• 전기의세계
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• v.43 no.5
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• pp.44-47
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• 1994

자기부상열차의 효율적인 추력제어 및 안전성 높은 운행을 위해서 고성능의 속도/위치 검출 시스템이 중요한 역할을 한다. 일반열차는 바퀴가 선로에 접촉하여 주행하므로 차축의 회전속도를 측정해서 열차의 선로위를 일정한 간격을 두고 부상하여 주행하므로 비접촉식 측정방법을 사용해야만 한다[1-5]. 특히, 고속으로 주행하는 자기부상열차의 속도를 측정하기 위해서는 응답속도가 빠른 센서시스템을 개발하며, 또한 열차주행에 수반되는 자기장의 영향을 극소화하도록 센서시스템을 설계해야만 한다. 본고에서는 전형적인 자기부상열차인 일본의 HSST 시스템(주행속도 100km/h)과 독일의 Transrapid 시스템(주행속도: 400km/h)에 적용되고 있는 속도/위치 검출 시스템의 작동원리를 상세히 설명한다. HSST 시스템은 유도무선(inductive radio system) 방법을 이용하고 Transrapid 시스템은 와전류근접센서(eddy-current proximity sensor)를 이용한다.

• 전기의세계
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• v.39 no.5
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• pp.68-75
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• 1990

급속한 경제발전과 이에 대응한 교통인구의 증가로 운송시스템의 속도 경쟁은 날로 심화되고 있다. 그러나, 기존의 차륜구동 시스템은 본질적으로 궤도와 차륜의 마찰에 의하여 추진력을 얻기 때문에 평균 최대속도 250Km/h(상한 최대속도 350Km/h)수준이며 소음, 진동 등의 많은 문제점이 있다. 이러한 단점을 극복하기 위하여 선진 외국에서는 부상식 열차의 개발에 관심을 표명하여 1960년대 후반부터 열차와 공기부상식 열차에 대한 연구를 병행하였다. 1970년대 중반까지 프랑스, 영국, 미국 등에서 개발이 진행된 공기 부상식 열차는 고속 주행 및 환경 문제 등에 문제점이 많아 실용화에는 이루지 못하고 신교통 시스템에 부분적으로 적용되고 있는 실정이다. 그러나 자기부상 열차는 Power Electronics 및 자기관련 기술의 급속한 발전에 힘입어 현재 실용화 단계에 이르고 있다. 특히 자기부상(Magnetic Levitation : Maglev) 시스템은 레일과의 마찰력에 의해 추진하는 방식이 아니기 때문에 본질적으로 고속성, 무공해, 안정성, 신뢰성, 경제성 그리고 승차감이 뛰어나다. Maglev는 레일 표면에서 자력을 이용해서 약 1.0cm 또는 10cm 가량 부상한 상태에서 주행하기 때문에 외부와의 물리적인 접촉이 필요 없어 마찰에 의한 소음, 공해, 마모 등이 없는 대단히 이상적인 미래의 운송 수단으로 각광을 받고 있다.

• Journal of the Korean Institute of Gas
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• v.14 no.2
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• pp.34-39
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• 2010

Flame propagation velocity is the one of the main mechanism of the stabilization of triple flame. To quantify the triple flame propagation velocity, Bilger presents the triple flame propagation velocity through the experiment, depending on the mixture fraction gradient, based on the laminar jet flow theory. However, in spite of these many analyses, there has not been any attempt to quantify the triple flame propagation velocity with the radius of flame curvature. In the present research, a relation of the flame propagation velocity is proposed with the radius of flame curvature for the flame stabilization mechanism. As a result, we have shown that the height of lifted flame is determined with the nozzle diameter and exit velocity of fuel and presented that the radius of flame curvature is proportion to the nozzle exit velocity of fuel and height of lifted flame. Therefore, the importance of the radius of flame curvature has to be recognized. To discribe the flame stabilization mechanism, Bilger's formula has to be modified with flame curvature effect.

• Proceedings of the Korean Society Of Semiconductor Equipment Technology
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• 2004.05a
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• pp.72-84
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• 2004

반도체 집적도가 높아지고 웨이퍼가 대구경화 됨에 따라 새로운 이송 장비의 개발이 필요하게 되었다. 본 연구에서는 이송장비의 새로운 개념인 공기부상 방식의 낱장이송 시스템을 설계하고 부상 노즐의 크기에 따른 부상 높이를 평가하였으며 그 결과 동일한 부상용 유량을 사용할 경우 0.5 mm 보다 0.8 mm 노즐이 부상 높이가 더 높고 에너지 절약적인 측면에서 유리함을 밝혔다. 또한 웨이퍼 이송용 추진 노즐의 배치에 따른 웨이퍼 이송 속도의 변화를 측정하여 동일 유량에서 추진속도가 훨씬 증가된 형상인 Type B(노즐 집중형)를 결정할 수 있었으며, 제조장비와 이송장비를 연결시켜주는 인터페이스에서의 웨이퍼 안정성을 평가한 결과 평균 16초 이내에 매우 안정된 공기부상 방식의 웨이퍼 낱장이송 시스템을 구현할 수 있었다.

