宽体飞机压力加油系统性能优化设计

IF 4.6 Q1 OPTICS Journal of Physics-Photonics Pub Date : 2023-11-01 DOI:10.1088/1742-6596/2633/1/012002
Hao Gong
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引用次数: 0

摘要

摘要为了降低宽体飞机加油过程的时间成本,提高机场运行效率,对压力加油系统的设计策略进行了创新。优化了换料过程中关闭阀的操作顺序。设计了压力加油系统燃油管路上的通孔直径。对不同工况下的压力加注性能进行了仿真分析。结果表明,通过优化燃油管路孔板设计和优化翼舱内侧截止阀操作顺序等压力加油工艺策略设计,可以提高不同工况下压力加油系统的性能。
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Performance optimization design of wide-body aircraft pressure refueling system
Abstract In order to reduce the wide body aircraft refueling process time-cost and improve the airport operation efficiency, pressure refueling system design strategy was innovated. The shutoff valves’ operation sequence in refueling process was optimized. The diameter of the orifices on the pressure refueling system fuel line was designed. Pressure refueling performance was simulated and analyzed at different scenarios. The results show that it can improve the pressure refueling system performance at different scenarios by optimizing the pressure refueling process strategy design including optimizing the fuel line orifice design and optimizing the wing tank inner side shut-off valve operation sequence.
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来源期刊
CiteScore
10.70
自引率
0.00%
发文量
27
审稿时长
12 weeks
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