基本信息:
- 专利标题：
- 申请号：DE60036234 申请日：2000-07-18
- 公开(公告)号：DE60036234D1 公开(公告)日：2007-10-11
- 发明人： AMAOKA KAZUAKI , NAGAO TAKAYUKI , HARADA ATSUSHI , TAKIZAWA NAOYA , HIDEYUKI SANO , TOI YASUHIRO , HIRAKI MEGUMI
- 申请人： FUJI HEAVY IND LTD
- 专利权人： FUJI HEAVY IND LTD
- 当前专利权人： FUJI HEAVY IND LTD
- 优先权： JP20445199 1999-07-19; JP22163799 1999-08-04; JP27850099 1999-09-30
- 主分类号： B64C3/00
- IPC分类号： B64C3/00 ; B64C3/18 ; B64C3/24 ; B64F5/00
摘要：
A wing (1) of composite material has an upper skin (2), a lower skin (3) and a plurality of intermediate spars (4) arranged between the upper (2) and the lower skin (3). The intermediate spars (4) extend from roots to tips of the upper (2) and the lower skins (3). The intermediate spars (4) are integrally formed with the upper (2) and the lower skins (3) or are adhesively bonded to the upper (2) and the lower skins (3). The wing (1) has a small number of parts, needs greatly reduced time for fabrication and can be fabricated at a low cost.
公开/授权文献:
- DE60036234T2 公开/授权日：2008-05-21