• Title/Summary/Keyword: Ultra high-speed tube

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Parametric Study on the Aerodynamic Drag of Ultra High-speed Train in Evacuated Tube - Part 2 (진공튜브 내 초고속열차의 공기저항 파라메타 연구 - 2)

  • Kwon, Hyeok-Bin;Nam, Seong-Won;Kim, Dong-Hyeon;Jang, Yong-Jun;Kang, Bu-Byoung
    • Journal of the Korean Society for Railway
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    • v.13 no.1
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    • pp.51-57
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    • 2010
  • The aerodynamic drag of ultra high-speed train in evacuated tube have been calculated using computational fluid dynamics and the variation of aerodynamic drag for the change of major system parameter of tube-vehicle system such as the train speed, air density, and the tunnel diameter. The aerodynamic drag in the tube increases with increasing train speed, however, the ratio of drag increase in tube is larger than that on the open field, the V square rule. The aerodynamic drag decreases with increasing tunnel diameter and increasing air density, and the drag increasing for air density is almost linear just like that on open field. For some combination of the parameters, the trend of aerodynamic drag of train showed irregularity.

Core Technologies of Superconducting Magnet for High-speed Maglev and R&D Activities in Korea (초고속 Maglev용 초전도 마그넷 요소 기술 및 국내 연구 개발 현황)

  • Lee, Chang-Young;Kang, Bu-Byoung;Han, Young-Jae;Sim, Ki-Deok;Park, Dong-Keun;Ko, Tae-Kuk
    • Proceedings of the KSR Conference
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    • 2009.05a
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    • pp.1454-1460
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    • 2009
  • Ultra-speed tube train, which runs in vacuum atmosphere to overcome aero-dynamic dragging force, is considered as a high-speed ground transportation system to back up long-distance air travel. To realize the ultra-speed tube train, feasibility study of currently available Maglev technologies especially for propulsion and levitation system is needed. Propulsion by linear synchronous motor(LSM) and levitation by electro-dynamic suspension(EDS) which are utilized in the Japan's MLX system could be one of candidated technologies for ultra-speed tube train. In the LSM-EDS system, the key component is superconducting magnet, and its reliability and performance is very important to guarantee the safe-operation of Maglev. As the initiative of the feasibility study, this paper deals with the basic structure of superconducting magnet and core technologies to design and operate it. And by surveying the current R&D achievement in Korea, the nation's capability to develop advanced superconducting magnet for Maglev is presented.

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Parametric Study on the Aerodynamic Drag of Ultra High-speed Train in Evacuated Tube - Part 1 (진공튜브 내 초고속열차의 공기저항 파라메타 연구 - 1)

  • Kwon, Hyeok-Bin;Kang, Bu-Byoung;Kim, Byeong-Yun;Lee, Du-Hwan;Jung, Hyun-Ju
    • Journal of the Korean Society for Railway
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    • v.13 no.1
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    • pp.44-50
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    • 2010
  • This study is devoted to understand the basic characteristics of the flowfield around a train in evacuated tube and to suggest an efficient numerical method to calculate the flowfield. To get steady-state solution in minimum calculation domain, various boundary condition have been tried for steady calculation and have been compared to the solution of unsteady calculation. At the train velocity of 300km/h, the aerodynamic drag results of both calculation method agreed very well. The drag ratio between on the open filed and in the tube from the calculation result by the suggested numerical method lied in the same fitting curve with that from the filed test of high-speed trains running in the line.

Application of Superfluid Shock Tube Facility to experiment of High Reynolds number flow (초유동 충격파관 장치의 고레이놀즈수 유동실험에의 응용)

  • ;H. Nagai;Y. Ueta;K. Yanaka;M. Murakami
    • Proceedings of the Korea Institute of Applied Superconductivity and Cryogenics Conference
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    • 2002.02a
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    • pp.27-30
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    • 2002
  • The particle velocity in superfluid helium (He II) induced by a gas dynamic shock wave impingement onto He II free surface were studied experimentally by using Schlieren visualization method with an ultra-high speed video camera. It is found form visualization results that a dark zone in the immediate vicinity of the vapor-He II interface region is formed because of the high compressibility of He II and is developed toward bulk He II with the flowing-down speed of the vapor-He II interface. The mass velocity behind a transmitted compression shock wave that is equal to the contraction speed of He II amounts to 10 m/sec, the Reynolds number of which reaches $10^{7}$. This fact suggests that the superfluid shock tube facility can be applied to an experimental facility for high Reynols number flow as an alternative to the superfluid wind tunnel.

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Flow Analysis Using 1 and 3 Dimensional Hybrid Mesh For Ultra-High Speed Vehicle Inside A Long Distance Tunnel (1-3차원 혼합격자를 이용한 장거리 터널 내 고속 운송체 유동해석)

  • Kim, Tae-Kyung;Choi, Joong-Keun;Kwon, Hyeok-Bin;Kim, Kyu-Hong
    • Proceedings of the KSR Conference
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    • 2011.10a
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    • pp.107-118
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    • 2011
  • This paper performs flow analysis of ultra-high speed vehicle inside the long distance tunnel. One and three dimensional hybrid mesh was used for describing moving motion and flow analysis of an vehicle inside a long distance tunnel which over 20 km. Flow analysis and aerodynamic drag measuring were performed by three dimensional mesh: around vehicle, and pressure waves of a tunnel was measured by one dimensional mesh: the other region where rare changing of flow pattern.

