• Title/Summary/Keyword: Thermal analysis characteristics

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Analysis of Characteristics of DLC Coating Thin Film in Tungsten Carbide for Production of Medical Thermal-Infrared Lenses

  • Park, Yong-Pil;Kim, Tae-Gon;Cheon, Min-Woo
    • Transactions on Electrical and Electronic Materials
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    • v.15 no.6
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    • pp.344-347
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    • 2014
  • This study was carried out on DLC thin film deposition technology used in infrared optical system production as a method of reducing the shape changes of the molding core and the consequent loss of life. Experiments on the deposition on silicon wafer and tungsten carbide used as a substrate for molding core were conducted at each processing condition using a filtered arc system, and it was found that the surface and mechanical properties were of the greatest quality when the substrate bias voltage of -150 V was used. In addition, it was confirmed that the PV and Ra characteristics were improved by the deposition of the DLC thin film.

A Study on Structural Safety of the Solid Fuel Grain by Hot Flow inside a Hybrid Rocket Combustor (Multi-port 하이브리드 로켓 연소기에서 고온 산화제 유동에 의한 고체연료의 구조적 안전성에 대한 연구)

  • Do, Gyu-Sung;Yoon, Chang-Jin;Kim, Jin-Kon;Moon, Hee-Jang
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.15 no.4
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    • pp.38-44
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    • 2007
  • This paper describes the structural safety of solid fuel in the Hybrid Rocket Motor (HRM). Hybrid rocket combustion has the distinct regression characteristics which include the process of thermal pyrolysis and fuel vaporization. Most of all, this regression characteristics would structurally affect the strength of the fuel having a multi-port configuration, and even may cause the breaking from the fuel grain. This problem would probably influence the performance and operating safety of HRM. Therefore, for the safe operation of HRM, the critical port radius which determines the structurally safe region was discussed from the heat analysis of the solid fuel.

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A Study on the Characteristics of Hydro-reactive Metal Fuel Solid Propellants (수반응 금속연료 고체추진제의 특성연구)

  • Kim, Jun-Hyung;Seo, Tae-Seok;Jung, Jung-Yong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.429-431
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    • 2011
  • The characteristics of hydro-reactive metal fuel(HRF) propellant on motor performances such as specific impulse and chamber temperature were analyzed by thermodynamic calculation methods. The thermal analysis and burning rate experiments of HRF propellants were also carried out for studying effects of metal fuels on combustion properties.

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Natural Gas Combustion Analysis in Power Generation Gas Turbine (발전용 가스터빈 연소기의 천연가스 연소유동 해석)

  • Kim, Tae-Ho;Choi, Jeong-Yeol
    • 한국연소학회:학술대회논문집
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    • 2005.10a
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    • pp.156-161
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    • 2005
  • Two and Three dimensional numerical simulations have been carried out to understand the combustion characteristics of LNG-fueled gas turbine combustor for power generation. Focus of the study was given to the influences of different fuel composition of imported and domestic natural gases with the flow conditions selected from the gas turbine operation data. Reacting flow characteristics of the swirl stabilized natural gas combustor were understood from the comparison of the two-dimensional and three-dimensional results. The thermal influences of different natural gases were very small and the fuel composition and flow rate were considered to be tuned well.

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Analysis of Combustion Flow of LNG-Fueled Gas Turbine Swirl Burner (LNG 연료를 이용한 가스 터빈 연소기의 연소유동 해석)

  • Kim, Tae-Ho;Kang, Ki-Ha;Choi, Jeong-Yeol;Kim, Sung-Chul
    • Journal of the Korean Society of Combustion
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    • v.13 no.3
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    • pp.33-40
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    • 2008
  • Two- and Three- dimensional numerical simulations are carried out to understand the combustion characteristics of LNG-fueled gas turbine combustor for power generation using imported and domestic natural gases. Reacting flow characteristics of the swirl stabilized natural gas combustor were understood from the numerical results with the flow conditions selected from the gas turbine operation data. The thermal influences of different natural gases were very small and the fuel composition and flow rate were considered to be tuned well. The flow structures of the recirculation and combustion region was understood from the comparison of the two- and three-dimensional results. The complexity of the three-dimensional swirl flows inside the gas turbine combustor with multiple swirlers was understood those resulting from the interactions of the stage and pilot burners.

