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作 者:王波 惠鑫[2] 李锋[3] 程明 张漫 杨金虎[6] WANG Bo;HUI Xin;LI Feng;CHENG Ming;ZHANG Man;YANG Jinhu(Department of Mechanics and Aerospace Engineering,Southern University of Science and Technology,Shenzhen Guangdong 518055,China;Research Institute of Aero-Engine,Beihang University,Beijing 100191,China;School of Energy and Power Engineering,Beihang University,Beijing 100191,China;Shenyang Engine Research Institute,Aero Engine Corporation of China,Shenyang 110015,China;Commercial Aircraft Engine Company Limited,Aero Engine Corporation of China,Shanghai 200241,China;Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100083,China)
机构地区:[1]南方科技大学力学与航空航天工程系,广东深圳518055 [2]北京航空航天大学航空发动机研究院,北京100191 [3]北京航空航天大学能源与动力工程学院,北京100191 [4]中国航发沈阳发动机研究所,沈阳110015 [5]中国航发商用航空发动机有限责任公司,上海200241 [6]中国科学院工程热物理研究所,北京100083
出 处:《航空动力学报》2022年第11期2479-2487,共9页Journal of Aerospace Power
基 金:国家科技重大专项(J2019-Ⅲ-0002-0045,2017-Ⅲ-0002-0026);国家自然科学基金(92041001)。
摘 要:阐述了动态燃烧的内涵,从先进军用和民用发动机的需求出发,强调了开展主燃烧室动态燃烧研究、支撑燃烧室精细化设计的重要性。对国内外动态燃烧研究进行了总结,从基础研究、模型燃烧室研究、数值模拟研究及工程应用四方面将国内外情况进行了对比。分析了开展动态燃烧研究的难点,梳理了我国开展动态燃烧研究需攻克的四大关键技术,并阐述了其内涵及可采取的技术路径。基于我国先进军民用发动机需求和国内研究现状,提出了建立数据库、发展设计方法、构建理论体系及培养研究队伍等合理化建议。The essence of dynamic combustion was explained. Based on the requirements of both military and civil aircraft engines, the importance of conducting dynamic combustion technologies and supporting the optimization design of aero-engine combustors was highlighted. The research progress on dynamic combustion technologies was summarized and compared from domestic and foreign aspects in terms of fundamental research, model combustor research, numerical simulation, and engineering application. The challenges in developing dynamic combustion technologies were analyzed, four key technologies to be developed in China were presented, and their connotation and technical pathways were expounded. Based on the design requirements of advanced engines along with current dynamic combustion progress, suggestions including establishing database, developing design methods, building theoretical system and training research teams, were put forward for developing dynamic combustion technologies in China.
关 键 词:主燃烧室 动态燃烧 过渡态 非定常仿真 光学诊断
分 类 号:V231.2[航空宇航科学与技术—航空宇航推进理论与工程]
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