• Title/Summary/Keyword: FCT

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In-X(X=Pb,Sn) 합금의 마르텐사이트변태거동 특성에 관한 연구 (A Study on the Characteristics of Martensitic Transformation Behaviors in In-X(X=Pb,Sn) Alloys)

  • 한창석;한승오
    • 열처리공학회지
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    • 제23권5호
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    • pp.233-238
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    • 2010
  • The phase transformations and the shape memory effect in In-rich Pb alloys and In rich-Sn alloys have been studied by means of X-ray diffractometry supplemented by metallographic observations. The alloys containing 12~15 at.%Pb transform from the ${\alpha}_2$ (fct) phase to the ${\alpha}_1$ (fct) phase by way of an intermediate phase (m phase) on cooling. The results of X-ray diffraction show that the metastable intermediate phase is observed both on cooling and heating, and has a face-centered orthorhombic (fco) structure. It is concluded that the ${\alpha}_1{\rightleftarrows}{\alpha}_2$ transformation is expressed by the ${\alpha}_1{\rightleftarrows}m{\rightleftarrows}{\alpha}_2$ transformation both on usual cooling and heating with the rate more than $8{\times}10^{-3}$ K/s. The $m{\rightleftarrows}{\alpha}_2$ transformation takes place with a mechanism involving macroscopic shear and are of diffusionless (martensitic) type. The temperature hysteresis in the two transformations is 10~13 K between the heating and cooling transformations. The alloys containing 0~11 at.%Sn are -phase solid solutions with a face centered tetragonal structure (c/a > 1) at room temperature, the axial ratio increasing continuously with tin content. The In-(11~15) at.%Sn alloys are mixtures of ${\alpha}$ and ${\beta}$ phases, the ${\beta}$ phase having a f. c. tetragonal structure (c/a < 1). The alloys containing more than 15 at.%Sn are ${\beta}$-phase solid solutions. The In-(12.9~15.0) at.%Sn alloys show a shape memory effect only when quenched to the temperature of liquid nitrogen, although their effect becomes weak and finally disappears after keeping at room temperature for a long time. The ${\beta}{\rightarrow}{\alpha}^{\prime}$ phase transformation is of the diffusionless (martensitic) type, and takes place between 330 K at 12.9 at.%Sn and 150 K at 14.5 at.%Sn. The hysteresis of transformation temperatures on heating and cooling is considerably large (29~40 K), depending on the composition. Both In-Pb and In-Sn alloys showed distinct the shape memory effects.

Mapping the Posterior Ledge and Optic Foramen in Orbital Floor Blowout Fractures

  • Yu Cong Wong;Doreen S.L. Goh;Celine S.Y. Yoong;Cowan Ho;Elijah Z. Cai;Angela Hing;Hanjing Lee;Vigneswaran Nallathamby;Yan L. Yap;Jane Lim;Sundar Gangadhara;Thiam C. Lim
    • Archives of Plastic Surgery
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    • 제50권4호
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    • pp.370-376
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    • 2023
  • Background The posterior ledge (PL) is a vital structure that supports the implant posteriorly during orbital floor reconstruction. This study describes a technique for mapping the PL in relation to the infraorbital margin (IM) in patients with orbital floor blowout fractures. This study establishes the location of the optic foramen in relation to the PL. Methods Facial computed tomography (FCT) scans of 67 consecutive patients with isolated orbital floor blowout fractures were analyzed using Osirix. Planes of reference for orbital fractures, a standardized technique for performing measurements on FCT, was used. Viewed coronally, the orbit was divided into seven equal sagittal slices (L1 laterally to L7 medially) with reference to the midorbital plane. The distances of PL from IM and location of optic foramen were determined. Results The greatest distance to PL is found at L5 (median: 30.1 mm, range: 13.5-37.1 mm). The median and ranges for each slice are as follows: L1 (median: 0.0 mm, range: 0.0-19.9 mm), L2 (median: 0.0 mm, range: 0.0-21.5 mm), L3 (median: 15.8 mm, range: 0.0-31.7 mm), L4 (median: 26.1 mm, range: 0.0-34.0 mm), L5 (median: 30.1 mm, range: 13.5-37.1 mm), L6 (median: 29.0 mm, range: 0.0-36.3 mm), L7 (median: 20.8 mm, range: 0.0-39.2 mm). The median distance of the optic foramen from IM is 43.7 mm (range: 37.0- 49.1) at L7.

