Reliability-Driven Analysis, Design and Characterization of Rotorcraft Structures: Decision-Making Framework

M. Gurvich
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Abstract

The objective of this work is a definition of a decision-making framework for reliability-driven assessment and corresponding methods of solutions, considering uncertainty, structural/material imperfections, missed information, randomness of input data, etc. More specifically, such framework is proposed to integrate critical steps including design, analysis, and experimental characterization and is suggested for typical rotorcraft and aircraft structures. The paper highlights details of the framework, key questions to address and proposed decision-making checklist for the assessment. Demonstrations of the framework are shown on cases of analysis, representing real structures, and on design studies based on their system-level understanding. In addition, enhanced solutions are shown for experimental characterization, specifically focused on assessment of variability and imperfections.
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旋翼机结构的可靠性驱动分析、设计和特性:决策框架
考虑到不确定性、结构/材料缺陷、缺失信息、输入数据的随机性等因素,本工作的目标是定义可靠性驱动评估的决策框架和相应的解决方案方法。更具体地说,提出了这样的框架,以整合关键步骤,包括设计,分析和实验表征,并建议典型的旋翼飞机和飞机结构。本文重点介绍了评估框架的细节、需要解决的关键问题和建议的评估决策清单。该框架的演示显示在分析案例上,代表了真实的结构,以及基于系统级理解的设计研究。此外,还展示了用于实验表征的增强解决方案,特别侧重于评估可变性和缺陷。
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