• 제목/요약/키워드: Micro-jet Engine

검색결과 24건 처리시간 0.02초

고온선박엔진용 MoSi$_2$금속간화합물의 경도와 방전가공특성 (Hardness and EDM Processing of MoSi$_2$Intermetallics for High Temperature Ship Engine)

  • 윤한기;이상필
    • 한국해양공학회지
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    • 제16권6호
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    • pp.60-64
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    • 2002
  • This paper describes the machining characteristics of the MoSi$_2$--based composites through the process of electric discharge drilling with various tubular electrodes. In addition to hardness characteristics, microstructures of Nb/MoSi$_2$laminate composites were evaluated from the variation of fabricating conditions, such as preparation temperature, applied pressure, and pressure holding time. MoSi$_2$-based composites have been developed in new materials for jet engines of supersonic-speed airplanes and gas turbines for high-temperature generators. These high performance engines may require new hard materials with high strength and high temperature-resistance. Also, with the exception of grinding, traditional machining methods are not applicable to these new materials. Electric discharge machining (EDM) is a thermal process that utilizes a spark discharge to melt a conductive material. The tool electrode is almost -unloaded, because there is n direct contact between the tool electrode and the work piece. By combining a non-conducting ceramic with more conducting ceramic, it was possible to raise the electrical conductivity. From experimental results, it was found that the lamination from Nb sheet and MoSi$_2$ powder was an excellent strategy to improve hardness characteristics of monolithic MoSi$_2$. However, interfacial reaction products, like (Nb, Mo)SiO$_2$and Nb$_2$Si$_3$formed at the interface of Nb/MoSi$_2$, and increased with fabricating temperature. MoSi$_2$composites, with which a hole drilling was not possible through the conventional machining process, enhanced the capacity of ED-drilling by adding MbSi$_2$, relative to that of SiC or ZrO$_2$reinforcements.

의치상용 자가중합레진의 중합조건에 따른 파괴인성 (FRACTURE TOUGHNESS OF SELF-CURING DENTURE BASE RESINS WITH DIFFERENT POLYMERIZING CONDITIONS)

  • 정수양;김지혜;양병덕;박주미;송광엽
    • 대한치과보철학회지
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    • 제43권1호
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    • pp.52-60
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    • 2005
  • Purpose. The intent of this study was to evaluate the effects of curing conditions on self-curing denture base resins to find out proper condition in self-curing resin polymerization. Materials and methods, In this study, 3 commercial self-curing denture base resins are used Vertex SC, Tokuso Rebase and Jet Denture Repair Acrylic. After mixing the self curing resin, it was placed in a stainless steel mold(3$\times$6$\times$60mm). The mold containing the resin was placed under the following conditions: in air at 23$^{\circ}C$; or in water at 23$^{\circ}C$; or in water at 23$^{\circ}C$ under pressure(20psi); or in water at 37$^{\circ}C$ under pressure(20psi) or in water at 50$^{\circ}C$ under pressure(20psi) , or in water at 65$^{\circ}C$ under pressure(20psi), respectively. Also heat-curing denture base resin is polymerized according to manufactures' instructions as control. Fracture toughness was measured by a single edge notched beam(SENB) method. Notch about 3mm deep was carved at the center of the long axis of the specimen using a dental diamond disk driven by a dental micro engine. The flexural test was carried out at a crosshead speed 0.5mm/min and fracture surface were observed under measuring microscope. Results and conclusion . The results obtained were summarized as follows : 1. The fracture toughness value of self-curing denture base resins were relatively lower than that of heat-curing denture base resin. 2. In Vertex SC and Jet Denture Repair Acrylic, higher fracture toughness value was observed in the curing environment with pressure but in Tokuso Rebase, low fracture toughness value was observed but there was no statistical difference. 3. Higher fracture toughness value was observed in the curing environment with water than air but there was no statistical difference. 4. Raising the temperature in water showed the increase of fracture toughness.

