• 항공우주기술
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• 제4권1호
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• pp.196-202
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• 2005

액체추진기관의 극저온 추진제 공급부에서 추진제의 주입 후 대기시간 동안의 온도상승은 배관내의 geysering 현상 및, 점화시 터보펌프에서의 cavitation을 발생시킬 수 있다. 본 자료에서는 이런 문제를 해결하는 방법 중 하나인 재순환배관 방식에 대하여 KSLV-I 예비안의 산화제부 형상을 바탕으로 LOX를 산화제로 사용한 경우에 있어서 그 성능을 파악하였다. 또한, 다양한 parametric study를 통하여 재순환배관의 설계인자를 찾고자 하였다. 재순환배관의 직경, 초기 LOX 온도, 재순환배관 높이, ullage 압력, 열전달 계수 등의 변화에 의한 영향 및 추가적인 He 분사를 통한 순환 촉진 효과를 살펴보았다. 상용 열유체해석프로그램인 SINDA/FLUINT를 사용하였고 1차원적으로 해석을 수행하였다.

• 동력기계공학회지
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• 제17권3호
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• pp.17-22
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• 2013

Diesel particulate filter has been adopted in new vehicle with diesel engine. Since the flow of exhaust gas was clogged as particulate matters were deposited in the filter, it have bad effects on a fuel consumption and power. It was investigated that a particulate filtering system with vacuum pump in the exhaust gas line could be free from clogging in previous research. In this study, the effects of water injection and position of inlet port in filtering system on reducing in particulate matter were investigated. It was noticed that particulate matter were decreased remarkable by water injection and moving the position of inlet port.

• 한국유체기계학회 논문집
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• 제5권4호
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• pp.11-18
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• 2002

A turbopump system composed of two pumps and one turbine is considered. The turbine composed of a nozzle and a rotor is used to drive the pumps while gas passes through the nozzle and potential energy is converted to kinetic energy, which forces the rotor blades to spin. In this study, an aerodynamic design of turbine system is investigated with some pre-determined design requirements (i.e., pressure ratio, rotational speed, required power, etc.) following Liquid Rocket Engine (L.R.E.) system specifications. For simplicity of turbine system, impulse-type rotor blades for open-type L.R.E. have been chosen. Usually, the open-type turbine system requires low mass flow-rate compared to close-type system. In this study, a partial admission nozzle is adopted to maximize the efficiency of the open-type turbine system. A design methodology of turbine system was introduced. Especially, partial admission nozzle was designed by means of simple empirical correlations between efficiency and configuration of the nozzle. Finally, a turbine system design is presented for a 10 ton thrust level of L.R.E.

• 융복합기술연구소 논문집
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• 제3권1호
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• pp.15-18
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• 2013

The next generation alternative fuel of diesel, DME (Dimethyl Ether) discharges particulate matter hardly due to chemical structural as oxygen-fuel so it has the eco-friendly property. Despite these advantages, the DME has the technical difficulties to apply to the diesel engine because of a low calorific value, viscosity and compressibility effects. From this point of view, we performed experimental studies on improved reliability of DME common-rail vehicle and lubricity enhancement of DME fuel for empirical distribution of eco-friendly DME fuel. Also we analyzed solubility of lubrication enhancer according to a drop in temperature, try to secure reliability about core parts of DME vehicle by applying lubrication enhancer in the DME common-rail vehicle.

• 한국해양공학회지
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• 제23권5호
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• pp.39-44
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• 2009

The hydrostatic slipper bearing is generally used in high pressure axial piston pumps to support the load generated from two surfaces which are sliding relatively at low speed. The object of the bearing is to remove the possibility of direct contact by maintenance of an adequate oil film thickness between two metal surfaces. Because the bearing performance is influenced by the bearing deformation, it is highly dependent on the injection pressure, the bearing surface profile and so on. In this study, the deformation characteristics of a hydrostatic slipper bearing is investigated according to the injection pressure by the finite element analysis. In the analysis, the special boundary condition to take the fluid-structure interaction (FSI) into account is used on the interactive surface. The results, such as bearing deformation, stress and lifting force, obtained from the fully coupled analysis are compared with those from the single step sequential method.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2000년도 유체기계 연구개발 발표회 논문집
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• pp.145-152
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• 2000

A turbopump system composed of two pumps and one turbine is considered. The turbine composed of a nozzle and a rotor is used to drive the pumps while gas passes through the nozzle, potential energy is converted to kinematic energy, which forces the rotor blades to spin. In this study, an aerodynamic design of turbine system is investigated using compressible fluid dynamic theories with some pre-determined design requirements (i.e., pressure ratio, rotational speed, required power etc.) obtained from liquid rocket engine (L.R.E.) system design. For simplicity of turbine system, impulse-type rotor blades for open type L.R.E. have been chosen. Usually, the open-type turbine system requires low mass flow rate compared to close-type system. In this study, a partial admission nozzle Is adopted to maximize the efficiency of the open-type turbine system. A design methodology of turbine system has been introduced. Especially, partial admission nozzle has been designed by means of simple empirical correlations between efficiency and configuration of the nozzle. Finally, a turbine system design for a 10 ton thrust level of L.R.E is presented.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2012년도 제42회 동계 정기 학술대회 초록집
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• pp.95-95
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• 2012

