• 제목/요약/키워드: n-well thickness

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다층 구조에 대한 새로운 strain 해석 모델 (A new strain analysis model in epitaxial multilayer system)

  • 장동현;심종인
    • 한국광학회:학술대회논문집
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    • 한국광학회 2007년도 하계학술발표회 논문집
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    • pp.237-238
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    • 2007
  • A new strain analysis model, so called the stress matched model, in an epitaxial multilayer system is proposed. The model makes it possible to know the strain, the stress, the elastic strain energy in each epitaxial layer. Analytical formulas of strain parameters in each epitaxial layer are derived under assumptions that the substrate thickness is finite and the in-plane lattice constant is the same for all epitaxial layers for dislocation free growth. As an example, the model is applied to a 405nm InGaN/InGaN multiple quantum well laser diode. Analysis result shows that AlxGa1-xN layer with Al mole fraction of 0.06 and the thickness of 6${\mu}m$ is one of good templates for a laser. In fact, this layer structure coincides with experimentally optimized one.

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A Study on the Fabrication and Structural Properties of Al-Co/AlN-Co Thin Films

  • Han, Chang-Suk;Han, Seung-Oh
    • 대한금속재료학회지
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    • 제49권3호
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    • pp.256-263
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    • 2011
  • We have synthesized Al-Co/AlN-Co multilayer films with different layer thicknesses by using a Two-Facing Target Type dc Sputtering (TFTS) system. The deposited films were annealed isothermally at different temperatures and their microstructure, magnetic properties and resistivity were investigated. The magnetization of the as-deposited films was found to be very small, irrespective of layer thickness. It was found that the annealing conditions and layer thickness ratio of Al-Co to AlN-Co (LTR) were able to control the microstructure, as well as the physical properties of the prepared films. The resistivity and magnetization increased and the coercivity decreased with a decreasing LTR. A high resistivity of 2500 ${\mu}{\Omega}-cm$, a magnetization of 360 $emu/cm^3$, and a coercivity of 5 Oe were obtained for the films with LTR=0.175.

피로균열진전에 미치는 시편 두께의 영향 (Effect of Specimen Thickness on Fatigue Crack Growth)

  • 김재훈;김영균;윤인수
    • 한국안전학회지
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    • 제13권4호
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    • pp.79-86
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    • 1998
  • The effect of specimen thickness on fatigue crack growth behavior has been carried out by compact tension specimens of thickness of 3mm, 10mm and 25mm for maraging steel and Al 7075-T6. The closure points were determined during the test by means of a clip-gage situated at the notch mouth. Specimen thickness have no apparent influence on the fatigue crack growth rate of maraging steel, but the crack growth rate of 25mm thickness specimen for Al 7075-T6 is faster than that of 3 and 10mm specimens. The difference of crack growth rates can be successfully explained by considering the different stress state of plane strain and plain stress due to the variation of specimen thickness. Also the crack opening ratio of 25mm specimen is greater than those of 3 and 10mm specimens. When a side groove is introduced in a 10mm specimen, the crack growth rate is approximately similar to that of 25mm specimen. The effective thickness expression of $B_e=B_o-(B_o-B_N)^2B_o$ is the most appropriate to evaluate the crack growth rate of side-grooved specimen. Fatigue crack growth rates can be well described by $\Delta K_{eff}$ of the crack closure points in regardless of all thickness and side-grooved specimens.

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Co/Ti 이중막 실리사이드 접촉을 갖는 p$^{+}$-n 극저접합의 형성 (Formation of p$^{+}$-n ultra shallow junction with Co/Ti bilayer silicide contact)

