Application Factors Affecting the Weight of Aerospace Static Inverters

L. Walker
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Abstract

The purpose of this paper is to reconcile the wide range of weights quoted for aerospace static inverters of the same VA rating. The inverters discussed are of conventional input and output: 15 to 500 vdc input and 400 cps sine wave output. Specification and application factors affecting inverter weight are tabulated. Graphical relationships are given for the effects of some factors for which relationships can be defined. Trends are indicated for the weight effect of factors for which graphical relationships are not given. The data presented should be useful to systems designers, in avoiding undue inverter weight, by proper specification and application of static inverters.
影响航空航天静态逆变器重量的应用因素
本文的目的是对相同额定电压的航空航天静态逆变器所引用的广泛权重进行调和。所讨论的逆变器是常规输入和输出:15至500 vdc输入和400 cps正弦波输出。表列了影响逆变器重量的规格和应用因素。给出了一些可以定义关系的因素的影响的图形关系。对于没有给出图形关系的因素的权重效应,指出了趋势。所提供的数据应该对系统设计人员有用,通过适当的规范和应用静态逆变器来避免不必要的逆变器重量。
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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