航空发动机模块化设计关键技术研究与展望  

Research and prospective on key technologies of modular design for aero-engines

作　　者：黄维娜 朱晓泉 潘辉 贺文虎 HUANG Weina;ZHU Xiaoquan;PAN Hui;HE Wenhu(AECC Sichuan Gas Turbine Establishment,Chengdu 610500,China)

机构地区：[1]中国航发四川燃气涡轮研究院,成都610500

出　　处：《燃气涡轮试验与研究》2025年第2期4-12,共9页Gas Turbine Experiment and Research

摘　　要：面向军事装备敏捷派生与视情维修的迫切需求,采用模块化设计理念,将复杂系统分解为若干个标准化、规格化独立模块单元,可显著提升装备维修性水平并实现基于模块复用的多平台快速派生发展。简要分析了航空发动机模块化设计的主要实施思路与关键技术路线,且通过理论分析与工程实践相结合,剖析了每项关键技术存在的难点与挑战,据此提出了其具体实现路径,并结合当前技术基础展望了未来发展趋势。In response to the urgent need for agile derivation and condition based maintenance for military equipment,modular design is applied to decompose complex systems into several standardized and normalized independent units,which can significantly enhance the maintainability level of equipment and enable rapid multi-platform development based on module reuse.The main implementation ideas and key technical routes of modular design for aero-engines was analyzed briefly.Through a combination of theoretical analysis and engineering practice,the difficulties and challenges of key technologies were investigated to propose detailed implementation roadmap and development trends based on current technological foundations.

关 键 词：航空发动机 模块化设计 系统工程 正向研发 敏捷派生 视情维修 关键技术 

分 类 号：V23[航空宇航科学与技术—航空宇航推进理论与工程]