基本信息:
- 专利标题： FLYAWAY KABOBS
- 申请号：PCT/US2008/076207 申请日：2008-09-12
- 公开(公告)号：WO2009036296A1 公开(公告)日：2009-03-19
- 发明人： ASHTON, Larry, J. , ALLMAN, Michael, G. , WHITE, Troy, L. , STARK, Danny, L.
- 申请人： SPECTRUM AERONAUTICAL, LLC
- 申请人地址： 2036 Palomar Airport Road Carlsbad, CA 92011 US
- 专利权人： SPECTRUM AERONAUTICAL, LLC
- 当前专利权人： SPECTRUM AERONAUTICAL, LLC
- 当前专利权人地址： 2036 Palomar Airport Road Carlsbad, CA 92011 US
- 代理机构： NYDEGGER, Neil, K. et al.
- 优先权： US11/855,357 20070914
- 主分类号： B64C3/24
- IPC分类号： B64C3/24
摘要：
An aircraft wing made of a composite material, and its method of manufacture, require a plurality of kabobs (i.e. substantially rectangular shaped hollow tubes having an open end and a closed end). Of these kabobs, several are aligned end-to-end, to create a section. Several sections are then positioned side-by-side and covered by a layer of composite material to define an aerodynamic surface for the wing. The juxtaposed sections also establish spar webs for the wing, and the closed ends of the juxtaposed sections establish transverse ribs for the wing. Thus, the kabobs form the main load-bearing member of the wing. The sections of composite material are co-cured with the composite material of the aerodynamic surface.
摘要（中）：
由复合材料制成的飞机机翼及其制造方法需要多个卡布巴（即具有开口端和封闭端的大致矩形的中空管）。 在这些kabobs中，几个对齐端到端，以创建一个部分。 然后将几个部分并排设置并被一层复合材料覆盖以限定机翼的空气动力学表面。 并列部分还建立翼的翼梁网，并列的部分的封闭端设置用于机翼的横向肋。 因此，卡布尔形成机翼的主承重构件。 复合材料的截面与空气动力学表面的复合材料共同固化。
IPC结构图谱:
| B | 作业；运输 |
| --B64 | 飞行器；航空；宇宙航行 |
| ----B64C | 飞机；直升飞机 |
| ------B64C3/00 | 机翼 |
| --------B64C3/24 | .模压结构或铸造结构 |