固体火箭发动机衬层与药柱脱粘高能X射线检测技术
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(1. 海军航空工程学院科研部,山东 烟台 264001;2. 中国航天科工集团8610厂,湖北 宜昌 444200;3. 中国航天科工集团389厂,呼和浩特 010076)

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V435

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High Energy X-Rays Testing Technology of Solid Rocket Motor Debonds Between Propellant and Liner
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(1. Department of Scientific Researche, NAAU, Yaitai Shandong 264001, China;2. Factory No.8610 of CASI, Yichang Hubei 444200, China; 3. Factory No.389 of CASI, Huhehaote 010076, China)

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    摘要:

    衬层与药柱脱粘严重影响固体火箭发动机的结构完整性和工作安全性,该缺陷的可靠检测至关重要。文章综述了固体火箭发动机高能X射线检测技术现状。基于射线照相检测和工业CT检测手段,评述了固体火箭发动机衬层与药柱脱粘的图像分析和缺陷评判技术。针对该类缺陷,提出了综合应用射线照相技术和工业CT技术进行印证检测的方法,评判结果表明能够满足缺陷检测的可靠性与准确性要求。

    Abstract:

    The debonds between propellant and liner seriously affect the structural integrity and working security of solid rocket motor, and reliable examination to this defect is crucial. In this paper, the research status of high energy X-rays testing technology of solid rocket motor was summarized. Based on radiography testing and industrial CT testing methods, the techniques of image analysis and defects evaluation were reviewed on debonds between propellant and liner of solid rocket motor. For this defect, the comprehensive application of radiography and industrial CT technology was presented by confirmation detection. The evaluation results showed that the reliability and accuracy could meet requirements of defect detection.

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郑伟,邓安华,刘云峰,刘荣臻.固体火箭发动机衬层与药柱脱粘高能X射线检测技术[J].海军航空大学学报,2014,29(4):355-359
ZHENG Wei, DENG An-hua, LIU Yun-feng, LIU Rong-zhen. High Energy X-Rays Testing Technology of Solid Rocket Motor Debonds Between Propellant and Liner[J]. JOURNAL OF NAVAL AVIATION UNIVERSITY,2014,29(4):355-359

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  • 在线发布日期: 2015-04-08
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