翼身融合布局客机的客舱设计

廖慧君; 张曙光

翼身融合布局客机的客舱设计

廖慧君¹,
张曙光²

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

基金项目: 国家863资助项目(2006AA11Z219)

详细信息

作者简介:
廖慧君(1984-),男,浙江丽水人,硕士生,lhjnbdx@126.com.

中图分类号: V 223.2
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- 被引次数: 0
出版历程
- 收稿日期: 2008-07-11
- 网络出版日期: 2009-08-31

Design of cabin layout for blended wing body passenger transports

Liao Huijun¹,
Zhang Shuguang²

1.
School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
2. School of Transportation Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

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.
- 翼身融合体 /
- 民机 /
- 适航性 /
- 系列化 /
- 客舱布置
Abstract: 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 parameterization 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.
- blended wing body (BWB) /
- commercial aircraft /
- airworthiness /
- family development /
- cabin layout

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参考文献(1)

[1] Liebeck R H. Design of the blended wing body subsonic transport . AIAA-2002-0002, 2002 [2] Reuther J, Jameson A. Aerodynamic shape optimization of wing and wing-body configuration using control theory . AIAA-95-0123, 1995 [3] 中国民用航空局.中国民用航空规章第25部:运输类飞机适航标准CCAR-25[S] Civil Aviation Administration of China. Transport airplane airworthiness criterion CCAR-25[S](in Chinese) [4] Jenkinson L R, Simpkin P, Rhodes D. Civil jet aircraft design [M]. London: Arnold, 1999:80-104 [5] Mukhopadhyay V. Blended-wing-body fuselage structural design for weight reduction . AIAA-2005-2349, 2005 [6] Bradley K R. A sizing methodology for the conceptual design of blended-wing-body transports . NASA/CR-2004-213016, 2004

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