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Development of 1-3 Dimensional Hybrid Mesh Method for Flow Analysis of the Ultra-High Speed Vehicle Inside a Long Distance Tunnel (장거리 터널 내 고속 운송체의 유동 해석을 위한 1-3차원 혼합격자 기법개발)

  • Choi, Joong-Keun;Kim, Tae-Kyung;Kwon, Hyeok-Bin;Kim, Kyu-Hong
    • Proceedings of the KSR Conference
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    • 2011.10a
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    • pp.119-127
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    • 2011
  • This paper shows development of 1-3 dimensional hybrid mesh method to analysis flow induced by ultra-high speed vehicle inside a long distance tunnel. For three-dimensional analysis of the tunnel system many meshes are required. However it is not efficient to calculate the whole tunnel system in three-dimension. Therefore in this paper, three-dimension meshes was used to describe stations, shafts and around vehicle, and one-dimension meshes was used to describe the tunnel except these three sections. And unsteady flow analysis of the ultra-high speed vehicle was performed with UDFs in commercial software, Ansys vr. 12.0.

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Air-tightness Evaluation of Tube Structures for Super-speed Tube Railway Systems: I. Analytical Modeling and Material Test (초고속 튜브철도 시스템을 위한 튜브 구조물의 기밀성 평가 : I. 해석모델 수립 및 재료 기밀성)

  • Park, Joo-Nam;Nam, Seong-Won;Kim, Lee-Hyeon;Yeo, In-Ho
    • Journal of the Korean Society for Railway
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    • v.14 no.2
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    • pp.143-150
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    • 2011
  • This paper presents a preliminary study for air-tightness evaluation of vacuum tube structures for super-speed tube railway systems. The formula for flow rate of the air caused by the pressure difference of the inside and outside of the tube structure is derived based on Darcy's law. A test is then performed to measure the air-permeability of concrete with various compressive strengths, the result of which is used for analytical simulation of the air intrusion for a tube structure with a preliminarily defined section. It has been shown that concrete with the compressive strength of at least more than 50MPa is recommended for effective operation and maintenance of the vacuum pump systems, as the air-permeability of concrete is inversely proportional to the exponent of its compressive strength.

Study on Vacuum Pump Capacity with Leakage of Tube Structure (튜브구조물의 누설을 포함한 진공 펌프 용량에 관한 연구)

  • Nam, Seong-Won
    • Proceedings of the KSR Conference
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    • 2011.10a
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    • pp.1157-1161
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    • 2011
  • Parametric study has been conducted to calculate the capacity of vacuum pump system that will be used to maintain the pressure of the tube system under atmosphere level. Recently many railroad researchers pay attention to the tube train system as one of the super high speed transportation system. To achieve the ultra super high speed, the inside of tube system should be maintained the low pressure level. In the low pressure environment, it is well known that air resistance of train is drastically decreased. Vacuum pump system will be used to make the low pressure level of tube system, exhaust the leakage air and supplement additional vacuum pumping. Qualitative and quantitative study has been conducted to review the effects of major parameters concerned with the capacity of vacuum pump system. As a results of these studies, we get the lump capacity of vacuum pump for various parameters. These results can be used to analyse the effects of the reduction of air resistance.

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Implementation and Performance Evaluation of a Precision Localizing Device for Hyperloop Pods Driving at Ulta-High Speeds (초고속주행 하이퍼루프 포드의 정밀 위치측정 장치 구현 및 성능평가)

  • Ok, Min-Hwan;Choi, Su-Yong;Choe, Jae-Heon;Lee, Kwan-Sup
    • The Journal of Korea Institute of Information, Electronics, and Communication Technology
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    • v.13 no.5
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    • pp.443-451
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    • 2020
  • A futuristic locomotion system called Hyperloop is projected for driving at ulta-high speed, levitated in the tube. In hyperloop localization of pods on the linear synchronous motor is essential for pod driving. precision localization is required for acceleration and deceleration of pods driving at speed above 1,000km/h, and also required for adjusting the pod speed driving at this very-high speed to maintain inter-vehicle distance. In this work, a new scale of localization is challenged by modified laser surface velocimeter. In acceleration the speed of a virtual pod is calculated along its displacement measured by laser reflection. Under the requirement of precise localization of the pod driving at ultra-high speed, a displacement measurement device, which detects the difference in reflections from tiles passing by the pod, is developed and evaluated through performance test. Tests of pod speeds below 500km/h have showed exact localization results of the precision in centimeters, and tests of pod speeds above 500km/h have showed localization with very low error rates under 0.1%. For the measurement above 500km/h, future works would pursue the error rate converges to zero.