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노치성형 발파공을 이용한 균열제어 발파방법의 균열발생 특성에 대한 수치해석적 고찰 (Numerical study on the charateristics of fracture growth in fracture controlled blasting using notched blasthole)

  • 백승규;김재동;임한욱;류창하
    • 터널과지하공간
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    • 제9권1호
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    • pp.64-71
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    • 1999
  • 균열면을 제어하는 발파방법의 하나로서 노치성형 발파공을 이용한 방법의 균열발생 특성을 2차원 및 3차원 유한요소 해석방법을 이용하여 고찰하였다. 균열제어를 위한 모델로는 노치가 성형된 발파공과 일반적인 원형 발파공을 대상으로 하였으며, 발파 압력에 대한 암반의 동적 반응, 탄성 및 소성 변형의 발생 특성, 그리고 이로 인한 발파 균열의 성장 전파 특성을 분석하여, 균열의 능동적 제어와 보다 효율적인 발파가 이루어 질 수 잇는 조건들을 규명하고자 하였다. 해석 결과 일반 발파공의 정하중 탄성 모델의 경우 공반경의 약 3배인 6cm 까지 집중된 응력의 크기가 파괴강도를 초과하는 것으로 나타났으며 탄소성 모델의 경우 균열이 전파거리는 공반경의 145배인 30cm 가지 확장되었다. 또한 폭 5mm 길이 30 mm 의 노치가 가공된 발파공의 경우 정하중하에서 공반경의 23배인 46cm 까지 균열이 진전되었으며, 균열의 방향은 노치 첨단의 방향으로 생성되는 것으로 나타났다.

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구치부 부분 무치악 결손에서 유용한 세 가지 임프란트 수복법들의 응력분산에 관한 3차원 유한요소법적 비교연구 (THE THREE DIMENSIONAL FINITE ELEMENT ANALYSIS OF THE STRESS DISTRIBUTION IN THE THREE TREATMENT OPTIONS OF IMPLANTS RESTORATIONS FOR THE POSTERIOR PARTIAL EDENTULISM)

  • 김일규;이성호;류승현;최진호;한예숙;손충렬;변효인
    • Journal of the Korean Association of Oral and Maxillofacial Surgeons
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    • 제30권3호
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    • pp.175-180
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    • 2004
  • In this study, three treatment options to replace two posterior missing teeth were investigated using three dimensional finite element analysis: two wide(${\phi}5.0mm$) implants(the experimental model I), two standard(${\phi}3.75mm$) implants(the experimental model II), and three standard(${\phi}3.75mm$) implants(the experimental model III). Two kinds of load case were applied ; 1) perpendicular on occlusal surface(axial load), parallel on occlusal surface(lateral load). 2) perpendicular on occlusal surface(3mm lateral to central point). The results obtained from this study were as follows; value of Von-mises stress (equivalent stress) was smallest in the two wide implant among the three experimental models. It was reported that the diameter is the efficient factor than osseointegrated surface area.

CT상의 HU 수치에 따른 유한요소모델을 이용한 RME 사용에 따른 응력분포에 대한 연구 (Stress Distribution following Rapid Maxillary Expansion using Different Finite Element Model according to Hounsfield Unit Value in CT Image)

  • 윤병선;차경석;정동화
    • 구강회복응용과학지
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    • 제23권4호
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    • pp.313-326
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    • 2007
  • With rising prevalency of mouth breathing children caused by developing civilization and increasing pollution, there are many maxillary transverse discrepancy patients with undergrowth of maxilla. For improving this, maxillary mid-palatal suture splitting was often performed. The purpose of this study was to analyse the stress distribution on the craniofacial suture and cranium after rapid maxillary expansion by finite element model. The boy(13Y6M) was chosen for taking computed-tomography for finite element model. Three-dimensional model of maxilla, first premolar, first molar, buccal and lingual part of rapid maxillary expansion were constructed. 1. The alveolar bone adjacent to the first molar and the first premolar that was affected directly by rapid maxillary expansion was displaced laterally approximately 4.04mm at maximum. The force decreased toward anterior region and frontal alveolar bone displaced laterally about 3.18mm. 2. A forward maximum displacement was exhibited at zygomatic process middle region. 3. At maximum, maxillary median part experienced 0.973mm downward repositioning and 0.65mm upward repositioning at lateral alveolar bone. 4. Von mises stress was observed the largest stress distribution around teeth and zygomatic buttress. 5. The largest tensile force was observed around alveolar bone of teeth, while compression force was observed at zygomatic buttress.

