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    • 2. 发明申请
    • TUBULAR MEMBERS INTEGRATED TO FORM A STRUCTURE
    • 组合成员组合形成一个结构
    • WO0157354A2
    • 2001-08-09
    • PCT/US0102048
    • 2001-01-22
    • CHAPMAN W CULLEN JR
    • CHAPMAN W CULLEN JR
    • B64C1/00E21B
    • B29D24/004B29C53/60B29C53/821B29C53/822B29C70/32B29L2031/3076B64C1/06B64C2001/0072Y02T50/433
    • Integrally stiffened and formed, load carrying structures comprising a plurality of elongated thin-walled tubes placed co-extensively in a complementary side-by-side fashion which together form a hollow structure having a desired external contour. Integral skins forming the external and internal surfaces of the structure cooperatively therewith. The structure can be formed with an underlying internal support member spanning the interior of the load carrying structure, thereby connecting opposite sides of the structure together. Also, each of the tubes are wound with fibers in controlled orientations generally paralleling the direction of the loads applied to the tubes to optimize the strength to weight ratio of the tubes. Still a number of embodiments are disclosed to couple two structures together. In addition, an apparatus and method is disclosed to form a window opening within the fuselage and to install a window covering that is both time saving and cost efficient.
    • 整体加强和形成的承载结构包括多个细长的薄壁管,其以互补的并排方式共同放置,共同形成具有期望的外部轮廓的中空结构。 与该结构的外表面和内表面协同地形成的整体表皮。 该结构可以形成有横跨负载承载结构的内部的底部内部支撑构件,从而将结构的相对侧连接在一起。 而且,每个管子以受控取向通常与施加到管子的负载方向平行的纤维缠绕,以优化管子的强度与重量比。 公开了许多实施例以将两个结构耦合在一起。 此外,公开了一种在机身内形成窗口开口并安装既节省时间又节省成本的窗户覆盖物的装置和方法。
    • 8. 发明申请
    • LATTICE SUPPORT STRUCTURE
    • LATTICE支持结构
    • WO2013102221A1
    • 2013-07-04
    • PCT/US2012/072334
    • 2012-12-31
    • SIGMA-TEK, LLC
    • RIDGES, Michael, D.WILSON, Erich, A.KIPP, Michael, D.
    • F16S3/08B29C70/06E04H12/00E04B1/19
    • B29C53/566B29C53/822B29C70/222B29C70/30B32B1/08E04C3/36E04H12/10Y10T428/1393
    • The present disclosure is drawn to a lattice support structures and methods of making such structures, including tooling and articles used therein. In one embodiment, a method for forming a composite lattice support structure can comprise: obtaining a semi-rigid mold having semi-rigid channels, at least some of the semi-rigid channels intersecting at strategic locations; laying up a fiber material, in the presence of a resin, within the semi-rigid channels forming a lay- up within the semi-rigid channels, such that the lay-up extends above the surface of the mold; consolidating the lay-up to form composite cross supports having a pre-determined lateral cross-sectional area controlled by a cross-sectional area of the channels, and that intersect to form nodes, thereby forming the composite lattice support structure; and subjecting the composite lattice support structure to a particulate, wherein the composite lattice support structure is at least partially submerged in the particulate and systematically rotated to cause the particulate to contact the various surfaces of the cross supports and nodes thereby reducing at least of portion of material on the surfaces.
    • 本公开涉及一种格子支撑结构和制造这种结构的方法,包括其中使用的模具和制品。 在一个实施例中,用于形成复合格子支撑结构的方法可以包括:获得具有半刚性通道的半刚性模具,至少一些半刚性通道在战略位置相交; 在半刚性通道内在树脂存在下铺设纤维材料,在半刚性通道内形成叠层,使得叠层在模具表面上方延伸; 固定叠层以形成具有由通道的横截面面积控制的预定横向横截面积并且相交以形成节点的复合交叉支撑,从而形成复合格架支撑结构; 并将所述复合晶格支撑结构经受颗粒状物,其中所述复合晶格支撑结构至少部分地浸没在所述颗粒中并且被系统地旋转以使所述颗粒接触所述交叉支撑件和所述节点的各个表面,从而将至少部分 表面材料。