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Synthesis and Characteristics of Polymer Electroluminescent Device Using PPV-Copolymer (PPV-Copolymer를 이용한 고분자 EL소자의 제작 및 특성연구)

  • Kim, H.Y.;Lim, D.J.;Lim, S.B.;Moon, H.D.;Kim, E.O.;Gil, S.K.;Kim, Y.H.
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2002.07b
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    • pp.984-987
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    • 2002
  • In this study, It is to synthesize PPV-copolymer and to make polymer electroluminesence device in single layer of ITO/PPV -copolymer/metal. and then it has been realized basic characteristics for display device through analysis and recognized application possibility by luminous material. PPV-copolymer is used spin coating method and electrode is evaporated of vacuum deposition method by changing materials. The result of experiment, The PPV-copolymer used this study emitted blue color, could be discovered a change of emttion characteristic by electrode material.

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Conceptual Design of Rocket Based Combined Cycle Engine (Rocket Based Combined Cycle Engine의 개념설계 연구)

  • Lee, Yang-Ji;Kang, Sang-Hun;Yang, Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.581-585
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    • 2009
  • In this study, conceptual design of the RBCC (Rocket Based Combined Cycle) engine was performed for the hypersonic propulsion system development. For the flight mission, RBCC engine takes off at sea level and accelerates up to Mach 8 at the altitude of 30km. By the flight speed characteristics, operating pattern of the engine is categorized into 3 modes : Ejector jet (~Mach 3), Ramjet (Mach 3~6), Scramjet (Mach 6~8). According to the engine mode characteristics, RBCC engine design and analysis was performed.

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Comparative dynamic studies of thick laminated composite shells based on higher-order theories

  • Ganapathi, M.;Patel, B.P.;Pawargi, D.S.;Patel, H.G.
    • Structural Engineering and Mechanics
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    • v.13 no.6
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    • pp.695-711
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    • 2002
  • Here, the dynamic response characteristics of thick cross-ply laminated composite cylindrical shells are studied using a higher-order displacement model. The formulation accounts for the nonlinear variation of the in-plane and transverse displacements through the thickness, and abrupt discontinuity in slope of the in-plane displacements at any interface. The effect of inplane and rotary inertia terms is included. The analysis is carried out using finite element approach. The influences of various terms in the higher-order displacement field on the free vibrations, and transient dynamic response characteristics of cylindrical composite shells subjected to thermal and mechanical loads are analyzed.

The Sensing Characteristics of $WO_3$ Thin Films for $NO_x$ Gas Detection with the Change of Deposition Methods (증착방법에 따른 $NO_x$가스 감지용 $WO_3$박막센서의 특성 변화 연구)

  • 김태송;김용범;유광수;성기숙;정형진
    • Journal of the Korean Ceramic Society
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    • v.34 no.4
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    • pp.387-393
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    • 1997
  • In order to apply WO3 thin films to the semiconducting NOx gas sensors as a sensing material, which have been expected to show good electrical properties, such as large sensitivity, rapid responsibility, and high selectivity, the fabrication method and their sensing characteristics were studied. The variations of surface morphologies, crystallographic orientations and crystallinity with the WO3 thin film growing methods thermal evaporation and DC sputtering methods were investigated by using scanning electron microscopy (SEM) and X-ray diffraction(XRD) analysis. As a result of sensitivity (Rgas/Rair) measurements for the 5 ppm NO2 test gas, the sensitivity values were 113 for the sputtered films and 93 for the evaporated films. It was also observed that the recovery rate of a sensing signal after measuring sensitivity was faster in the sputtered films than in the evaporated films.

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Metal work function dependent photoresponse of schottky barrier metal-oxide-field effect transistors(SB MOSFETs) (금속(Al, Cr, Ni)의 일함수를 고려한 쇼트키 장벽 트랜지스터의 전기-광학적 특성)

  • Jung, Ji-Chul;Koo, Sang-Mo
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2010.06a
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    • pp.355-355
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    • 2010
  • We studied the dependence of the performance of schottky barrier metal-oxide-field effect transistors(SB MOSFETs) on the work function of source/drain metals. A strong impact of the various work functions and the light wavelengths on the transistor characteristics is found and explained using experimental data. We used an insulator of a high thickness (100nm) and back gate issues in SOI substrate, subthreshold swing was measured to 300~400[mV/dec] comparing with a ideal subthreshold swing of 60[mV/dec]. Excellent characteristics of Al/Si was demonstrated higher on/off current ratios of ${\sim}10^7$ than others. In addition, extensive photoresponse analysis has been performed using halogen and deuterium light sources(200<$\lambda$<2000nm).

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