Flame-wall interaction for gas turbine applications
编号:172 访问权限:仅限参会人 更新:2025-09-30 11:49:29 浏览:4次 主旨报告

报告开始:2025年10月10日 13:30(Asia/Shanghai)

报告时间:30min

所在会场:[S1] Computer simulations for reducing CO2 emission [S6-1] Session 6-1: Numerical methods in multiscale and multi-physics modeling

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摘要
The climate change has forced many combustion systems move away from hydrocarbon fuels. The strongest alternative fuel is hydrogen whose exhaust only emits water vapor. Therefore, many gas turbine manufacturers are developing 100% hydrogen-powered gas turbines. In switching the fuel, one of the major technical issues is flame flashback – the reactivity of hydrogen is so fast so that the flame propagates upstream of the fuel nozzle. Once the flame flashback happens that the fuel nozzle which is weak for high temperature can be burnt and the nozzle has to be replaced. The flame flashback would incur interruption of the operation as well as the huge replacing cost. To prevent flame flashback, gas turbine manufacturers are now switching nozzle types from swirlers to micro-mixers which is relatively more robust to flame flashback. Still, fundamental understanding on flame flashback is necessary to rule out the onset of flame flashback and optimize the nozzle to reduce the pressure drop. The current talk presents the recent findings on the dynamics on flame flashback on hydrogen flames. Premixed flame propagation in a turbulent boundary layer reveals the interaction between the flame propagation and the modification of approaching turbulent flows. Furthermore, the quenching distance of the flame can change by wall thermal characteristics of walls.
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报告人
Donghyuk Shin
Korea Advanced Institute of Science and Technology Department of Aerospace Engineering, South Korea

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重要日期
  • 会议日期

    10月09日

    2025

    10月13日

    2025

  • 08月30日 2025

    初稿截稿日期

  • 10月13日 2025

    注册截止日期

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