Cu-65%Mn 합금의 진동감쇠능 퇴화 및 회복 (A Study on Degradation and Recovery of Damping Capacity in Cu-65%Mn Alloy)

  • 정태신;전중환;이승훈;이영국;최종술
    • 열처리공학회지
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    • 제11권2호
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    • pp.92-98
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    • 1998
  • Degradation and recovery of damping capacity in a Cu-65%Mn alloy have been studied. When the alloy was isothermally aged at $400^{\circ}C$, the highest damping capacity was observed after aging for 4 hours. In case when the alloy aged at $400^{\circ}C$ for 4 hours was maintained at $100^{\circ}C$, the damping capacity gradually decreased with time. The microstructural observations showed that the formation of subdomains and ${\alpha}$-Mn precipitates are responsible for the degradation of damping capacity. When the degraded specimen was reheated at $250^{\circ}C$ for 30 minutes, the damping capacity was recovered considerably owing to the redistribution of impurity atoms, the extinction of subdomains and the release of damping sources from ${\alpha}$-Mn precipitates during the repeated transformation, fcc${\leftrightarrow}$fct.

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배열이용 공기증폭기를 활용한 고효율 연료전지 시스템 (High Efficiency Fuel Cell System with Air Amplifier using Waste Heat)

  • 전재호;최영재;전중환;김선태;김성완
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2010년도 추계학술대회 초록집
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    • pp.72.1-72.1
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    • 2010
  • 지금까지 연료전지 시스템의 효율을 극대화시키기 위한 기술들이 개발되어 왔는데, 대표적인 방법은 CHP(Combined Heat & power)와 FCT(Fuel cell & Turbine) Hybrid 시스템이다. 그러나 본 연구의 기술은 연료전지 배열을 이용한 Coanda 공기증폭기를 장착한 새로운 개념의 고효율 연료전지 시스템이다. 원래 공기 증폭기는 완만한 곡면 주위를 흐르는 유체가 곡면의 표면을 따라 흐름의 방향이 바뀌는 원리(Coanda Effect)를 이용한 장치로서, 소량의 고압유체를 구동 에너지원으로 사용하여 최고 20배에 해당하는 많은 양의 주변 유체를 빠른 속도로 이송시키는 역할을 한다. 문제는 고압의 유체원을 만드는 것인데, 본 연구에서는 발전용 연료전지 시스템의 배기가스를 활용하여 먼저 고압의 수증기를 발생시키고, 다음으로 고압의 수증기를 공기 증폭기의 구동원으로 사용함으로써 연료전지 시스템의 Air blower를 대체하는 것이다. 이러한 개념을 검증하기 위해서 고압의 스팀작동 Coanda 공기증폭기를 제작하여 선행실험을 진행하였다. 먼저 공기증폭기의 Gap 및 스팀압력에 따른 공기유량, 압력 등의 기본특성을 조사하였고, 출력 공기의 특성을 개선하기 공기증폭기의 형상 및 재료를 새롭게 설계하였다. 그리고 실제 시스템의 적용가능성을 알아보기 위해서, 예로 300kW급 용융탄산염 연료전지 발전시스템의 Air blower 대체가능성을 확인하였고, 배열이용 Coanda 공기증폭기를 활용한 고효율 연료전지 시스템의 개념설계를 수립하였다. 결론적으로 본 기술을 활용하면 연료전지 시스템의 최종 전기효율을 향상시킬 뿐 아니라는 시스템의 장기 신뢰성을 증대시키는 효과를 기대할 수 있다.

