论文部分内容阅读
通过回顾国军标GJB241—87《航空涡轮喷气和涡轮风扇发动机通用规范》实施七年来,在结构完整性方面碰到的一些问题,并在与国外军用发动机最新标准,美国的MIL—STD—1783《发动机结构完整性大纲》和英国的DEF STAN 00—971《航空燃气涡轮发动机通用规范》对比分析的基础上,对国军标提出了一些修改补充建议。
By reviewing the national military standard GJB241-87 “Aviation Turbine Jet and Turbofan Engine General Code of” implementation of seven years in the structural integrity encountered some problems, and with the latest foreign military standards, the United States MIL-STD-1783 Based on the comparative analysis of “Outline of Engine Structural Integrity” and British DEF STAN 00-971 “General Specification of Aviation Gas Turbine Engine”, some amendments and supplements to the national military standard are proposed.