$MoSi_2$ 금속간화합물 복합재료의 미세구조와 방전가공특성 (Microstructure and EDM Processing of $MoSi_2$ Intermetallic Composite)

  • 윤한기;이상필;윤경욱;김동현
    • 한국해양공학회:학술대회논문집
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    • 한국해양공학회 2002년도 춘계학술대회 논문집
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    • pp.23-28
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    • 2002
  • This paper describes the machining characteristics of the $MoSi_2$ based composites by electric discharge drilling with various tubular electrodes, besides, Hardness characteristics and microstructures of $Nb/MoSi_2$ laminate composites were evaluated from the variation of fabricating conditions such as preparation temperature, applied pressure and pressure holding time. $MoSi_2$ -based composites has been developed in new materials for jet engine of supersonic-speed airplanes and gas turbine for high- temperature generator. Achieving this objective may require new hard materials with high strength and high temperature-resistance. However, With the exception of grinding, traditional machining methods are not applicable to these new materials. Electric discharge machining (EDM) is a thermal process that utilizes a spark discharge to melt a conductive material, the tool electrode being almost non-unloaded, because there is no direct contact between the tool electrode and the workpiece. By combining a nonconducting ceramics with more conducting ceramic it was possible to raise the electrical conductivity. From experimental results, it was found that the lamination from Nb sheet and $MoSi_2$ powder was an excellent strategy to improve hardness characteristics of monolithic $MoSi_2$. However, interfacial reaction products like (Nb, Mo)$SiO_2$ and $Nb_2Si_3$ formed at the interface of $Nb/MoSi_2$ and increased with fabricating temperature. $MoSi_2$ composites which a hole drilling was not possible by the conventional machining process, enhanced the capacity of ED-drilling by adding $NbSi_2$ relative to that of SiC or $ZrO_2$ reinforcements.

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선박용 디젤엔진 SCR 시스템 요소 기술에 관한 기초 연구 (Preliminary Study on Factor Technology of Selective Catalytic Reduction System in Marine Diesel Engine)

  • 박윤용;송하철;안기주;심천식
    • 한국항해항만학회지
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    • 제40권4호
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    • pp.173-181
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    • 2016
  • 2016년부터 배출통제지역(ECA : Emission Control Atea)을 운항하는 선박에 대하여 배출되는 NOx(질소산화물) 및 SOx(황산화물)의 배기량 감소규제가 강화되었다. 상기의 규제 물질 중 NOx를 제거하는 탈질장비 중 선택적 촉매 환원(SCR : Selectivity Catalytic Reduction) 시스템은 효율이 높고 상업적으로 많이 활용되고 있으나, 높은 온도에서 요소수가 활성화되는 단점이 있다. 이에 초미세기포를 이용하여 낮은 온도에서도 반응할 수 있는 요소수 및 요소수 활성화 기기를 개발하여 상기의 문제점들을 최소화 할 수 있도록 하였다. 또한 SCR 시스템의 효율성을 향상시키는 방안을 마련하기 위하여, ANSYS-CFX package를 이용한 전산유체역학(CFD : Computational fluid dynamics)기법을 사용하였다. Navier-Stokes 방정식을 해석의 지배방정식으로 적용하여 SCR 시스템의 점성유동해석 시뮬레이션을 수행하였다. SCR 시스템의 형상은 CATIA V5를 사용하여 3D 모델링을 하였고, SCR 시스템의 효율성을 비교하기 위해 요소수 분사 노즐의 위치를 요소수 분사 노즐은 배기관의 입구로부터 1/3, 1/2, 2/3로 변경하며 확인하였다. 또한, 노즐의 분사구 수가 SCR 시스템의 효율에 미치는 영향을 확인하기 위하여 분사구 수가 4, 6, 8개일 경우를 시뮬레이션 하여 비교 분석하였다. 시뮬레이션 결과 배기관 입구에 가까울수록, 분사구 수가 많을수록 효율이 향상됨을 확인하였다.