低压和低温设施的设计和应用,用于在拉开过程中研究航空火焰
M-E Clavel1, W Vasquez2, A Vandel1
1INSA Rouen Normandie, Univ Rouen Normandie, CNRS, Normandie Univ, CORIA UMR 6614, F-76000 Rouen, France.
The Review of scientific instruments
|March 17, 2025
概括
一个新的高空重点点燃气轮机 (HARTur) 设施研究了发动机重点燃. 高海拔地区的低压和低温会破坏火焰的稳定,影响航空发动机的可操作性.
科学领域:
- 航空工程 航空工程
- 燃烧科学 燃烧科学
- 热力学是一种热力学.
背景情况:
- 点火和重新点火对于航空发动机的可操作性至关重要,特别是在高空.
- 高海拔条件 (低压,低温,流量减少) 会对燃料的原子化,蒸发和火焰稳定性产生负面影响.
研究的目的:
- 开发和利用高空燃气轮机 (HARTur) 设施的高空重新点火,以模拟高空条件.
- 为了研究燃气轮机中重新点火的拉开阶段.
- 描述丰富-灭-瘦注射系统的性能,并确定灭绝极限.
主要方法:
- 开发了HARTur设施,可以复制高达30,000英尺的高度,压力低至30kPa,温度高达248K.
- 估计的燃烧效率使用燃烧的气体温度通过压力下降通过出口喷嘴.
- 采用先进的光学诊断,包括激光断层扫描,平面激光诱导光和粒子图像速度计,用于局部喷雾和火焰分析.
主要成果:
- 燃烧效率在接近大气条件下比在低压,低温和高海拔条件下更高.
- 低温,低压环境导致喷射角度更广,原子化较差,再循环区域不稳定.
- 在高海拔条件下,火焰不稳定和灭绝的可能性更大,缩小了拉开走廊.
结论:
- 高海拔条件极大地挑战了航空发动机的重新点火和可操作性.
- 优化注射器设计和燃料计量策略对于在极端环境中提高发动机性能至关重要.
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