Automated system of contactless ultrasound nondestructive quality control of solid fuel rocket engines from composite materials

Pub Date : 2021-07-01 DOI:10.15407/KNIT2021.03.076
A. Kulyk, P. Zheltov, S. Klymenko, V. V. Chabanov
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引用次数: 1

Abstract

Currently, in various industries (engineering, aircraft, energy, etc.) the issue of product quality assurance and control is particularly acute. This is due primarily to the ever-increasing requirements for increasing reliability with increasing loads on products, which entails the strengthening of technical standards. The issue of quality control for rocket and space technology products is especially relevant. Modern power structures of rocket and spacecraft made of polymer composite materials, and especially the body of solid fuel rocket engines (SFRЕ), are multilayer packages of various polymer-composite materials (PKM), obtained and interconnected in the process of manufacturing the body. The efficiency of SFRЕ depends on the quality of the formation of PKM in production conditions. The most important issues are the implementation of production quality control of composite structures, the reliability of control results and the ability to automate the control process. The article presents an automated system of non-contact ultrasonic non-destructive testing, which allows to control the stability of the technological process of forming the composite material of the wall of the SFRЕ body and, if necessary, to adjust it. The probability of detecting zones of anomalous violation of the integrity of the wall material of the SFRЕ housing is carried out due to adaptive algorithms, digital systems of multilevel matrix processing and optimal filtering of the received signals. The automated system of contactless ultrasonic non-destructive quality control of SFRЕ cases allows to register conditions of scanning and control for more visual representation of the defectogram in the expanded look of the case of a product in the course of control and at documentation of its results. The presented results of work on the development of an automated system of non-destructive testing of the integrity of the buildings of the SFRЕ type "cocoon" confirm the possibilities of practical implementation in production.
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复合材料固体燃料火箭发动机非接触式超声无损质量控制自动化系统
目前,在各个行业(工程、飞机、能源等)中,产品质量保证和控制的问题尤为突出。这主要是由于随着产品负载的增加,对可靠性的要求不断增加,这就需要加强技术标准。火箭和空间技术产品的质量控制问题尤其重要。现代用高分子复合材料制成的火箭和航天器的动力结构,特别是固体燃料火箭发动机(SFRЕ)的机体,是在机体制造过程中获得的各种高分子复合材料(PKM)的多层封装,并相互连接。SFRЕ的效率取决于PKM在生产条件下形成的质量。最重要的问题是复合结构生产质量控制的实施、控制结果的可靠性和控制过程自动化的能力。本文介绍了一种自动化的非接触式超声无损检测系统,该系统可以控制SFRЕ阀体壁复合材料成型工艺过程的稳定性,并在必要时进行调整。通过自适应算法、多层矩阵处理数字系统和接收信号的最优滤波,实现了SFRЕ壳体壁材料完整性异常破坏区域的概率检测。SFRЕ案例的非接触式超声无损质量控制自动化系统允许注册扫描和控制条件,以便在控制过程中产品案例的扩展外观中更直观地表示缺陷图,并记录其结果。介绍了对SFRЕ型“茧”建筑完整性无损检测自动化系统的开发结果,证实了在生产中实际实施的可能性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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