Abstract <p>This paper presents an analysis of the design optimization criteria for the suspension units of the main airframe of civil aircraft, an analysis of the relationship between the criteria of the weak links of various suspension units of the main airframe, and a presentation of an algorithm for finding the optimal ratio of these criteria for fastening the suspension units of the main airframe.</p>

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An Approach to Solving the Problem of Designing Critical Components of Modern Airliners

  • E. I. Titov,
  • S. A. Serebryanskii

摘要

Abstract

This paper presents an analysis of the design optimization criteria for the suspension units of the main airframe of civil aircraft, an analysis of the relationship between the criteria of the weak links of various suspension units of the main airframe, and a presentation of an algorithm for finding the optimal ratio of these criteria for fastening the suspension units of the main airframe.