军用航空发动机适航符合性验证及表明模式研究  

Pattern of verification and demonstration of airworthiness compliance for military aero-engine

作　　者：晏祥斌 黄红超 芦振平 卿华 周玉波 YAN Xiangbin;HUANG Hongchao;LU Zhenping;QING Hua;ZHOU Yubo(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》2023年第6期1-7,共7页Gas Turbine Experiment and Research

摘　　要：军用航空发动机引入和贯彻适航理念对于提升其安全水平和品质具有促进作用。我国军用航空发动机适航理念的贯彻体现出要求多源性、验证融合性及符合性表明独立性等特点。在探索军用航空发动机适航理念贯彻模式和解析适航符合性验证及表明业务域基础上,提出一种军用航空发动机适航符合性验证及表明模式。所提出的模式对我国军用航空发动机研制贯彻适航理念,保证及提升其最低安全水平具有积极的参考作用。To introduce and implement airworthiness concept for military aero-engine is helpful to promote its safety level and quality.Implementation of airworthiness concept in military aero-engine in China shows some characteristics,such as the diversity of requirements,fusion characteristic of verification,and independent indication characteristic of conformity.Based on exploration of military aero-engine airworthiness concept implementation pattern and resolving of airworthiness compliance verification and demonstration business domain,a verification and demonstration pattern of airworthiness conformity for aero-engine was proposed,which is referential to ensure and improve minimum level of safety for implement airworthiness concept in development of military aero-engine.

关 键 词：军用航空发动机 适航性 适航符合性验证 符合性表明 模式 最低安全水平 

分 类 号：V23[航空宇航科学与技术—航空宇航推进理论与工程]