1. 大连理工大学 航空航天学院, 辽宁 大连 116024
2. 中国航天科工集团第六研究院41所, 内蒙古 呼和浩特 010010
*E-mail: dechuans@dlut.edu.cn
收稿:2021-11-26,
网络出版:2023-07-25,
纸质出版:2023-04-28
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孙得川, 贤光. 超声波测量大尺寸固体火箭发动机燃速的关键技术[J]. 兵工学报, 2023,44(4):1097-1106.
Dechuan SUN, Guang XIAN. Key Technology for Ultrasonic Measurement of Burning Rate in Large-scale Solid Rocket Motors[J]. Acta Armamentarii, 2023, 44(4): 1097-1106.
孙得川, 贤光. 超声波测量大尺寸固体火箭发动机燃速的关键技术[J]. 兵工学报, 2023,44(4):1097-1106. DOI: 10.12382/bgxb.2021.0805.
Dechuan SUN, Guang XIAN. Key Technology for Ultrasonic Measurement of Burning Rate in Large-scale Solid Rocket Motors[J]. Acta Armamentarii, 2023, 44(4): 1097-1106. DOI: 10.12382/bgxb.2021.0805.
确定固体火箭发动机工作时的真实燃速是发动机研制中的难题
而利用超声波测量是目前比较可行的方案。综述了利用超声波测量动态燃速和大尺寸发动机燃速的相关技术
并针对低频超声波开展了钢壳体/推进剂组合件的静态试验和钢壳体固体发动机热试车试验验证。通过综述和试验验证指出采用低频超声波是测量大尺寸固体发动机燃速的最可行的方案
提出进一步的研究方向是优化探头布置方案
并给出超声数据处理的建议。
Measuring the true burning rate of a solid rocket motor (SRM) is a challenging problem in SRM research and development. Ultrasonic measurement has been proven to be a feasible solution. This study provides an overview of the related technologies for measuring dynamic and large-scale motor burning rates using ultrasonic technology. Static tests of steel shell/propellant assembly and high-temperature verification tests of the steel shell solid motor are carried out using low-frequency ultrasonic technology. After review and experimental verification
it is determined that low-frequency ultrasonic is the most feasible approach for measuring the burning rate of large-scale SRM. A further research direction is to optimize the probe layout. The study also provides suggestions for ultrasonic data processing.
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