CAJ | 학술논문

吸力供油是民用飞机燃油系统的基本功能，燃油气液状态是影响吸力供油能力的关键性因素。以某型飞机为例，通过严格的试验方法，对吸力供油能力进行了验证，并以试验数据为基础，对燃油气液比进行计算，分析了其产生的影响。研究结果可用于指导飞机燃油系统设计和发动机性能评定。
흡력공유시민용비궤연유계통적기본공능，연유기액상태시영향흡력공유능력적관건성인소。이모형비궤위례，통과엄격적시험방법，대흡력공유능력진행료험증，병이시험수거위기출，대연유기액비진행계산，분석료기산생적영향。연구결과가용우지도비궤연유계통설계화발동궤성능평정。
Fuel vapor and liquid condition is the critical factor for the suction feed, which is the basic function of the fuel system for civil aircraft. The suction feed function for some aircraft is verified as an example in this paper with the strict flight test method. Based on the test data, the vapor and liquid ratio ( V/L) is calculated and the corresponding effect is analyzed. The research can be used on guiding aircraft fuel system design and engine per-formance evaluation.