섬유 강화 컴포지트의 수리 후 접합 강도 (Bond strength of fiber reinforced composite after repair)

  • 김민정;김경호;최광철
    • 대한치과교정학회지
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    • 제36권3호
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    • pp.188-197
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    • 2006
  • 교정 치료 시 사용되는 섬유 강화 컴포지트(FRC, fiber reinforced composite)는 구강 내에서 저작압 등의 지속적인 응력과 수분 흡수 등의 이유로 파절이 일어나는 경우가 있다. 이 때 모든 FRC를 제거하지 않고 수리(repair)하는 경우에 적절한 강도를 얻기 위해 첨가해야 할 FRC의 양 및 그 파절 양상을 알아보고자 하였다. 두 개의 FRC strips를 1, 2, 3, 그리고 4mm 만큼 겹쳐(E1, E2, E3, E4군) 시편을 만드는 방법으로 수리를 재현한 후 light emitting diode 광중합기로 중합하고, 3점 굽힘 실험을 시행하여 겹침 길이와 접합 강도간의 관계에 대해 조사하였다. 최대 하중치는 E4군에서 2.67N으로 최대였고, 대조군(2.39N), E3군(2.35N), E2군(2.10N), 그리고 E1군(1.75N)의 순이었다. 강성 역시 최대 하중치와 같이 E4군(2.32 N/mm)에서 최대치를 기록하였으나, E3군(2.06N/mm)의 강성이 대조군(1.88N/mm)보다 더 큰 값을 보였다. 겹침 길이가 길수록 완전히 두 조각으로 파절되기 보다 가운데 또는 critical section 에서 굽힘 양상을 보였다. 반면 겹침 길이가 짧은 경우 두 조각으로 부러지는 파절 양상을 보였다. 이상의 실험에서 길이 10 mm인 연결자 형태의 FRC의 수리 시 적절한 강도를 얻기 위해서는 최소 3 mm의 strips를 겹쳐야 하고, 이 때 주로 나타나는 실패 양상인 굽힘을 최소화하기 위해 연결 부위에 바로 인접하여 두께가 급격하게 변하는 critical section의 보강이 필요할 것으로 사료된다.

Cr-Mo강 용접후 열처리재의 피로파괴에 관한 연구

  • 임재규;정세희;최동암
    • Journal of Welding and Joining
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    • 제5권1호
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    • pp.73-80
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    • 1987
  • During PWHT, it is well known that residual stress in weld HAZ is one of the reasons for PWHT embitterment. In case of static loading, it was experimentally found that fracture toughness of weld HAZ was dependant upon PWHT conditions. However, the effects of PWHT on fatigue behavior are not clearly verified. Therefore, in this paper, the effects of heating rate PWHT conditions and residual stress simulated in weld HAZ of Cr-Mo steel on fatigue crack propagation behavior were evaluated by fatigue Testing and SEM observation. The obtained results are summarized as follows; 1. Applied stress($10 Kgf/mm^2$) in weld HAZ during PWHT tneded to decrease fatigue strength and to increase fatigue crack growth rate. 2. Applied stress and slow heating rate of 60.deg. C/hr during PWHT contributed to precipitin of impurity elements as well as carbide, which promoted the fatigue crack growth. 3. Fatigue crack growth rate decreased at the heating rate of 220.deg. C/hr in contrast with 600.deg. C/hr and 60.deg. C/hr.

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피로균열 성장과정에 대한 평가방법의 영향 (Influence of Evaluation Methods for Fatigue Crack Growth Process)

  • 안철봉
    • 한국생산제조학회지
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    • 제8권1호
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    • pp.119-125
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    • 1999
  • The distribution of fatigue crack growth rate is subjected to the measuring interval and calculated method of growth rate. In this paper, in order to establish the method of determining the distribution of fatigue crack growth rate, which ignores those influences, a series of fatigue crack growth experiments and measuring intervals of crack length calculated reasonable are presented. The main conclusions obtained are summarized as follows: 1) As a result of the ΔP constant test and ΔK constant test, it is thought that an approximate measuring interval of 0.3~0.7mm is reasonable, which allows for few errors and is little subjected to the calculated method of crack growth rate. 2) After generally comparing the error estimation by using the experimental data of CCT specimen with the error rating of the CT specimens, it is possible that the fatigue test has few errors within the measuring interval, ξ(Δa/W)=0.0067~0.017, regardless of the dimension of specimen geometry.

