摘要
随着飞机设计技术的发展,机翼整体油箱已经成为改善飞机性能、减轻飞机质量的一项重要措施。针对波音B737、A320等几个经典机型的机翼整体油箱结构布局、油泵布置和用油顺序进行了分析,以期对整体油箱设计起一定的参考和借鉴作用。
With the development of aircraft design technique, integral fuel tank technique is already employed to improve the aircraft performance and reduce aircraft weight. Integral fuel tank layout, pump layout and using sequence on B737, A320 and other typical aircraft, are discussed in this article with the aim of providing the reference for future wing integral fuel tank design.
出处
《民用飞机设计与研究》
2011年第3期39-44,共6页
Civil Aircraft Design & Research
关键词
经典机型
机翼整体油箱
油泵布置
用油顺序
typical aircraft
wing integral fuel tank
pump layout
using sequence
