周晗, 陈芊, 汪虹余, 史昊蓝, 魏鹏轩, 李嘉诚, 张天宏, 盛汉霖(
)
收稿日期:2024-10-23
修回日期:2024-11-12
接受日期:2024-12-06
出版日期:2024-12-18
发布日期:2024-12-18
通讯作者:
盛汉霖
E-mail:dreamshl@nuaa.edu.cn
基金资助:
Han ZHOU, Qian CHEN, Hongyu WANG, Haolan SHI, Pengxuan WEI, Jiacheng LI, Tianhong ZHANG, Hanlin SHENG(
)
Received:2024-10-23
Revised:2024-11-12
Accepted:2024-12-06
Online:2024-12-18
Published:2024-12-18
Contact:
Hanlin SHENG
E-mail:dreamshl@nuaa.edu.cn
Supported by:摘要:
高通流双变循环发动机(High Flow Dual Variable Cycle Engine, HFDVCE)以全速域大流量、高节流比、涵道比和增压比同步组合调节以及高涡轮前温度等气动热力方案来获得高性能工作能力,满足低速经济性和高速大推力的需求。相比于常规发动机,HFDVCE在全包线范围内及模式切换时具有更加突出的气动稳定性问题。因此,本研究致力于开展HFDVCE的气动稳定性研究,针对当前研究中整机失稳模拟的缺失与多工况下各子模型间参数不匹配等问题,提出了一种含失稳模拟的HFDVCE模型。首先,基于部件法建立高精度发动机非线性模型,获得压缩部件气动参数。然后,提出了一种压缩部件气动失稳动力学建模方法。通过引入扭矩项表征转速对失稳模型特性的影响,建立含失速、喘振两类不稳定工况的失稳模型,避免了定转速假设,解决了多失稳子模型间系数不匹配的问题。进一步,厘清压缩部件失稳模型与发动机非线性模型之间的耦合关系,通过失稳系数表征压缩系统气动失稳对发动机整机性能的影响,建立了含失稳模拟的HFDVCE模型,实现了整机失稳的动态模拟。最后,开展了4种HFDVCE典型失稳模式的仿真实验,验证了该模型的有效性,为主动稳定性控制设计提供了仿真平台。
中图分类号:
周晗, 陈芊, 汪虹余, 史昊蓝, 魏鹏轩, 李嘉诚, 张天宏, 盛汉霖. 含失稳模拟的高通流双变循环发动机动态模型[J]. 航空学报, 2025, 46(14): 131436.
Han ZHOU, Qian CHEN, Hongyu WANG, Haolan SHI, Pengxuan WEI, Jiacheng LI, Tianhong ZHANG, Hanlin SHENG. A high flux dual variable cycle engine model coupled with instability simulation[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(14): 131436.
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