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MIL-E-5007D《涡轮喷气和涡轮风扇发动机通用规范》和MIL-E-8593A《涡轮轴和涡轮螺桨发动机通用规范》对航空发动机燃油与控制系统附件提出了包括定义、界面、设计、安装、环境条件、标准以及试验考核项目等内容。这两项规范不但内容丰富而且技术先进,要求严格。初步统计,两项规范均有600余条规定,而直接或间接涉及发动机燃油与控制系统附件的条文就有120条左右,约占总条文的1/6强。众所周知,目前世界各先进国家的航空事业
MIL-E-5007D Turbojet and Turbofan Engine Generic Specifications and MIL-E-8593A Turboshafts and Turboprop Propellers General Specifications include a definition, interface, design, and installation for the aeroengine fuel and control system attachment , Environmental conditions, standards and test items such as examination. These two norms not only rich in content and advanced technology, demanding. According to the preliminary statistics, there are more than 600 provisions in both regulations. There are about 120 provisions directly or indirectly involving the annexes to the engine fuel and control system, accounting for about 1/6 of the total provisions. As we all know, aviation in all the advanced countries in the world today