翼身融合布局客机的客舱设计  

Design of cabin layout for blended wing body passenger transports

作　　者：廖慧君[1] 张曙光[2] 

机构地区：[1]北京航空航天大学航空科学与工程学院,北京100191 [2]北京航空航天大学交通科学与工程学院,北京100191

出　　处：《北京航空航天大学学报》2009年第8期986-989,共4页Journal of Beijing University of Aeronautics and Astronautics

基　　金：国家863资助项目(2006AA11Z219)

摘　　要：翼身融合作为一种新型民机布局,其客舱设计较常规布局有很大不同.以翼身融合布局客机客舱为研究对象,结合其自身特性,确定了与客舱设计相关的适航条例和舒适性要求;确定基本布局方案和客舱参数化设计方法;以250座三级布置为例,对客舱区座椅和设施等进行了详细布置.结果表明,翼身融合布局客舱的参数化方法是可行的,能够满足飞机系列化发展对客舱灵活布置的需要.但应急撤离设计方案是否满足90 s撤离适航要求的应急疏散问题还有待进一步的实验验证.The blended wing body （BWB） commercial aircraft configuration has become a hot topic and has been widely studied around the world. As a new configuration, its cabin design is very different from the conventional, so it＇s necessary to study the new problems with the BWB cabin design. Focused on the marked traits, some basic cabin-relative issues were studied. The cabin layout must meet the CCAR-25 criteria, as well as the passengers＇ comfort need, so the cabin related airworthiness and comfort items were firstly abstracted. A cabin layout solution and the accompanying parameterization method were followed. The 250 seating BWB transport was then taken as example for the details of layout design. The results show that the parameter- ization method of the cabin layout is feasible for the need of a BWB family. However, such requirements as emergent evacuation within 90 seconds must be further highlighted and verified by experiments.

关 键 词：翼身融合体 民机 适航性 系列化 客舱布置 

分 类 号：V223.2[航空宇航科学与技术—飞行器设计]