스터퍼링 기술이 1852년 Grove에 의해서 최초 발견되어 1979년 Chapin에 의해서 planar magnetron cathode 개발로 진공코팅기술의 새로운 영역을 열게 되어 현재까지 디스플레이, 반도체, 태양전지, 광학산업 및 전자부품 등 나노 산업에 필수적으로 적용되고 있다. 스퍼터링 입자는 운동량 전달에 의한 것으로 운동량을 갖는 나노 스퍼터링 입자는 기판에 대한 박막의 부착력이 우수하고 대면적에 균일하고 재현성 있게 성막되는 특징을 갖고 있다. 마그네트론 스퍼터링 기술이 산업에 응용되면서 주로 4분야에서 많은 연구, 개발이 되어져 왔다. 첫째는 타겟의 고순도 및 고밀도화와 더불어 가격이 고가로 됨에 따라 타겟 사용효율의 향상이다. 플라즈마를 발생시키는 캐소드의 자기회로를 1차원, 2차원 및 회전운동을 통해서 사용효율을 향상시키고 있다. 둘째는 기판에 대해서 박막특성이 균일하도록 코팅하는 것이다. 디스플레이에서는 글래스 기판이 대면적으로 됨에 따라서 핸들링이 어려워져 여러 개의 캐소드 자기회로를 선형적으로 이동시켜 박막두께분포를 최적화하며 반응성 가스를 사용해서 균일한 특성의 박막을 제작하는 경우에는 가스분사관과 배기펌프계의 기하학적 위치 및 가스 유동학적 해석이 필요하다. 셋째는 스퍼터링 입자의 이온화로 의한 박막의 특성향상과 반도체 trench의 높은 aspect ratio hole을 채우는 것이다. 이온화 방법으로는 inductively coupled plasma (ICP), microwave amplified (MA), high power impulse (HIPI), hollow cathode magnetron (HCM), self-sustained sputtering 등이 사용되어져 왔으며 최근에는(neutral beam-assisted sputtering (NBAS)에 의한 박막특성향상 방법이 발표되고 있다. 넷째는 플라즈마 및 박막두께 시뮬레이션에 대해서 많은 발표가 되고 있다. 본 발표에서는 상기의 4 분야를 포함한 향후 개발방향에 대해서 소개할 예정이다.

• 한국자동차공학회논문집
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• 제15권3호
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• pp.99-105
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• 2007

Currently, BLDC fuel pump was applied on LPi vehicle using 3rd fuel supply system as liquified phase LPG injection method had already shown better performance than others. Its cost, however, is rather expensive because of drawbacks such as complicated structure, a fault of localization of system. In this work, demonstration system for a developed turbine type fuel pump to replace BLDC system was setup and investigated. This study results that fuel mass flow rate of turbine type pump and injection performance of injector were better compared to BLDC type. Comparing flow rate of summer LPG with that of winter LPG, the flow rate decreased about 25% using winter LPG. Performance applying turbine type LPi fuel pump to engine is confirmed.

• 한국추진공학회지
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• 제9권3호
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• pp.1-9
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• 2005

고성능 로켓엔진의 터보펌프를 구동하기 위한 연료 과농 가스발생기에서 연소 불안정 발생시, 음향 모드 공진주파수를 모사하는 방법을 통하여 모사배관을 결정하였다. 관심 음향모드의 몇 파장만을 모사하여 실제 연소시험에 바로 적용할 수 있는 팎은 길이의 배관도 제시하였다. 가스발생기에서의 연소 불안정을 제어하기 위한 하나의 방안으로, 모사배관의 길이를 변경하여 분사기의 동특성과 연소실의 공진 음향 모드를 서로 분리시킴으로써 상호작용이 일어나지 않게 할 수 있다. 이러한 특성은 연소시 험을 통해 확인되었고, 이를 통하여 비행용 가스발생기의 연소시험과 연소불안정 제어를 위한 한 가지 방안으로서 모사배관을 결정하는 방법을 확립하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회B
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• pp.2910-2915
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• 2008

This paper was investigated the behaviors of the engine and combustion phenomena for various LPG compositions in the semi-return type system, which is not recircurated to LPG tank through furl rail, applied LPi engine during a cold idle condition and including a cold start of the engine. Cyclic HC and NOx emissions were measured at exhaust port to examine their formation mechanical and reduction mechanical with fast response gas analyzers. Various ignition timing is experimented to study the characteristics of combustion phenomena, HC/NOx emissions during fast idle. Also, this study was investigated start delay time, cylinder pressure, HC/NOx emissions, Mass Fraction Burned, starting time to evaluate performance of transient cold startability. Compared to the return type system, the semi-return type system have advantages in point of production cost and equivalent performance of engine starting time and pressure settling time.