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    • 8. 发明授权
    • Epoxy curing agent
    • 环氧固化剂
    • US3789071A
    • 1974-01-29
    • US3789071D
    • 1971-10-07
    • HITCO
    • BABAYAN E
    • C07C275/18C08G18/58C08G18/80C08G59/40C07C127/12
    • C08G18/58C07C275/18C08G18/808C08G59/4021
    • An improved curing agent for epoxy resin compositions containing a polyepoxide comprising a substituted diurea formed by the reaction of two mols of a secondary amine, preferably an aliphatic amine, such as dimethylamine with one mol of a diisocyanate containing one cycloaliphatic isocyanate group and one aliphatic isocyanate group such as isophorone diisocyanate. The curing temperature of the composition can be substantially increased to provide products having improved properties without the danger of undercuring or substantial shortening of the gel time.
    • 一种环氧树脂组合物的改进固化剂,其含有聚环氧化物,其包含通过两摩尔仲胺,优选脂族胺如二甲胺与1摩尔含有一个脂环族异氰酸酯基的二异氰酸酯和一个脂族异氰酸酯反应形成的取代的二脲 组如异佛尔酮二异氰酸酯。 组合物的固化温度可以显着增加,以提供具有改进性能的产品,而不会出现低凝固或大幅缩短凝胶时间的危险。
    • 9. 发明授权
    • Variable aerodynamic structure
    • 可变的空气动力学结构
    • US3666210A
    • 1972-05-30
    • US3666210D
    • 1969-12-18
    • HITCO GARDENA
    • LOOK LANCE GERICKSON DAVID G
    • B64C3/56B64C3/54
    • B64C3/56Y02T50/145
    • An aerodynamic or airfoil structure for a given span dimension includes a fixed spar or base portion and at least one movable portion comprising a plurality of pivotable rib elements which define a three dimensional aerodynamic structure when extended. The rib elements are hingedly mounted at one end to the fixed portion and at the other to an edge member, so as to form an internally movable parallelogram structure. When the ribs are in the compacted position, they nest against or within the fixed portion, and fold within each other. The aerodynamic or airfoil structure may be in two or more sections that are extendible spanwise through operation of an internal mechanism. Structures of this type may comprise aircraft wings, rotor blades, control surfaces, spoilers, flaps or specialized airfoil devices for atmospheric or reentry vehicles. The airfoils may have either or both trailing and leading edges that are compactible and deployable.
    • 用于给定跨度尺寸的空气动力学或翼型结构包括固定翼梁或基部部分和至少一个可移动部分,该可移动部分包括多个可枢转的肋元件,其在延伸时限定三维空气动力学结构。 肋元件在一端铰接安装到固定部分,另一端铰接安装到边缘部件上,以形成内部可移动的平行四边形结构。 当肋处于压实位置时,它们嵌套在固定部分内或内部,并且彼此折叠。 空气动力学或翼型结构可以是两个或更多个部分,其可以通过内部机构的操作来展开。 这种类型的结构可以包括飞行器机翼,转子叶片,控制表面,扰流板,襟翼或用于大气或再入式车辆的专用翼型装置。 机翼可以具有可压缩和可展开的任何一个或两个尾部和前缘。