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Changes in Dietary Guidance: Implications for Food Composition Tables

  • Murphy, Suzanne P.
    • Nutritional Sciences
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    • 제7권2호
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    • pp.88-91
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    • 2004
  • New Dietary Reference Intakes (DRIs) forthe United States and Canada have recently been set for both macronutrients and micronutrients, and are likely to be of interest to health professionals in Korea as well. DRIs are now available for nutrients that did not have Recommended Dietary Allowances set in the past (amino acids, n-3 and n-6 fatty acids, total fiber, added sugar, choline, boron, nickel, and vanadium). Furthermore, the units for the DRIs do not always match those traditionally carried on food composition tables (FCTs). FCT developers will also need to consider carrying new variables to allow the calculation of folate intake in $\mu$g of dietary folate equivalents, vitamin E intake as mg of a-tocopherol (not as mg of a-tocopherol equivalents), and vitamin A intake as $\mu$g of retinol activity equivalents (not as $\mu$g of retinol equivalents). Because the new recommendations for upper levels of intake sometimes refer to a specific form or source of a nutrient, nutrients occurring in foods must be separated from added or supplemental forms for vitamin E, niacin, and folate; pharmacological magnesium must be carried as a separate variable; and preformed vitamin A must be separated from vitamin A from carotenoids. For more information on the DRIs, see: www.nap.edu.

Lateral-torsional buckling of prismatic and tapered thin-walled open beams: assessing the influence of pre-buckling deflections

  • Andrade, A.;Camotim, D.
    • Steel and Composite Structures
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    • 제4권4호
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    • pp.281-301
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    • 2004
  • The paper begins by presenting a unified variational approach to the lateral-torsional buckling (LTB) analysis of doubly symmetric prismatic and tapered thin-walled beams with open cross-sections, which accounts for the influence of the pre-buckling deflections. This approach (i) extends the kinematical assumptions usually adopted for prismatic beams, (ii) consistently uses shell membrane theory in general coordinates and (iii) adopts Trefftz's criterion to perform the bifurcation analysis. The proposed formulation is then applied to investigate the influence of the pre-buckling deflections on the LTB behaviour of prismatic and web-tapered I-section simply supported beams and cantilevers. After establishing an interesting analytical result, valid for prismatic members with shear centre loading, several elastic critical moments/loads are presented, discussed and, when possible, also compared with values reported in the literature. These numerical results, which are obtained by means of the Rayleigh-Ritz method, (i) highlight the qualitative differences existing between the LTB behaviours of simply supported beams and cantilevers and (ii) illustrate how the influence of the pre-buckling deflections on LTB is affected by a number of factors, namely ($ii_1$) the minor-to-major inertia ratio, ($ii_2$) the beam length, ($ii_3$) the location of the load point of application and ($ii_4$) the bending moment diagram shape.

제트 확산화염의 연소특성과 매연생성에 관한 연구 (Combustion Characteristics and Soot Formation in a Jet Diffusion Flame)

  • 이교우;백승욱
    • 대한기계학회논문집
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    • 제18권10호
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    • pp.2712-2723
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    • 1994
  • Numerical simulation of an axisymmetric ethylene-air jet diffusion flame has been carried out in order to investigate flame dynamics and soot formation. The model solves the time-dependent Navier-Stokes equations and includes models for soot formation, chemical reaction, molecular diffusion, thermal conduction, and radiation. Numerically FCT(Flux Corrected Transport) and DOM(Discrete Ordinate Method) methos are used for convection and radiation trasport respectively. Simulation was conducted for a 5 cm/sec fuel jet flowing into a coflowing air stream. The maximum flame temperature was found to be approximately 2100 K, and was located at an axial position of approximately 5 cm from the base of the flame. The maximum soot volume fraction was about $7{\times}10^{-7}$, and was located within the high temperature region where the fuel mole fraction ranges from 0.01 to 0.1. The buoyancy-driven low-frequency(12~13 Hz) structures convected along the outer region of the flame were captured. In case without radiation trasport, the maximum temperature was higher by 150 K than in case with radiation. Also the maximum soot volume fraction reached about $8{\times}10^{-6}$. As the the hydrocarbon fuel forms many soot particles, the radiation transport becomes to play a more important role.

