经典机型的机翼整体油箱布置分析  

Wing Integral Fuel Tank Layout Analysis of Typical Aircraft

作　　者：张明星[1] 

机构地区：[1]上海飞机设计研究院结构设计研究部,上海200232

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

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.

关 键 词：经典机型 机翼整体油箱 油泵布置 用油顺序 

分 类 号：V267[航空宇航科学与技术—航空宇航制造工程]