研究者業績

森吉 泰生

モリヨシ ヤスオ  (Yasuo Moriyoshi)

基本情報

所属
千葉大学 大学院工学研究院 教授
次世代モビリティパワーソース研究センター センター長
学位
工学博士
工学修士

J-GLOBAL ID
200901076796461220
researchmap会員ID
1000010405

外部リンク

論文

 274
  • Shen Wu, Yasuo Moriyoshi, Tie Li, Xinyi Zhou, Tatsuya Kuboyama, Run Chen, Koji Morikawa, Shin Kimura, Shuai Huang, Kimitoshi Tanoue
    Journal of Engineering for Gas Turbines and Power 146(10) 2024年8月21日  査読有り
    Abstract Although prechamber (PC) is regarded as a promising solution to enhance ignition in lean-burn gas engines, a lack of comprehensive understanding of PC jet penetration dynamics remains. This study proposed a zero-dimensional (0D) model for PC jet penetration, considering the mixing of combustion products and unburned gases in jets and the floating ejection pressure. A combustion completion degree was defined by employing fuel properties and heat release to estimate the time-varying jet density. Pressure differences between the PC and the main chamber (MC) were referred to as the ejection pressure. Then, this model was validated against experimental data from a constant volume chamber (CVC) and a rapid compression and expansion machine (RCEM) with CH4-H2 blends at different equivalent ratios. Results showed that the proposed model can provide a good prediction in stationary and turbulent fields with the calibrated model coefficient. The overall jet penetration exhibits a t0.5 dependence due to its single-phase characteristic and the relatively lower density compared to the ambient gas in MC. The flame propagation speed and heat release in PC influence the combustion completion degree at the start of jet ejection. The mass fraction of burned gas in the ejected jet grows in response to the mixture equivalent ratio. Jet penetration is primarily driven by ejection pressure, with tip dynamics barely affected by the pressure difference after peaks. Tip penetration intensity rises with increasing fuel equivalent ratio and H2 addition, owing to the faster flame propagation. These findings can offer useful suggestions for model-based design and combustion model development for gas engines.
  • 森吉泰生
    LEMA (555) 2024年  
  • 野村卓矢, 森川弘二, 森川弘二, 窪山達也, 森吉泰生, 森吉泰生
    自動車技術会論文集(Web) 55(6) 2024年  
  • ZENG Changzhi, 窪山達也, 森吉泰生
    自動車技術会大会学術講演会講演予稿集(Web) 2024 2024年  
  • 石川輝明, 窪山達也, 森吉泰生
    自動車技術会大会学術講演会講演予稿集(Web) 2024 2024年  

MISC

 255
  • Moriyoshi Yasuo, Kobayashi Haruki, Kamimoto Takeyuki
    International Journal of Vehicle Design 10(5) 598-608 1989年  
    In a previous report, it was revealed that the k-ε turbulence model, which assumes an isotropic eddy viscosity, was not appropriate for the prediction of an anisotropic in-cylinder flow field. In this article, the k-ε turbulence model is modified so as to be applicable to the anisotropic in-cylinder flow, using a flux Richardson number which represents the effect of anisotropy of turbulence on turbulent diffusivity. A comparison between the prediction and the experimental data, obtained by an LDV system using a transparent cylinder engine, shows that the modified k-ε turbulence model allows successful prediction of the mean flow field but little improvement regarding the turbulence field.
  • 森吉 泰生, 神本 武征, 八木 田幹, 小林 治樹, 盛田 英夫
    日本機械学会論文集 B編 54(502) 1541-1548 1988年  
    A theoretical-experimental study of the in-cylinder air motion in a mortored reciprocating engine is made in order to assess the k-ε turbulence model, boundary and initial conditions. LDV measurements of tangential and axial velocities are conducted throughout the whole space in a transparent cylinder engine which realizes the axi-symmetrical flow field. The numerical calculation commences at 90°BTDC with an experimental flow field as an initial condition. Agreement between the calculation and the experiment is satisfactory good on the mean velocity field ; but on the turbulent energy and dissipation, the qualitative disagreement is large. The latter calls for some improvement in the k-ε turbulence model.
  • 神本 武征, 八木田 幹, 森吉 泰生, 小林 治樹, 盛田 英夫
    日本機械学会論文集 B編 53(492) p2686-2693 1987年8月  
    A transparent model engine was developed which can generate an axially symmetrical flow field in the cylinder and which allows an easy access for optical measurement of the in-cylinder air motion. Experimental data on flow characteristics such as mean velocity, turbulent velocity and turbulent scale in the entire space of the cylinder obtained with this engine are expected to be available for evaluating the reliability of mathematical models popular at present. This paper describes the design concept and details of the construction of the engine, and offers some experimental data measured by both a flow visualization technique and Laser-Doppler anemometry.
  • Takeyuki Kamimoto, Miki Yagita, Yasuo Moriyoshi, Haruki Kobayashi, Hideo Morita
    Transactions of the Japan Society of Mechanical Engineers Series B 53(492) 2686-2693 1987年  
    A transparent model engine was developed which can generate an axially symmetrical flow field in the cylinder and which allows an easy access for optical measurement of the in-cylinder air motion. Experimental data on flow characteristics such as mean velocity, turbulent velocity and turbulent scale in the entire space of the cylinder obtained with this engine are expected to be available for evaluating the reliability of mathematical models popular at present. This paper describes the design concept and details of the construction of the engine, and offers some experimental data measured by both a flow visualization technique and Laser-Doppler anemometry. © 1987, The Japan Society of Mechanical Engineers. All rights reserved.

書籍等出版物

 4

共同研究・競争的資金等の研究課題

 15