研究者業績
基本情報
研究分野
1経歴
5-
2022年2月 - 現在
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2017年2月 - 2022年1月
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2003年10月 - 2017年1月
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2002年 - 2003年
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2001年 - 2002年
学歴
1-
- 2001年
論文
169-
Cryogenics 131 103652-103652 2023年4月
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IEEE Transactions on Applied Superconductivity 32(6) 1-5 2022年 査読有り
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IEEE Transactions on Applied Superconductivity 31(5) 2021年8月
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International Journal of Hydrogen Energy 46(57) 29583-29596 2021年8月 査読有り
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Journal of Spacecraft and Rockets 58(5) 1-14 2021年6月28日 査読有り
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INTERNATIONAL JOURNAL OF HYDROGEN ENERGY 46(11) 8239-8252 2021年2月 査読有り
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CRYOGENICS 112 2020年12月 査読有り
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Journal of Physics: Conference Series 1559(1) 2020年6月19日
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INTERNATIONAL JOURNAL OF HYDROGEN ENERGY 45(7) 5098-5109 2020年2月 査読有り
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IEEE TRANSACTIONS ON APPLIED SUPERCONDUCTIVITY 29(5) 2019年8月 査読有り
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IEEE TRANSACTIONS ON APPLIED SUPERCONDUCTIVITY 29(5) 2019年8月 査読有り
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INTERNATIONAL JOURNAL OF HYDROGEN ENERGY 44(33) 18483-18495 2019年7月 査読有り
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IOP Conference Series: Materials Science and Engineering 502(1) 2019年6月3日 査読有り
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IOP Conference Series: Materials Science and Engineering 502(1) 2019年6月3日 査読有り
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PROMOTE THE PROGRESS OF THE PACIFIC-BASIN REGION THROUGH SPACE INNOVATION 166 45-57 2019年 査読有り
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航空宇宙技術 18 19-28 2019年 査読有り<p>Many space vehicles are powered by liquid hydrogen and liquid oxygen. Such fuel are cryogenic fluids, so they are easy to boil and become gas-liquid two phase flow. The LE-5B-3 engine has the capability of the idle mode firing same as the LE-5B-2 engine. Assessment of flow condition at the inlet of fuel turbo pump is important to operate the engine, because the fuel may flow in saturated condition under the idle mode in principle. In a two-phase flow state, void fraction is one of the most important parameters to assess the flow. Although many types of void fraction sensors were proposed, the capacitive technique has advantages to mount on the engine from the viewpoint of size, weight, toughness. In this study, plural circular electrodes capacitive void fraction sensor is developed for LE-5B-3 engines' ground firing test. The sensor was designed based on electric field analysis, and the specification was assessed prior to the ground test. The sensor was used in qualification test, and it was succeeded in achieving stable measurement and it helped to understand the fluid state during the engine operation. The sensor design technique, the assessment results and the ground test results are discussed in this paper.</p>
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JOURNAL OF SPACECRAFT AND ROCKETS 56(1) 91-103 2019年1月 査読有り
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CRYOGENICS 96 25-33 2018年12月 査読有り
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CRYOGENICS 94 36-44 2018年9月 査読有り
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INTERNATIONAL JOURNAL OF HYDROGEN ENERGY 43(37) 17928-17937 2018年9月 査読有り
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INTERNATIONAL JOURNAL OF HYDROGEN ENERGY 43(37) 17938-17953 2018年9月 査読有り
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Physics of Fluids 30(6) 2018年6月1日 査読有り
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DNB heat flux on inner side of a vertical pipe in forced flow of liquid hydrogen and liquid nitrogenCRYOGENICS 92 105-117 2018年6月 査読有り
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日本航空宇宙学会誌 = Aeronautical and space sciences Japan 66(2) 41-46 2018年2月
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Advances in the Astronautical Sciences 166 45-57 2018年
