많이 진행되고 있는 반면 오염에 덜 민감하고 장시간 작동에 용이한 포핏 밸브는 구조가 복잡하여 여전히 많은 연구가 필요하다. 포핏 밸브를 설계하기 위해서 고려해야 하는 사항으로 포핏의 직경, 포핏의 각도, 디스크의 지름, 스프링 강성, 스프링 예하중, 유로 구조 등 다양한 설계변수가 있다. 기존 연구에서는 설계변수를 한가지로 선정하여 연구가 진행되었고, 설계변수가 포핏 밸브의 유동특성에 미치는 영향에 대한 연구가 부족하다. 본 논문에서는 3/2Way 솔레노이드 밸브용 포핏 밸브의 설계변수 변화에 따른 유동특성의 변화를 분석하였다. 포핏 밸브의 설계변수 선정은 선행연구된 사례와 초기모델해석결과를 참고하여 진행하였다. 그리고 설계변수에 따른 최대압력, 최소압력, 압력강하의 영향을 평균분석(ANOM)을 사용하여 살펴보았다. 향후 3/2Way 솔레노이드 밸브용 포핏 밸브를 설계할 때 주효과를 파악하여 설계변수 선정에 사용하면 효율적인 설계변수 선정이 가능할 것으로 예상된다.

• 대한치과보철학회지
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• 제44권6호
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• pp.740-750
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• 2006

Statement of problems. In an attempt to reduce screw loosening, dry lubricant coatings such as pure gold or tefron have been applied to the abutment screw. However, under repeated tightening and loosening procedures, low wear resistance and adhesion strength of coating material produced free particles on the surface of abutment screw and increased frictional resistance resulting in screw tightening problems. Purpose. The aim of this study was to compare friction coefficient, adhesion strength, vickers hardness and evaluate coating surface of titanium alloy specimens coated with TiN(titanium nitride), ZrN(zirconium nitride) and WC(tungsten carbide). Material and method. Titanium alloy(Ti-6Al-4V) discs of 12mm in diameter and 1mm in thickness divided into 4 groups. TiN, ZrN and WC was coated for the specimens of 3 groups respectively, and those of 1 group were not coated. Each group was made up of 4 specimens. In this study, sputtering method was used among the PVD(Physical Vapor Deposition) techniques available for TiN, ZrN and WC coatings. Friction coefficient, adhesion strength, vickers hardness and coating surface of 4 groups were measured. Results. 1. For all three coating conditions, friction coefficient was significantly decreased. Especially, ZrN coated surface showed the lowest value. $TiN(0.39{\pm}0.02)$, $ZrN(0.24{\pm}0.01)$, $WC(0.31{\pm}0.03)$. 2. TiN coating showed the highest adhesion strength, however ZrN coating had the lowest value. $TiN(25.3N{\pm}1.6)$, $ZrN(14.8N{\pm}0.6)$, $ WC(18.4N{\pm}0.7)$. 3. Vickers hardness of all three coatings was remarkably increased as compared with that of none coated specimen. TiN coating had the highest Vickers hardness, however WC coating showed the lowest value. $TiN(1865.2{\pm}33.8)$, $ZrN(1814.4{\pm}18.6)$, $WC(1008.5{\pm}35.9)$. 4. The ZrN or WC coated specimen showed a homogeneous and smooth surface, however the rough surface with defects was observed for TiN coating. Conclusions. When TiN, ZrN and WC coating applied to the abutment screw, frictional resistance would be reduced, as a result, the greater preload and prevention of the screw loosening could be expected.

• 콘크리트학회지
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• 제11권1호
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• pp.279-288
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• 1999

콘크리트 구조물의 크리프해석은 주로 크리프식의 중첩원리에 기초한 방법에 의해 수행되고 있다. 그러나 크리프식의 중첩을 응력이 증가하거나 일정할 경우에는 비교적 정확한 예측이 가능하지만, 응력이 감소하는 경우에는 상당한 오차를 나타낸다. 이것은 지속하중과 응력감소 과정에서 크리프와 관련된 콘크리트의 성질이 변화되므로 크리프 회복을 크리프 식의 중첩으로 정확하게 모사할수 없기 때문이다. 따라서, 본 연구에서는 감소와 증가를 반복하는 응력 이력을 지니는 콘크리트 구조물의 좀더 정확하고 합리적인 장기거동 해석을 위하여 응력의 감소를 단순히 크리프식의 중첩에 의해 해석한 기존의 방법과는 달리 크리프식과 크리프 회복식으로 표현하여, 소위 2함수 방법(two-function method)를 콘크리트구조물의 해석에 적용하는 방법을 제시하였다. 본 연구의 2함수방법을 콘크리트 구조물의 장기거동 해석을 적용하기 위해, 시간단계 동안 다양한 응력 변화에 대하여 크리프 변형도 증분량을 계산하는 방법을 제시하였다. 본 연구의 해석방법에 의해서 해석된 결과를 기존의 크리프식의 중첩에 의한 결과 및 기존의 실험결과들과 비교 분석한 결과, 기존의 중첩법은 실험결과와 많은 차이를 보이고 있으나 본 연구의 해석방법은 실험결과와 잘 맞고 있음을 보여주고 있다. 따라서, 크리프회복식을 이용하는 본 연구의 해석방법은 기존의 크리프식의 중첩방법이나 기존의 설계기준에 비해 변화하는 응력이력 하에서의 콘크리트 구조물의 크리프거동을 더 정확하게 서술할 수 있는 방법으로서 앞으로 설계기준 작성과 실제 구조물 해석에 효율적인 응용이 기대되고 있다.

• 대한치과보철학회지
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• 제45권5호
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• pp.675-686
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• 2007

Statement of problem: Titanium nitride(TiN) coatings are the most general and popular coating method and used to improve the properties of metallic surface for industrial purposes. When TiN coating applied to the abutment screw, frictional resistance would be reduced, as a results, the greater preload and prevention of the screw loosening could be expected. Purpose: The purpose of this study was to investigate mechanical properties of TiN coated film of various coating thickness on the titanium alloy surface and to evaluate proper coating thickness. Material and method: 95 Titanium alloy (Ti-6Al-4V) discs of 15 mm in diameter and 3 mm in thickness were prepared for TiN coating and divided into 7 groups in this study. Acceding to coating deposition time (CDT) with TiN by using Arc ion plating, were divided into 7 groups : Group A (CDT 30min), Group B (CDT 60min), Group C (CDT 90min), Group D (CDT 120min), Group E (CDT 150min), Group F(CDT 180min) and Group G (no CDT) as a control group. TiN coating surface was observed with Atomic Force Microscope(AFM), field emission scanning electron microscopy(FE-SEM) and examined with scratch tester, wear tester. Result: 1. Coating thickness fir each coated group was increased in proportion to coating deposition time. 2. Surface of all coated groups except Group A was homogeneous and smooth. However, surface of none coated Group G had scratch. 3. Adhesion strength for each coated group was increased in proportion to coating deposition time. 4. Wear resistance for each coated group was increased in proportion to coating deposition time. 5. Surface roughness in Group A, B, C was increased in proportion to coating deposition time. But, surface roughness in Group D, E, F was showed decreased tendency in proportion to coating deposition time. Conclusion: According to coating deposition time, mechanical properties of TiN coated film were changed. It was considered that 120 minutes coating deposition time ($1.32{\mu}m$ in coating thickness) is necessary.