  • 장지근;엄우용;신철상;장호정
    • 전자공학회논문지D
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    • 제35D권5호
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    • pp.87-92
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    • 1998
  • Ultr shallow p$^{+}$-n junction with Co/Ti bilayer silicidde contact was formed by ion implantation of BF$_{2}$ [energy : (30, 50)keV, dose:($5{\times}10^{14}$, $5{\times}10^{15}$/$\textrm{cm}^2$] onto the n-well Si(100) region and by RTA-silicidation and post annealing of the evaporated Co(120.angs., 170.angs.)/Ti(40~50.angs.) double layer. The sheet resistance of the silicided p$^{+}$ region of the p$^{+}$-n junction formed by BF2 implantation with energy of 30keV and dose of $5{\times}10^{15}$/$\textrm{cm}^2$ and Co/Ti thickness of $120{\AA}$/(40~$50{\AA}$) was about $8{\Omega}$/${\box}$. The junction depth including silicide thickness of about $500{\AA}$ was 0.14${\mu}$. The fabricated p$^{+}$ -n ultra shallow junction depth including silicide thickness of about $500{\AA}$ was 0.14${\mu}$. The fabricated p$^{+}$-n ultra shallow junction with Co/Ti bilayer silicide contact did not show any agglomeration or variation of sheet resistance value after post annealing at $850^{\circ}C$ for 30 minutes. The boron concentration at the epitaxial CoSi$_{2}$/Si interface of the fabricated junction was about 6*10$6{\times}10^{19}$ / $\textrm{cm}^2$./TEX>.

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Effect of growth interruption on InN/GaN single quantum well structures

  • Kwon, S.Y.;Kim, H.J.;Na, H.;Seo, H.C.;Kim, H.J.;Shin, Y.;Kim, Y.W.;Yoon, S.;Oh, H.J.;Sone, C.;Park, Y.;Sun, Y.P.;Cho, Y.H;Cheong, H.M.;Yoon, E.
    • 한국진공학회지
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    • 제12권S1호
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    • pp.95-99
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    • 2003
  • We successfully grew InN/GaN single quantum well structures by metal-organic chemical vapor deposition and confirmed their formation by optical and structural measurements. We speculate that relatively high growth temperature ($730^{\circ}C$) of InN layer enhanced the formation of 2-dimensional quantum well structures, presumably due to high adatom mobility. As the growth interruption time increased, the PL emission efficiency from InN layer improved with peak position blue-shifted and the dislocation density decreased by one order of magnitude. The high resolution cross-sectional TEM images clearly showed that the InN layer thickness reduced from 2.5 nm (without GI) to about I urn (with 10 sec GI) and the InN/GaN interface became very flat with 10 sec GI. We suggest that decomposition and mass transport processes on InN during GI is responsible for these phenomena.

Application of Patient-Specific 3D-Printed Orthopedic Splint for Bone Fracture in Small Breed Dogs

  • Kwangsik Jang;Eun Joo Jang;Yo Han Min;Kyung Mi Shim;Chunsik Bae;Seong Soo Kang;Se Eun Kim
    • 한국임상수의학회지
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    • 제40권4호
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    • pp.268-275
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    • 2023
  • In this paper, we designed 3D-printed orthopedic splint models for patient-specific external coaptation on fracture healing and analyzed the stability of the models through finite element method (FEM) analysis under compressive load conditions. Polylactic acid (PLA) and acrylonitrile-butadiene-styrene (ABS) based 3D splint models of the thicknesses 1, 3, 5 and 7 mm were designed, and Peak von Mises stress (PVMS) and maximum displacement (MD) of the models were analyzed by FEM under compressive loads of 50, 100, 150, and 200 N. The FEM results indicated that PVMS and MD values, regardless of material, had a negative correlation with the thickness of the models and a positive correlation with the compressive load. There was a risk of splint deformation under conditions more extreme than 100 N with 5 mm thickness. For successful clinical application of 3D-printed orthopedic splints in veterinary medicine, it is recommended that the splint should be produced not less than 5 mm thickness. Also, it is expected to be stable when the splint is applied to situations with a compressive load of 100 N or less. There is an advantage of overcoming the limitations of the existing bandage method through 3D-printing technology as well as verifying the stability through 3D modeling before application. Such 3D printing technology will be widely used in veterinary medicine and various fields as well as orthopedics.

