高超声速飞机机载作动系统发展分析  

Analysis on Hypersonic Aircraft Actuation System Development

作　　者：李洋[1,2] 成超乾 陈龙 焦宗夏 Li Yang;Cheng Chaoqian;Chen Long;Jiao Zongxia(Beihang University,Beijing 100191,China;The State Key Laboratory of Fluid Power and Mechatronic Systems,Hangzhou 310027,China;Science and Technology on Aircraft Control Laboratory,Beihang University,Beijing 100191,China;Chinese Aeronautical Establishment,Beijing 100012,China)

机构地区：[1]北京航空航天大学,北京100191 [2]流体动力基础件与机电系统国家重点实验室,浙江杭州310027 [3]北京航空航天大学飞行器控制一体化技术重点实验室,北京100191 [4]中国航空研究院,北京100012

出　　处：《航空科学技术》2023年第11期44-50,共7页Aeronautical Science & Technology

基　　金：国家自然科学基金(52272409);流体动力与机电系统国家重点实验室开放基金(GZKF-202111)。

摘　　要：吸气式高超声速飞机面临严酷的高动压、大热流飞行环境,要求机载系统既要兼具高功率、高效能与高耐热能力,又要满足严苛的体积、重量(质量)与能量约束,给飞控作动系统设计带来了极大的技术挑战。本文通过对高超声速飞机任务和平台动力特点的分析,系统地论述了其飞控作动系统面临的挑战,包括能源、结构和热管理等问题。基于已有高速飞机的公开资料,对作动技术发展现状进行了梳理,结合热管理与机载能源的发展趋势,展望了高超声速飞机作动系统的重点发展方向,并给出了具有可行性的发展路线。The high speed and high dynamic pressure of the air-breathing hypersonic aircraft put forward high requirements on the accuracy and power of the actuation system.The strict volume,weight,energy and heat constraints have brought great difficulties to the design of the actuation system.Based on the analysis on the hypersonic aircraft mission and platform,this paper systematically discusses the technical challenges of the flight control actuation system,especially on the issues of energy,structure and thermal management.Based on the released information,the state of the art of the high speed aircraft actuation technology development is summarized.The technical development emphases of hypersonic aircraft actuation system are prospected,and the feasible technical routes are given.

关 键 词：高超声速 作动系统 多电化 高压化 灵巧驱动 

分 类 号：V227.8[航空宇航科学与技术—飞行器设计]