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日本航空宇宙学会論文集 66(6) 147-152 2018年 査読有り<p>Reducing the amount of propellant for re-cooling is an important issue for the rocket propulsion system using cryogenic fuel. Immediately after the start of the engine, the liquid fuel boils and becomes two-phase flow. In the state of two-phase flow, the void fraction, which is the gas-liquid ratio, is one of the important value for flow control. For above problem, we are developing void fraction measurement system for the cryogenic fluid. These devices were attached to the S310-43 sounding rocket for the purpose of "measuring two-phase flow behavior and heat transfer characteristics during coasting flight." These devices withstood the vibration shock test of 40G and succeeded to measure the void fraction of liquid/gas nitrogen two phase flow under vacuumed and microgravity circumstance. This report explains development and experiment results of the void fraction sensor and a capacitance amplifier. </p>
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日本航空宇宙学会誌 66(2) 41-46 2018年<p>超電導推進システムを使用する水素航空機の概念検討を行った.従来のターボファンエンジンに比べてバイパス比を向上させて低騒音化と推進効率向上を図るため,超電導モータで駆動する分散ファンを備えた推進システムを想定し,設計仕様を設定した.超電導を維持するための冷媒としては,極低温の液体水素燃料を使用することを想定した.過去の超電導発電機/モータの開発事例を参考にして諸元を設定するとともに,設計回転数と分散ファン個数を変更して,質量の変化を評価した.結果として,回転子の周速を変えずに設計回転数を上昇させることで,超電導発電機/モータの寸法と質量を大幅に低減できる可能性があることを確認した.また,分散ファンについては,超電導モータの質量を低減するために,減速機と組み合わせて設計回転数をさらに向上させる必要があることを確認した.さらに,超電導発電機/モータの出力と質量の関係を整理した.</p>
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IOP Conference Series: Materials Science and Engineering 278(1) 2017年12月30日 査読有り
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IOP Conference Series: Materials Science and Engineering 278(1) 2017年12月30日 査読有り
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INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER 111 115-122 2017年8月 査読有り
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日本航空宇宙学会誌 65(4) 89-95 2017年<p>本研究では,水素社会の普及に対応する将来の航空機システムについて,主に推進系の比較検討を行った.水素は単位質量あたりの発熱量が高く,搭載燃料を軽量にできる利点があるが,密度が低くタンク容積が大きくなることが欠点となっている.また,燃料電池自動車等に用いられている固体高分子形燃料電池(PEFC)等による電力変換が可能なこと,極低温の液体水素は冷熱源として利用しやすく,電動機器を超電導としやすいことも特徴としてあげられる.これらを踏まえ,化石燃料を使用し燃焼により動力を得る現在の推進システムをベースに,推進の電動化を含む将来の推進系候補を17ケース選定し,推進系を構成する要素の効率,重量見積もりから航続距離の簡易的な比較を行った.この結果,飛行速度の低い小型機において,液体水素を利用するケースが将来技術レベルにおいて競争力を得やすい結果となった.</p>
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53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017 2017年
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年次大会 2017 J0110104 2017年<p>JAXA has constructed an experimental facility to pressurize and supply liquid hydrogen at a maximum pressure of 90 MPa to conduct experimental research on the injection of high pressure liquid hydrogen into the atmosphere. Liquid hydrogen has a property that its density greatly changes depending on pressure despite being a liquid phase. In addition, the high pressure hydrogen gas is in a supercritical state and has an intermediate property between a gas and a liquid. Therefore, it is a difficult question whether to treat the injection of high pressure liquid hydrogen as a gas phase phenomena or as a liquid phase phenomena. As a result of the experiment, it was found good to apply the liquid orifice equation to predict the discharge flow rate of high pressure liquid hydrogen.</p>
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IEEE Transactions on Applied Superconductivity 26(3) 2016年4月 査読有り
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Journal of Fluid Science and Technology 11(2) JFST0008-JFST0008 2016年A capacitance-based void fraction sensor has been developed for the rocket or airbreathing engines, which is simple and do not disturb the flow. Typical conventional sensors usually have two concave electrodes mounted on the outer wall of the dielectric tube. They are relatively low accuracy if they have a noise shield; the maximum measurement error is over 30% in our research. The aim of this study is to improve the measurement accuracy while keeping the advantage of simplicity, mountability and non-intrusive characteristics. A theoretical formulae and electromagnetic field analysis, EFA, are used to design the sensors and are compared to an experiment using air/silicon-oil mixture flow. As the result, a newly developed asymmetrical type sensor which consists of asymmetric flat electrodes with side walls shows good performance; the inaccuracy between true void fraction and measured void fraction is 6% for the stratified flow.
