高超声速飞机尾喷管设计-制造与验证技术发展综述  

Technological development in hypersonic nozzle design,manufacture and validation:A review

作　　者：林鹏 庄福建 曲林锋[3] 许阳阳 苏亚东[3] LIN Peng;ZHUANG Fujian;QU Linfeng;XU Yangyang;SU Yadong(Chinese Aeronautical Establishment,Beijing 100029,China;Yangzhou CIRI,AVIC Shenyang Aircraft Design&Research Institute,Yangzhou 225000,China;AVIC Shenyang Aircraft Design&Research Institute,Shenyang 110035,China)

机构地区：[1]中国航空研究院,北京100029 [2]航空工业沈阳飞机设计研究所扬州协同创新研究院,扬州225000 [3]航空工业沈阳飞机设计研究所,沈阳110035

出　　处：《航空学报》2022年第6期45-55,共11页Acta Aeronautica et Astronautica Sinica

摘　　要：高超声速飞机是临近空间领域的重要飞行器形式,具有重要的发展意义。尾喷管是其产生推力的主要部件,其性能和可靠性直接影响整机全局。针对高超声速飞机尾喷管技术,梳理涡轮发动机、火箭发动机和冲压发动机的尾喷管分类与技术特点,总结尾喷管工程研制与应用水平以及共性技术的国内外研究现状,并指出高超声速飞机尾喷管结构关键技术,包括优化设计技术、材料与工艺技术和综合验证技术,最后,给出了高超声速飞机尾喷管技术的重要难题以及后续发展建议。Development of hypersonic aircraft,one of the most important flight vehicles in the near-space domain,is of critical significance.The nozzle is the main part in generating thrust in hypersonic aircraft,with its performance and reliability directly affecting the whole aircraft.Focusing on the hypersonic aircraft nozzle technology,this paper analyzes nozzles of the turbine engine,rocket,and ramjet in their classification and technical features,summarizes the state-of-the-art of the nozzle technology,presenting the key technologies of nozzle structure,include design and optimization,material and manufacturing,and comprehensive validation.Important challenges and development suggestions in the future were finally provided.

关 键 词：高超声速 临近空间 尾喷管 涡轮发动机 火箭发动机 冲压发动机 

分 类 号：V228.73[航空宇航科学与技术—飞行器设计]