고저 접합 에미터 구조를 갖는 $N^+NPP^+$ Si 태양전지의 효율 개선 (Efficiency Improvement of $N^+NPP^+$ Si Solar Cell with High Low Junction Emitter Structure)

  • 장지근;김봉렬
    • 대한전자공학회논문지
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    • 제21권1호
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    • pp.62-70
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    • 1984
  • 비저항이 10Ω-cm, 두께가 13∼15mi1인 <111> oriented, p형 Si기판을 이용하여 N+PP+ BSF 전지와 에미터 영역이 N+N 고저 접합으로 이루어진 N+NPP+ HELEBSF(high low emitter bach surface field) 전지를 설계 제작하였다. 접합형 태양전지의 에미터 영역에서 고저 접합구조가 효율 개선에 미치는 영향을 검토하기 위해 HLEBSF 전지의 N영역을 제외하고는 같은 마스크와 동시 공정을 통해 N+PP-전지와 N+NPP+ 전지의 가영역에서 물리적 파라미터들(불순물 농도, 두께)을 동일하게 만들었다. 100mW/㎠의 인공조명에서 측정한 결과 N+PP+ 전지들의 전면적 (유효 수광면적) 평균 변환효율이 10.94%(12.16%)이었고, N+NPP+ 전지들의 평균 변환효율은 12.07% (13.41%)로 나타났다. N+NPP+ 전지의 효율개선은 N+N-고저 접합 에미터 구조가 N+ 에미터 영역에서 나타나는 heavy doping effects를 제거함으로써 에미터 재결합 전류의 증가를 억제하고 나아가 개방전압(Voc)과 단락전류(Ish)의 값을 증가시켜 준 결과로 볼 수 있다.

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측면홈 시험편을 이용한 평면 변형률 피로 균열 진전에 관한 연구 (Investigation of Plane Strain Fatigue Crack Growth Behavior by Using Side-Grooved Specimens)

  • 김종한;송지호
    • 대한기계학회논문집
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    • 제16권1호
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    • pp.63-69
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    • 1992
  • 본 연구에서는 특히 앞서 지적한 표면균열의 진전거동에 관한 연구와도 관련 하여 측면홈을 가진 중앙관통균열(side-grooved center cracked tension) 시험편에 대 해 피로균열 진전실험을 수행하고, 평면변형률 조건의 만족여부 및 응력강도계수 평가 방법에 관하여 검토하여 비교적 새로운 결과를 얻었으므로 여기에 보고하고자 한다.

Four New Species of the Genus Hyattella (Dictyoceratida: Spongiidae) from Korea

  • Sim, Chung Ja;Lee, Kyung Jin
    • Animal Systematics, Evolution and Diversity
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    • 제30권1호
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    • pp.16-21
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    • 2014
  • Four new species of the genus Hyattella (Dictyoceratida: Spongiidae); H. sinchangensis n. sp., H. mara n. sp., H. chuja n. sp. and H. lendenfeldi n. sp., were collected from Jeollanam-do and Jeju-do, Korea. Hyattella sinchangensis n. sp., H. mara n. sp., H. chuja n. sp. and H. grobosa Lendenfeld, 1889 are very similar to each other in some characters. However, Hyattella sinchangensis n. sp. characterized by no special dermal lamella and no tertiary fibres, and more thin secondary fibres than H. globosa. Hyattella mara n. sp. is differs in having well developed dermal lamella, slightly fasciculated primary fibres, and thick tertiary fibres. Hyattella chuja n. sp. differs in surface characters with a slightly elevated part, skeleton with abundant spongine, and very complex meshes. Hyattella lendenfeldi n. sp. is similar to H. tenella (Lendenfeld, 1889) in skeletal structure, thickness of primary and secondary fibres, but differs in growth form.

Experimental study on the fatigue performance of aluminum foam sandwich with 304 stainless steel face-sheet

  • Yan, Chang;Jing, Chuanhe;Song, Xuding
    • Steel and Composite Structures
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    • 제39권3호
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    • pp.229-241
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    • 2021
  • This work focused on aluminum foam sandwich (AFS) with different foam core densities and different face-sheet thicknesses subjected to constant amplitude three-point bending cyclic loading to study its fatigue performance. The experiments were conducted out by a high frequency fatigue test machine named GPS-100. The experimental results showed that the fatigue life of AFS decreased with the increasing loading level and the structure was sensitive to cyclic loading, especially when the loading level was under 20%. S-N curves of nine groups of AFS specimens were obtained and the fatigue life of AFS followed three-parameter lognormal distribution well. AFS under low cyclic loading showed pronounced cyclic hardening and the static strength after fatigue test increased. For the same loading level, effects of foam core density and face-sheet thickness on the fatigue life of AFS structure were trade-off and for the same loading value, the fatigue life of AFS increased with aluminum foam core density or face-sheet thickness monotonously. Core shear was the main failure mode in the present study.