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基于自激扫掠喷嘴的加力燃烧效率实验研究

王士奇1,温泉1,贾志刚2,程奕鑫1,李林1,3,4,张弛5,霍伟业6,马梁7   

  1. 1. 中国航空发动机研究院
    2. 中航空天发动机研究院有限公司
    3. 北京航空航天大学 航空发动机气动热力重点实验室
    4. 北京航空航天大学 航空发动机研究院
    5. 北京航空航天大学 航空发动机研究院 航空发动机气动热力国家级重点实验室
    6. 北华航天工业学院 中国
    7. 中国民航大学
  • 收稿日期:2024-04-29 修回日期:2024-06-12 出版日期:2024-06-17 发布日期:2024-06-17
  • 通讯作者: 王士奇
  • 基金资助:
    国家自然科学基金;先进航空动力创新工作站

Experimental study on the afterburner combustion efficiency based on self-excited sweeping nozzle

  • Received:2024-04-29 Revised:2024-06-12 Online:2024-06-17 Published:2024-06-17
  • Supported by:
    National Natural Science Foundation of China;Advanced Jet Propulsion Innovation Center, AEAC

摘要: 为了验证自激扫掠喷嘴应用于加力燃烧室的可行性,以及高频动态扫掠燃油喷射方法对于提高加力燃烧效率的有效性,本研究首先设计了耦合自激扫掠喷嘴结构的加力燃油喷杆,对其流量、频率、张角等基本工作特性进行测量,并与圆孔直射式喷杆进行对比分析。然后,基于矩形加力燃烧室性能测试平台,在相同工况条件和油气比范围内,分别采用直射喷杆和自激扫掠喷杆,测量总体燃烧效率,并监测壁面动态压力脉动信息。结果表明,在10mm直径的加力燃油喷杆内,可实现多个自激扫掠喷嘴的结构耦合;与等几何通径的直射式喷杆相比,自激扫掠喷杆的流通能力提高了23%;同一喷杆内的多个自激扫掠喷嘴,其工作频率和扫掠张角随进口压力的变化规律基本相同,具有较好的一致性。采用自激扫掠喷杆,加力燃烧效率可提高3.7%,且未监测到与自激扫掠喷嘴工作频率相同或接近的压力脉动频率,表明高频动态扫掠燃油喷射不会对火焰热声振荡模态及稳定器后方的大尺度脱落涡结构产生直接影响。

关键词: 自激扫掠喷嘴, 高频动态扫掠喷射, 加力燃烧室, 振荡频率, 压力脉动, 流体振荡器

Abstract: In order to prove the feasibility of applying the self-excited sweeping nozzle in the afterburner, and the effectiveness of high frequency dynamic sweeping fuel injection methods for improving the efficiency of afterburner combustion, this study first designed a fuel spray bar integrated with the self-excited sweeping nozzles, and its basic working charac-teristics, such as flow rate, frequency and sweeping angle are tested, and further compared with the plain-orifice spray bar. Then, based on the rectangular afterburner test rig, under the same test conditions and the fuel-to-air ratio range, employing the plain-orifice spray bar and self-excited sweeping spray bar respectively, the overall combustion efficien-cies are tested and the dynamic wall pressure pulsation information is monitored. The results show that multiple self-sweeping nozzles can be integrated into the spray bar with the diameter limitation of 10mm. the flow capability of the self- excited sweeping spray bar is increased by 23%, compared to the plain-orifice spray bar with the equivalent ge-ometric flow area. For the nozzles in the same spray bar, their operating frequency and sweeping angle responses to the pressure drop are basically the same and have good consistency. The afterburner combustion efficiency is im-proved by 3.7%, by employing the self-excited sweeping spray bar,and no frequency which is same or close to the operating frequency of self- excited sweeping nozzle is found in the monitored wall pressure pulsation spectrum, indi-cating that high frequency dynamic sweeping fuel injection has no direct impact on the flame thermoacoustic oscilla-tion mode and large scale shedding vortex structure downstream the flameholder.

Key words: self-excited sweeping nozzle, high frequency dynamic sweeping fuel injection, afterburner, oscillation frequency, dynamic pressure pulsation, fluidic oscillator

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