装备服役环境特征解析与适应性分析方法

吴卓远; 任战鹏; 周传磊; 刘立彬; 田培强; 吴敬涛

doi:10.7643/issn.1672-9242.2026.06.004

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装备环境工程 ›› 2026, Vol. 23 ›› Issue (6) : 42-55. DOI: 10.7643/issn.1672-9242.2026.06.004

航空航天装备

装备服役环境特征解析与适应性分析方法

吴卓远¹, 任战鹏¹, 周传磊², 刘立彬², 田培强¹, 吴敬涛¹

作者信息 +

Equipment Operational Environment Characterization and Worthiness Analysis Methods

WU Zhuoyuan¹, REN Zhanpeng¹, ZHOU Chuanlei², LIU Libin², TIAN Peiqiang¹, WU Jingtao¹

Author information +

文章历史 +

摘要

为提升装备在复杂服役环境下的全寿命周期可靠性,解决严寒、沙漠、沿海、高原等典型严酷环境下装备失效机理不明晰、环境敏感性参数难确定等关键问题,提出了“环境特征解析-多层级响应分析-耦合失效机制揭示”的系统化研究方法。基于我国典型地理气候特征,划分严寒、沙漠、沿海、高原四大环境区域,提取核心环境参数。通过多学科交叉分析,建立了装备结构特性、机构功能及系统性能的多层级环境响应分析方法,构建了“环境区域-环境类型-环境参数”三级环境特征框架与“装备类型-分系统-部件-性能指标”四级装备对象框架的映射关系。阐明了不同环境参数对运输机/战斗机结构完整性、机构运动可靠性及系统功能稳定性的多物理场耦合失效机制,揭示了无人机电池低温容量衰减与高温热失控、电机沙尘磨损,以及导弹推进剂低温脆化、高原低压燃烧效率下降等关键响应规律。本文构建的多场耦合映射关系系统指导装备环境适应性正向设计,为全域多维战场环境下的装备全寿命周期可靠性提升提供理论支撑与技术路径。

Abstract

The work aims to propose a systematic methodology comprising "environmental characterization, multi-level response analysis, and coupled failure mechanism revelation" to enhance the whole-life-cycle reliability of equipment operating in complex service environments, and to address the critical issues of unclear failure mechanisms and difficult-to-determine environmental sensitivity parameters under typical severe conditions including frigid, desert, coastal, and plateau regions. Based on China's typical geographical and climatic characteristics, four major environmental zones were delineated, and core environmental parameters were extracted. Through multidisciplinary cross-analysis, a multi-level analytical method was established for equipment structural characteristics, mechanism functionality, and system performance environmental response, and a multi-field coupling mapping relationship was constructed between the three-tier environmental characterization framework of "environmental zone-environmental type-environmental parameter" and the four-tier equipment hierarchy of "equipment type-subsystem-component-performance indicator". The multi-physics coupling failure mechanisms affecting the structural integrity, kinematic reliability of mechanisms, and functional stability of transport/fighter aircraft systems under various environmental parameters were elucidated. Key response patterns were revealed, including low-temperature capacity fade and high-temperature thermal runaway of UAV batteries, motor wear caused by sand and dust, low-temperature propellant embrittlement in missiles, and reduced combustion efficiency under plateau hypobaric conditions. The multi-field coupling mapping relationship established herein provides systematic guidance for the forward design of equipment environmental worthiness, offering theoretical underpinning and technical pathways for enhancing equipment whole-life-cycle reliability across global multi-dimensional battlefield environments.

导出引用

吴卓远, 任战鹏, 周传磊, 刘立彬, 田培强, 吴敬涛. 装备服役环境特征解析与适应性分析方法[J]. 装备环境工程. 2026, 23(6): 42-55 https://doi.org/10.7643/issn.1672-9242.2026.06.004

WU Zhuoyuan, REN Zhanpeng, ZHOU Chuanlei, LIU Libin, TIAN Peiqiang, WU Jingtao. Equipment Operational Environment Characterization and Worthiness Analysis Methods[J]. Equipment Environmental Engineering. 2026, 23(6): 42-55 https://doi.org/10.7643/issn.1672-9242.2026.06.004

中图分类号： TJ01 V216.5

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