Effects of Healing Agent on Crack Propagation Behavior in Thermal Barrier Coatings

  • Jeon, Soo-Hyeok;Jung, Sung-Hoon;Jung, Yeon-Gil
    • 한국세라믹학회지
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    • 제54권6호
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    • pp.492-498
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    • 2017
  • A thermal barrier coating (TBC) with self-healing property for cracks was proposed to improve reliability during gas turbine operation, including structural design. Effect of healing agent on crack propagation behavior in TBCs with and without buffer layer was investigated through furnace cyclic test (FCT). Molybdenum disilicide ($MoSi_2$) was used as the healing agent; it was encapsulated using a mixture of tetraethyl orthosilicate and sodium methoxide. Buffer layers with composition ratios of 90 : 10 and 80 : 20 wt%, using yttria stabilized zirconia and $MoSi_2$, respectively, were prepared by air plasma spray process. After generating artificial cracks in TBC samples by using Vickers indentation, FCTs were conducted at $1100^{\circ}C$ for a dwell time of 40 min., followed by natural air cooling for 20 min. at room temperature. The cracks were healed in the buffer layer with the healing agent of $MoSi_2$, and it was found that the thermal reliability of TBC can be enhanced by introducing the buffer layer with healing agent in the top coat.

Structural and Magnetic Properties of $FePt-B_x\;at.\%$ (X=5, 10, 15, 25 and 33) thin Film by Post-Annealing

  • Lee Young-min;Lee Byeong-Seon;Lee Chan-Gyu;Koo Bon-Heun;Shimada Y.;Kitakami O.;Okamoto S.;Miyazaki T.
    • 한국자기학회:학술대회 개요집
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    • 한국자기학회 2005년도 동계학술연구발표회 및 2차 아시안포럼
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    • pp.154-155
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    • 2005
  • Multi-layer film of $MgO/(FePt-B)_{50nm}/ MgO$ was deposited on Si(100) substrates by RF magnetron sputtering. The boron chips were uniformly placed oil tile FePt target. The boron content of thin film was found to be about 5, 10, 15, 25 and $33 at\%$ by using a CAMECA SX-51 wavelength dispersive spectroscopy (WDX). It is observed that X-ray diffraction patterns of FePt-B film by post-annealing exhibited a transformation from disordered fcc structure to ordered $Ll_0$ phase with fct structure from around $400^{\circ}C$. By adding B, annealing temperature for ordering is about $200^{\circ}C$ lower than that of pure FePt. This remarkable decrease of the annealing temperature is closely related to the high diffusivities of Fe and Pt associated with the defects caused by movements of B atoms. The maximum coercivity(Hc) for FePt films was found to be ${\~}$13 kOe after annealing at $600^{\circ}C$ for 1hr.

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FePt/MgO(100) 자성박막의 결정화 연구 (Crystallization of FePt/MgO(100) magnetic thin films)

  • 정지욱;조태식;이민수
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2005년도 하계학술대회 논문집 Vol.6
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    • pp.278-279
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    • 2005
  • The crystallization of FePt/MgO(100) magnetic thin films of various thicknesses has been studied using synchrotron x-ray scattering, atomic force microscope, and vibrating sample magnetometer. In film with a 500-${\AA}$-thick, ordered (fct) FePt phase was dominantly crystallized into perpendicular (001) grains keeping the magnetically easy c-axis normal to the film plane during annealing. In film with a 812-${\AA}$-thick, however, longitudinal (110) grains keeping the c-axis parallel to the film plane were grown on top of the perpendicular (001) grains. The behavior of the magnetic properties was consistent with the thickness dependence of the crystallization. We attribute the thickness dependence of the crystallization to the substrate effect, which prefers the growth of the c-axis oriented perpendicular grains near the film/substrate interfacial area.

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