含硼推进剂的点火燃烧及推进性能研究  

Research on Ignition and Combustion Characteristics and Propulsion Performance of Boron-containing Propellants

作　　者：刘欢[1] 李和平[2] 徐江荣[1] 刘建忠[2] LIU Huan LI Heping XU Jiangrong LIU Jianzhong(Institution of Energy, Hangzhou Dianzi University, Hangzhou Zhejiang 310018, China State Key Laboratory of Clean Energy Utilization, Zhejiang University, Hangzhou Zhejiang 310027, China)

机构地区：[1]杭州电子科技大学能源研究所,浙江杭州310018 [2]浙江大学能源清洁利用国家重点实验室,浙江杭州310027

出　　处：《杭州电子科技大学学报（自然科学版）》2017年第3期73-78,共6页Journal of Hangzhou Dianzi University：Natural Sciences

基　　金：浙江省自然科学基金资助项目(LQ14E060004);科技集团公司航天科技创新基金资助项目(YF-2014-0106-wx)

摘　　要：搭建了激光点火实验台,设计不同尺寸和结构的微小燃烧室用以研究含硼推进剂在微小燃烧室中的点火燃烧特性及推进性能.实验结果表明:大管径有利于点火且利于燃烧充分,但是燃烧速度较慢,而小管径有利于提高推进性能;喷嘴管的燃烧速度稍微大于直管,但是直管的点火性能最优且燃烧强度大,而突变管的推进性能最优.In order to study the ignition and combustion characteristics and propulsion performance of boron-containing propellant in the small-sized combustion chamber, a laser ignition test-bed was established and some small-sized combustion chambers with different size and structure were designed. The results show that： the large diameter is beneficial to ignition and combustion but has low combustion velocity, and the small diameter is helpful to improve the propulsion performance; the tube without nozzle has better ignition property and stronger burning intensity but a little lower combustion velocity than the tubes with nozzle, and the mutated tube has the best propulsion performance.

关 键 词：含硼推进剂 激光点火 燃速 推力 冲量 

分 类 号：V512[航空宇航科学与技术—航空宇航推进理论与工程]