Aircraft fuel oil pipeline icing ice type research device

The utility model relates to an airplane fuel oil pipeline icing ice type research device, which comprises a quick-opening door type double-layer test oil tank system and a measurement and control system, can be matched with a cooling system and a fuel oil configuration system for use, and passes through the double-layer oil tank system (the outer layer is a cooling medium; the inner layer is a test fuel tank, in addition, automatic simulation of core parameters such as fuel tank gas phase space pressure is achieved through a pressure control system, and finally the icing ice type mechanism of the aircraft fuel pipeline is studied in a test mode. According to the utility model, not only is the test cost greatly reduced, but also the test efficiency is remarkably improved. 本实用新型涉及飞机燃油管路结冰冰型研究装置，其包括快开门式双层试验油箱系统和测控系统，其可与冷却系统及燃油配置系统配套使用，并且通过双层油箱系统(外层为冷却介质，内层为试验油箱)实现对不同燃油温度、降温速率的自动模拟，另外还通过压力控制系统实现对油箱气相空间压力等核心参数的自动模拟，最终通过试验方式，对飞机燃油管路结冰冰型机理进行研究。本实用新型不仅大大降低了试验成本，而且还显著提升了试验效率。