COMPOSITE USE IN NOSE CONE DESIGNING FOR AIRCRAFTS

R. Nesterenko, A. Magdin, D. Kudryavcev, D. Zhanzakova
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Abstract

The purpose of the work presented in the paper consists in the choice of radio-transparent material that can withstand loads influencing a nose cone of an aircraft during a flight. In the paper there is solved a problem which consists in comparing the characteristics of different materials used in aircraft industry both common materials and composites and in the choice of the most efficient field of materials that meet the requirements of radio-transparency, strength and heat-resistance. The investigation work is carried out by means of the collection, processing and analysis of data obtained through an experimental way and containing information on strength characteristics, radio-transparency characteristics, on the range of operation temperatures, density and rigidity of each kind of material analyzed. On the basis of the investigation results a field of application of the materials under consideration is offered: in accordance with physical characteristics of composites analyzed the most efficient solution will be the application of glass-ceramic composites for manufacturing radio-transparent nose cones exposed to strong temperature changes during short periods of time caused by super-sonic speed achieved during flights and glass-ceramics, but glass-plastic having lower density and heat-resistance – for manufacturing nose cones of sub-sonic planes which are not subjected to such high thermal loads, at that it was defined that aircraft steels and composites based on metal matrix are not suitable for manufacturing nose cones in view of their high density and low radio-transparency.
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复合材料在飞机前锥设计中的应用
本文所介绍的工作的目的在于选择能够承受飞行过程中影响飞机鼻锥的载荷的无线电透明材料。本文解决了飞机工业中不同材料(普通材料和复合材料)的特性比较问题,并在满足无线电透明度、强度和耐热性要求的材料中选择最有效的材料。调查工作是通过收集、处理和分析通过实验方式获得的数据来进行的,这些数据包含了所分析的每种材料的强度特性、辐射透明度特性、工作温度范围、密度和刚度等信息。根据调查结果,提出了正在考虑的材料的应用领域:根据复合材料的物理特性分析,最有效的解决方案将是应用玻璃陶瓷复合材料制造无线电透明鼻锥,该鼻锥在飞行过程中获得的超音速速度会在短时间内产生强烈的温度变化,而玻璃陶瓷,但玻璃塑料具有较低的密度和耐热性-用于制造不受如此高热负荷的亚声速飞机的鼻锥。指出飞机用钢和金属基复合材料密度大、射线透明度低,不宜用于制造机头锥。
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