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针对民用飞机液压系统排液设计问题,本文对设计要求和关键设计要素等方面进行了研究,并给出了民用飞机液压系统可燃液体排放设计的方法。民用飞机可燃液体主要包括燃油和液压油,两种可燃液体的控制和排放问题有明确的适航条款要求。液压系统作为飞机的重要二次能源系统,其元件、管路分布于全机各大区域,整个系统内的液压油是可燃液体的重要来源,在液压系统的设计过程中就需要充分考虑排液设计要求,满足适航条款要求。本文通过在某型民用飞机可燃液体排
In this paper, the design requirements and key design elements are studied in this paper, and the design of flammable liquid for hydraulic system of civil aircraft is given. Combustible liquids for civil aircraft are mainly composed of fuel oil and hydraulic oil. There are clear airworthiness provisions for the control and emission of two flammable liquids. Hydraulic system as an important secondary energy system of the aircraft, its components, pipelines distributed in major areas of the whole machine, the entire system of hydraulic oil is an important source of flammable liquids in the hydraulic system design process needs to fully consider the drainage Design requirements to meet airworthiness requirements. This article through a type of civilian aircraft combustible liquid row