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고출력 CW Nd:YAG 레이저를 이용한 인코넬 600의 용접 특성 (Welding Characteristics of Inconel 600 using a high power CW Nd:YAG Laser)

  • 유영태;신호준;임기건
    • 한국공작기계학회논문집
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    • 제13권6호
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    • pp.119-126
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    • 2004
  • The welding characteristics of Inconel 600 Alloy using a continuous wave Nd:YAG laser are experimentally investigated. The major process parameters studied in the present laser welding experiment were the positions of focus, laser power and travel speed of laser bean We measured the fusion zone size and its shape using an optical microscope for the observation of cross-sectional area. We performed two tests regarding the tension and the micro hardness for welding quality estimation. Then we measured residual stress in welds by electronic speckle pattern interferometry(ESPI). In conclusion the optimum butt welding process parameters were 0.5mm focus position, 1.6kW laser power, 1m/min travel speed and 5.5$\ell$/min assist gas discharge.

알루미늄 합금 피로 스트라이에이션의 나노 스케일 관찰 (Nano-Scale Observation of Fatigue Striations for Aluminum Alloy)

  • 최성종;권재도
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집A
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    • pp.153-158
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    • 2000
  • Atomic Force Microscope (AFM) was used to study cross sectional profiles and dimensions of fatigue striations in 2017-T351 aluminum alloy. Their widths (SW) and heights $(SH,\;SH_h)$ were measured from the cross sectional Profiles of three-dimension AFM images. The following results that will be helpful to understand the fatigue crack growth mechanism were obtained. (1) Coincidence of the crack growth rate with the striation width was found down to the growth rate of $10^{-5}$ mm/cycle. (2) The relation of $SH={\alpha}(SW)^{1.2}$ was obtained. (3) The ratio of the striation height to its width SH/SW and did not depend on the stress intensity factor range ${\Delta}K$ and the stress ratio R. From these results, the applicability of the AFM to nano-fractography is discussed.

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열 필라멘트 CVD법에 의해서 제작한 다이아몬드 막의 잔류응력제어 (Control of Residual Stress in Diamond Film Fabricated by Hot Filament CVD)

  • 최시경;정대영;최한메
    • 한국세라믹학회지
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    • 제32권7호
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    • pp.793-798
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    • 1995
  • The relaxation of the intrinsic stresses in the diamond films fabricated by the hot filament CVD was studied, and it was confirmed that the tensile intrinsic stresses in the films could be controlled without any degradation in the quality of the diamond films. The tensile intrinsic stresses in the films decreased from 2.97 to 1.42 GPa when the substrate thickness increased from 1 to 10mm. This result showed that the residual stress was affected by the substrate thickness as well as by the interaction between grains. Applying of +50 V between the W filament and the Si substrate during deposition, the tensile intrinsic stress in the film deposited at 0 V was decreased from 2.40 GPa to 0.71 GPa. Such large decrease in the tensile intrinsic stress was due to $\beta$-SiC which acted as a buffer layer for the stress relaxation. However, the application of the large voltage above +200V resulted in the change of quality of the diamond film, and nearly had no effect on relaxation in the tensile intrinsic stress.

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차체의 종류별 로어암 형상의 변화에 따른 내구성 향상에 관한 연구 (Durability Improvement due to the Change of Lower Arm by the Class of Automotive Body)

  • 한문식;조재웅
    • 한국기계가공학회지
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    • 제16권6호
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    • pp.29-34
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    • 2017
  • This study analyzed automobile lower arm assembly structure and fatigue to identify configuration changes to enhance structural safety. Parts connected to the car body were fixed and 500 N load was applied at the lower arm head. Maximum equivalent stress and maximum total deformation were minimized for model 1 ( MPa and 0.10315 mm, respectively). Fatigue analysis using extreme SAE bracket history fatigue loads showed model 1 also improved fatigue life ($3.3693{\times}10^5cycles$). This study provides important inputs to improve lower arm durability by modifying the arm configuration.