张永杰1, 吴莹莹1, 赵书旺2, 司江涛3, 袁昌盛1
收稿日期:
2019-04-02
修回日期:
2019-04-07
出版日期:
2019-09-15
发布日期:
2019-05-15
通讯作者:
张永杰
E-mail:zyj19191@nwpu.edu.cn
基金资助:
ZHANG Yongjie1, WU Yingying1, ZHAO Shuwang2, SI Jiangtao3, YUAN Changsheng1
Received:
2019-04-02
Revised:
2019-04-07
Online:
2019-09-15
Published:
2019-05-15
Supported by:
摘要: 翼身融合布局飞机具有大升阻比、低阻力、低噪声等优点,是未来民机最具潜力的发展方向之一;但由于特殊布局所采用的非圆截面增压机身,给翼身融合布局民机结构设计带来了巨大挑战。为了降低非圆截面机身承受增压载荷时产生的高弯曲应力、提高机身结构稳定性及承载效率,翼身融合民机机身结构设计先后经历了圆柱组合式多舱室机身、双蒙皮多舱室机身、带加强支撑的盒式机身、基于拉挤杆缝合高效一体化结构(Pultruded Rod Stitched Efficient Unitized Structure,PRSEUS)的盒式中央机体等发展阶段,其中最具承载优势和可实现性的是由美国国家航空航天局NASA和波音公司共同提出的基于PRSEUS盒式中央机体结构设计方案。PRSEUS结构不仅充分利用了复合材料一体化缝合、整体共固化、低成本等制造优势,而且具有抗拉伸/压缩、多路径止损/止裂、刚度和稳定性裕度大、承载效率高、易金属修补等优异的力学特性,已被拓展应用到了翼身融合民机机翼等结构设计中。本文以非圆截面机身结构设计为重点,回顾了翼身融合民机结构设计发展历程;从整机身结构、关键部件结构、整机优化设计等方面详细阐述了翼身融合民机结构设计的研究进展与发展现状,基于国外相关技术研究发展趋势,提出了中国翼身融合民机机身结构设计研究未来需要重点关注的方向。
中图分类号:
张永杰, 吴莹莹, 赵书旺, 司江涛, 袁昌盛. 翼身融合布局民机非圆截面机身结构设计研究综述[J]. 航空学报, 2019, 40(9): 623054-623054.
ZHANG Yongjie, WU Yingying, ZHAO Shuwang, SI Jiangtao, YUAN Changsheng. Review of non-circular cross-section fuselage structure design research on blended-wing-body civil aircraft[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(9): 623054-623054.
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