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从失效到失能——服役/作战完整性的发展历程OA

From failure to incapacity:development of operational integrity

中文摘要英文摘要

早期的装备结构和功能比较简单,对装备质量特性的研究多从失效故障的角度展开.随着对装备要求的不断提高,装备逐渐趋于复杂化、多功能化,随之而来的是更多样的故障和失效模式.对装备的质量控制早已不只是简单的防止失效,而是着眼于防止其功能性能的退化,也就是防止装备的失能.事实上,最终装备的退化表现为功能性能的退化,本文系统地回顾了针对装备失效故障进行质量控制的历程,阐述了装备维修性、可靠性、安全性、测试性、生存性、修复性等发展过程.总结了直接影响装备功能性能发挥的质量控制参数,分析了装备保障性、环境适应性、电磁兼容性、体系兼容性的发展历程.在此基础上,介绍了装备服役/作战完整性的发展历程,明确了数字孪生技术已成为实现和保持装备服役/作战完整性的重要途径.

In the early days,the structure and function of equipment were relatively simple,and the research on the quality characteristics of equipment was mostly carried out from the perspective of failure faults.With the continu-ous improvement of requirements for equipment,it is gradually becoming more complex and multi-functional,and along with this comes a greater variety of faults and failure modes.The quality control of equipment is no longer merely about preventing failure,but rather focuses on preventing the degradation of its functional performance,that is,preventing the equipment from becoming dysfunctional.In fact,the degradation of the equipment is manifested as the degradation of functional performance finally.This paper systematically reviews the process of quality control for equipment failure and faults,and elaborates the development process of equipment maintainability,reliability,safety,testability,survivability,repairability,etc.The quality control parameters that directly affect the functional performance of the equipment are summarized,and the development processes of equipment supportability,envi-ronmental adaptability,electromagnetic compatibility and system compatibility are analyzed.On this basis,the de-velopment process of equipment operational integrity is introduced,and it is clarified that digital twin technology has become an important way to achieve and maintain the operational integrity of equipment.

何宇廷

空军工程大学 航空工程学院,西安 710038

航空航天

服役/作战完整性失效失能装备质量特性可靠性修复性数字孪生

operational integrityfailureincapacityequipment quality characteristicsreliabilityrecoverabilitydigital twin

《航空工程进展》 2026 (2)

1-19,19

国家自然科学基金(52575191)

10.16615/j.cnki.1674-8190.2026.02.01

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