摘要: |
针对发动机控制规律的选取对飞机/发动机性能一体化设计的影响,基于飞机/发动机性能一体化设计方法,开展了发动机控制规律优化设计方法研究。从先进战斗机飞行任务出发,开展了飞机/发动机性能一体化设计方法研究,进行约束分析和任务分析,以起飞总重最低为目标优选飞机/发动机设计方案,验证了设计方法的合理性。采用飞机/发动机性能一体化设计方法,分别研究了不同节流比和不同控制规律设计对飞机/发动机性能一体化设计的影响。研究表明:在飞机/发动机性能一体化设计过程中,采用合理的发动机最大状态控制规律同时选取恰当的发动机节流比,可以有效扩大约束可行域,同时能够降低发动机的燃油消耗量,降低飞机起飞总重。 |
关键词: 飞机/发动机性能一体化 控制规律 升阻特性 非安装性能 安装性能 |
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Research on Aero-Engine Control Law Optimization Design Based on Integrated Fighter / Aero-Engine Performance |
SONG Wen-yan,MENG Ping-ping,CHAI Zheng
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(School of Power and Energy,Northwestern Polytechnical University,Xi’an 710072,China)
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Abstract: |
In view of the effects of the selection of the engine control law on the integrated fighter / aero-engine performance, the optimization design method of the engine control law based on the integrated fighter / aero-engine performance was carried out. Based on the typical advanced fighter flight mission, the integrated fighter / aero-engine performance design is carried out, and constraint analysis and mission analysis were conducted. Taking the lowest total takeoff weight as the optimization target, the optimal fighter / aero-engine were obtained. The rationality of the design method was verified. The effects of different throttle ratios and different control laws on integrated fighter / aero-engine performance design were respectively studied by using the method of integrated fighter / aero-engine performance. The results show that reasonable aero-engine control law under maximum condition and reasonable aero-engine throttle ratio can effectively expand the constraint feasible region and reduce the fuel consumption of engine and the total take-off weight of aircraft in the integrated fighter / aero-engine performance. |
Key words: Aircraft/engine performance integration Control law Lift drag characteristic Uninstalled performance Installed performance |