首先介绍了某航空飞行器静力试验系统的组成,在此基础上设计了为保证该静力试验系统安全可靠运行所需要的试验室,重点介绍了该静力试验室的工艺布局、土建设计要点,其设计核心为静力试验区承力柱及地轨的基础设计及施工要求。最后简要介绍了该试验室配套的油源泵房、控制间及工具间等的设计要点。 Firstly, the composition of static test system of an aeronautic aircraft is introduced. On the basis of this, the laboratory required to ensure the safe and reliable operation of the static test system is designed. The layout of the static test chamber, the main points of civil engineering design , Its design core for the static test area bearing column and the basic design and construction requirements of the ground rail. At last, the design essentials of the oil source pump room, control room and tool room of the laboratory are briefly introduced.