热脉冲去毛刺方法的发展分析

Aleksey Losev, Valeriy Sikulskyi, Hanna Seleznova, Igor Bychkov, Iurii Vorobiov
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摘要

本文的研究课题是利用爆轰混合气体燃烧热脉冲法去除金属加工中获得的细部毛刺的过程的理论和实验研究。本文的目的是证实使用热脉冲方法来完成零件,这是哈尔科夫航空研究所在20世纪70年代早期开发的,用于灵活自动化清洁航空和火箭航天设备液压和燃料单元零件的表面和边缘,使其免受毛刺和技术污染。任务是确定热脉冲法的特点,从其加工具有复杂内外表面的零件边缘的应用角度出发,确定工艺过程的参数,并揭示其在精密工程中的应用潜力。所使用的研究方法是使用有限元方法和实验方法来模拟过程,以检查所提出的数值模型的充分性。得到了以下结果:不同导热系数材料的零件加工,橡胶制品的清洗,铝合金零件螺纹孔边缘的熔化磨圆。所得结果的科学性和实用性新颖性体现在:给出了热脉冲加工的工艺可能性、合理的控制参数和加工方式的优化;考虑部件元件的加热过程和起爆混合物在设备工作室内的燃烧过程;获得了脉冲加热、恒定加热和混合加热过程中液体和零件结构元件温度场的变化规律,从而可以在材料的几种热物理性质中考虑零件的结构特征,形成零件的热脉冲加工体系;利用T-15装置的建模和实验改进结果,开发了热脉冲去除毛刺、微粒和边缘尺寸圆角的工艺。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Аналіз розвитку термоімпульсного методу видалення задирок
The subject of study in this article is theoretical and experimental studies of the process of removing burrs in the details obtained by metalworking using the thermopulse method of combustion of detonating gas mixtures. The purpose of this article is to substantiate the use of the thermopulse method for finishing parts, which was developed at Kharkiv Aviation Institute in the early 70s of the 20th century for the flexible automation of cleaning the surfaces and edges of parts of hydraulic and fuel units of aviation and rocket-space equipment from burrs and technological contamination. The task was to determine the features of the thermal pulse method, the parameters of the technological process from the viewpoint of its application for processing the edges of parts with complex internal and external surfaces, and to reveal its potential for use in precision engineering. The research methods used are the modeling of processes using the finite element method and an experimental method for checking the adequacy of the proposed numerical models. The following results were obtained: processing of parts made of materials with different thermal conductivities, cleaning of rubber products, and rounding of the edges of threaded holes of aluminum alloy parts by melting. The scientific and practical novelty of the obtained results is as follows: the technological possibilities of thermopulse processing, justified control parameters, and optimization of processing modes are given; to consider the processes of heating the elements of the part and the combustion of detonating mixtures in the working chamber of the equipment; obtained regularities of changes in the temperature fields of liquids and structural elements of parts during pulsed, constant, and mixed heating, which make it possible to form regimes of thermopulse processing of parts considering their structural features in several thermophysical properties of materials; developed processes of thermal pulse removal of burrs, microparticles, and dimensional rounding of edges using the results of modeling and experimental refinement on T-15 installations.
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