• Journal of the Korean Institute of Gas
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• v.12 no.4
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• pp.21-28
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• 2008

A numerical analysis is achieved to elucidate the behavior of lifted flames and characteristics of flow near flame zone according to the exit velocity of triple flame, Poiseuille and uniform distribution. For the cases of Poiseuille and uniform nozzle exit velocity, we reviewed previous results with the present numerical results and investigated characteristics of the flame structure near the flame zone comparing with liftoff height generalized by momentum flux. In addition, a close inquiry into the combustion flow characteristics near flame zone was made with the characteristics of velocity, pressure, temperature and chemical reaction. From nozzle to flame zone, center line velocity profile traced well with the velocity profile of typical cold jet flow, but very near the flame zone, this study examined phenomenon that flow velocity decreases very quickly before the flame zone and then increases very quickly after the flame zone. Because flame zone acts as a barrier at the flow region which is before the flame zone and accelerate the flow velocity when it pass through the flame zone. This phenomenon was not clarified previous cold jet flow.

• Journal of the Korean Institute of Gas
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• v.13 no.3
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• pp.33-42
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• 2009

A numerical analysis of reactive flow in a liftoff flame is accomplished to elucidate the characteristics of liftoff flame. To verify reliance of numerical calculation, the liftoff heights of liftoff flame for various fuel exit velocities are compared between the existing experimental research results and the present calculation results. The flame propagation velocity is conducted at the flow redirection point which is on a stoichiometric line ahead of flame front. This point was selected constant distance from triple point regardless of fuel exit velocity at the previous research. This causes considerable errors for the flame propagation velocity and scalar dissipation rate. The main issue of the present research is to establish the resonable method to select the redirection point and so that to clarify the relationship between flame propagation velocity and scalar dissipation rate, which is the core properties in a triple flame stability.

• Journal of Advanced Marine Engineering and Technology
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• v.34 no.2
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• pp.250-258
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• 2010

A numerical analysis of reactive flow in a liftoff flame is accomplished to elucidate the characteristics of flame propagation velocity and volume integral of reaction rate with the variation of nozzle diameter and fuel injection flow rate in a liftoff flame consisted with fuel rich region, fuel lean region and diffusion flame region. The increase of fuel injection velocity enhances flame propagation velocity for the selected three nozzle diameter(d=0.25, 0.30, 0.35mm), but its effect on the flame propagation velocity is not much greater than 4.3%. The increase of fuel flow rate is directly and linearly related with the volume reaction rate and so the volume reaction rate, not the flame propagation velocity, might be considered to accommodate the variation of fuel flow rate in a liftoff flame.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.24 no.2
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• pp.167-175
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• 2011

The purpose of this study is to examine the impact that change in speed and modeling methods has on maglevs' runnability. The study constructed equations of motion on 4-DOF, 6DOF, and 10-DOF vehicles respectively and carried out numerical analysis, applying 4th Runge Kutta method, in order to run six different model maglev as changing the vehicles speed on the same bridge that had 2000 to 1 deflection. The analysis revealed that maglev's runnability improved as speed was lower and the specific model had higher number of bogey and EMS.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.19 no.4
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• pp.532-542
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• 2018

Because maglev trains have a propulsion and absorption force without contact with the rails, they can drive safely at high-speed with little oscillation. Recently, test model of a maglev propulsion train was produced and operated, and has since been chosen as a national growth industry in South Korea; there have been many studies and considerable investment in these fields. This study examined the dynamic responses due to bridge-maglev train interaction and basic material to design bridges for maglev trains travelling at high-speed. Depending on the major factors affecting the dynamic effects, the scope of this study was restricted to the relationship between dynamic responses. A concrete box girder was chosen as a bridge model and injured train and rail types in domestic production were selected as the moving train load and guideway analysis model, respectively. From the analysis results, the natural frequency of a bridge for a maglev train, which has a deflection limit L/2000, was higher than those of bridges for general trains. The dynamic responses of the girder of the bridge for a maglev train showed a substantial increase in proportion to the velocities of the moving train like other general bridge cases. Maximum dynamic response of the girder is shown at a moving velocity of 240km/h and increased with increasing moving velocity of train. These results can be used to design a bridge for maglev propulsion trains and provide the basic data to confirm the validity and verification of the design code.

• Proceedings of the Computational Structural Engineering Institute Conference
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• 2009.04a
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• pp.544-547
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• 2009

본 연구는 자기부상력의 선형 및 비선형효과가 이동중인 자기부상열차의 부상공극에 미치는 영향을 파악하는데 목적이 있다. 이를 위하여 자기공극의 피드백을 포함한 1자유도 차량에 대한 운동방정식을 구성하고, 최적능동제어기법을 적용하여 수치해석을 수행하였다. 해석결과 차량의 속도가 증가함에 따라 자기부상력의 선형 및 비선형효과가 자기부상차량의 부상공극에 미치는 영향에 뚜렷한 차이가 발생함을 알 수 있다. 결국 자기부상열차의 정확한 해석을 위해서는 자기부상력의 비선형효과를 고려한 해석이 필요할 것으로 판단된다.