航空学报 > 2025, Vol. 46 Issue (20): 531919-531919   doi: 10.7527/S1000-6893.2025.31919

基于噪声与油耗的超声速客机进近程序优化

李亚飞(), 赵瑞   

  1. 中国民航大学 空中交通管理学院,天津 300300
  • 收稿日期:2025-03-03 修回日期:2025-04-07 接受日期:2025-04-27 出版日期:2025-05-12 发布日期:2025-05-06
  • 通讯作者: 李亚飞 E-mail:commissioner@126.com
  • 基金资助:
    中央高校基本科研业务费项目中国民航大学专项资助(3122024055);天津市民航能源环境与绿色发展工程研究中心开放基金(NYHJ2023-KF-02)

Optimization of supersonic passenger aircraft approach procedure based on noise and fuel consumption

Yafei LI(), Rui ZHAO   

  1. College of Air Traffic Management,Civil Aviation University of China,Tianjin 300300,China
  • Received:2025-03-03 Revised:2025-04-07 Accepted:2025-04-27 Online:2025-05-12 Published:2025-05-06
  • Contact: Yafei LI E-mail:commissioner@126.com
  • Supported by:
    Central Universities’Basic Research Funding Program for Civil Aviation University of China(3122024055);Tianjin Civil Aviation Energy Environment and Green Development Engineering Research Center Open Fund(NYHJ2023-KF-02)

摘要:

针对超声速客机在下降阶段的实际运行所面临的噪声污染严重及燃油成本高昂两大突出问题,以繁忙且具有代表性的民航枢纽机场广州白云国际机场做为研究场景,依据现有的基于性能导航(PBN)进近程序,结合超声速客机飞行性能参数,开展了深入研究。首先,依据超声速客机独特的飞行性能,初步设计一条适用于超声速客机的进近程序。随后,通过选取机场附近噪声敏感点,运用噪声评估模型与油耗计算模型,采用多目标智能优化算法,对现行的PBN进近程序进行针对性的优化调整,使进近程序更适配于超声速客机降落阶段的实际运行,在保障飞行安全的前提下,最大程度降低噪声影响与运行油耗。研究结果显示:超声速客机遵循优化后的进近程序运行,噪声值与油耗值较优化前具有较大改进,噪声值最多降低37.3%,整体运行噪声影响降低了9.2%;油耗值最多降低16.45%,整体运行油耗降低了11.8%。

关键词: 超声速客机, PBN进近程序, 噪声, 燃油消耗, 多目标优化

Abstract:

To address the two prominent problems of serious noise pollution and high fuel cost faced by supersonic passenger aircraft in the descent phase, this paper takes Guangzhou Baiyun International Airport, a busy and representative civil aviation hub airport, as a research scenario. Based on the existing Performance Based Navigation(PBN)approach procedures and the performance parameters of the flight of supersonic airliners, an in-depth study is conducted. First, a preliminary approach procedure for supersonic airliners is designed based on the unique flight performance of supersonic passenger aircraft. Subsequently, by selecting noise-sensitive points near the airport, applying the noise assessment model and fuel consumption calculation model, and adopting the multi-objective intelligent optimization algorithm, the current PBN approach procedure is optimized and adjusted, so as to make the approach procedure more suitable for the actual operation of supersonic passenger aircraft during the landing phase, and to minimize the noise impact and fuel consumption under the prerequisite of safeguarding flight safety. The results of the study show that when the supersonic passenger aircraft follows the optimized approach procedure, the noise value and fuel consumption value are greatly improved compared with those before optimization. The noise value is reduced by 37.3% at most, and the overall operational noise impact is reduced by 9.2%. The fuel consumption value is reduced by 16.45% at most, and the overall operational fuel consumption is reduced by 11.8%.

Key words: supersonic passenger aircraft, PBN approach procedure, noise, fuel consumption, multi-objective optimization

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