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熱工学コンファレンス講演論文集 2016 C113 2016年<p>The payload capacity of launch vehicles must be increased in order to allow the exploration and development of space to be extended from low-Earth orbit into the solar system. A propellant system using a cryogenic fluid must reduce the amount of unusable propellant due to evaporation and boiling. However, in space exploration and development, where safety and reliability of missions are critical, predictions of the boiling heat transfer of current technology are not sufficiently reliable for thermal management design due to a lack of knowledge and relevant research. Therefore, the objective of this research is to understand and accurately predict boiling heat transfer by developing numerical simulation tools for two-phase flows that consider phase change. In this paper, recent research activity toward the development of chill-down process simulation technology is presented.</p>
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Physics Procedia 81 158-161 2016年 査読有り
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低温工学 51(5) 155-163 2016年 査読有りThe research and development conducted regarding fully superconducting motors for liquid-hydrogen transfer pumps using MgB<sub>2</sub> monofilamentary wires are gathered into this paper. Synchronous rotation without slip can be realized using squirrelcage-type rotor windings composed of quasi-superconducting loops soldered between MgB<sub>2</sub> wires, thereby enabling superconducting motors with low loss and high efficiency to be achieved. The use of MgB<sub>2</sub> wires for stator windings also enables the primary winding loss to be reduced drastically compared to conventional copper winding. The transfer of liquid hydrogen from a metal cryostat containing the fabricated MgB<sub>2</sub> motor to a glass Dewar vessel for visual monitoring is demonstrated successfully.<tt> </tt>
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PROCEEDINGS OF THE 28TH INTERNATIONAL SYMPOSIUM ON SUPERCONDUCTIVITY (ISS 2015) 81 158-161 2016年 査読有り
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IOP Conference Series: Materials Science and Engineering 101(1) 2015年12月18日 査読有り
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IOP Conference Series: Materials Science and Engineering 101(1) 2015年12月18日 査読有り
MISC
168講演・口頭発表等
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年次大会 2018年<p>A loading system plays a role of loading and unloading liquid hydrogen between a carrier ship and a ground storage facility in hydrogen supply chain in which hydrogen in the form of liquid phase is transported by the carrier ship from a resource-rich country to a consuming country. An emergency release system (ERS), which is one of components of the loading system, is installed in the middle of transfer pipe of the loading system, and has function of separating and plugging the pipe at an abnormality during loading so as to prevent a large amount of cryogenic fluid from scattering. We have conducted R & D study of the ERS for liquid hydrogen based on an existing one for liquid natural gas (LNG). Whole system function of the ERS including separation behavior was verified conducting a field experiment with the ERS test model and liquid hydrogen. Through several tests, the separation mechanism and behavior were verified, and also, soundness of the seal mechanism was evaluated. While, auto-ignition phenomena were observed on the separation surface of the ERS after the separation, of which causes have not been identified yet. Characteristics of dispersion behavior of hydrogen that was released at the separation could be investigated measuring distribution of temperature and hydrogen concentration around the ERS test model.</p>
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年次大会 2018年<p>To improve safety regulations for fuel cell vehicles and hydrogen infrastructure, experiments of cryo-compressed hydrogen leakage diffusion were conducted. The experimental apparatus can supply 90 MPa hydrogen of various temperature conditions. Measurement items were hydrogen concentration distribution, blast pressure, flame length, and radiant heat. In addition, high speed camera observation was carried out to investigate the near-field of cryogenic hydrogen jet at supercritical pressure. The experimental apparatus can supply 90 MPa hydrogen at various temperature conditions (50 K–300 K) at a maximum flow rate of 100 kg/h. The hydrogen leakage flow rate was measured using pinhole nozzles with different outlet diameters (0.2 mm, 0.4 mm, 0.7 mm, and 1 mm). It was confirmed that the hydrogen leakage flow rate increases as the supply temperature decreases. The hydrogen concentration distribution was measured by injecting high-pressure hydrogen from the 0.2-mm pinhole for 10 min under a constant pressure/temperature condition. As the hydrogen injection temperature decreased, it was found that the hydrogen concentration increased, and an empirical formula of the 1% concentration distance for the cryogenic hydrogen system was newly presented.</p>
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年次大会 2017年<p>JAXA has constructed an experimental facility to pressurize and supply liquid hydrogen at a maximum pressure of 90 MPa to conduct experimental research on the injection of high pressure liquid hydrogen into the atmosphere. Liquid hydrogen has a property that its density greatly changes depending on pressure despite being a liquid phase. In addition, the high pressure hydrogen gas is in a supercritical state and has an intermediate property between a gas and a liquid. Therefore, it is a difficult question whether to treat the injection of high pressure liquid hydrogen as a gas phase phenomena or as a liquid phase phenomena. As a result of the experiment, it was found good to apply the liquid orifice equation to predict the discharge flow rate of high pressure liquid hydrogen.</p>
共同研究・競争的資金等の研究課題
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日本学術振興会 科学研究費助成事業 2023年4月 - 2027年3月
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日本学術振興会 科学研究費助成事業 2020年4月 - 2023年3月
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日本学術振興会 科学研究費助成事業 2019年4月 - 2022年3月
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日本学術振興会 科学研究費助成事業 2015年4月 - 2018年3月
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日本学術振興会 科学研究費助成事業 2013年5月 - 2018年3月