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    • 153. 发明授权
    • Laminated composite building component
    • 层压复合建筑构件
    • US06205728B1
    • 2001-03-27
    • US08841356
    • 1997-04-30
    • Frank Sutelan
    • Frank Sutelan
    • E04C224
    • B32B3/28B29C44/12B29C70/086B32B5/024B32B2315/085B32B2331/04B60P3/14E04B1/14E04B2/845E04B7/102E04C2/296E04C2/3405E04C2/365E04C3/291E04C2002/3444Y10T428/233Y10T428/24694Y10T428/24996
    • A laminated composite building component, capable of sustained axial stress as a primary support structure and enclosure of a building structure, comprising a lamination of rigid and resilient material, said rigid material formed of sheets with continuous corrugations parallel to the supporting axis and which have opposite faces being bonded to and encapsulated by said resilient material, said resilient material being a cellular foam matrix, an adhesive or fusion that bonds the rigid and resilient material together in either a static or continuous laminating process, said resilient material forming two outer surfaces spaced from the rigid material, said rigid material having opposite lateral edges being exposed from said resilient material, said lateral edges of the rigid material having return flanges for interlocking said laminated composite building component with adjacent building component, and said building components capable of being supplied and distributed in generic lengths and custom field-cut like lumber.
    • 一种层压复合建筑构件,其能够作为主要支撑结构的持续轴向应力和建筑结构的外壳,包括刚性和弹性材料的层压,所述刚性材料由具有平行于支撑轴线的连续波纹的片材形成,并且具有相反的 所述弹性材料是泡沫泡沫基质,粘合剂或熔融物,其以静态或连续层压方法将刚性和弹性材料粘合在一起,所述弹性材料形成两个外表面 所述刚性材料具有相对的侧边缘从所述弹性材料露出的刚性材料,所述刚性材料的所述侧边缘具有用于将所述层压复合建筑构件与相邻建筑构件互锁的返回凸缘,以及能够供应和分配的所述建筑构件 在通用长度a 和自定义切割像木材。
    • 154. 发明授权
    • Blast resistant laminate composite container wall construction
    • 防爆层压复合容器墙体施工
    • US06177368B1
    • 2001-01-23
    • US09039836
    • 1998-03-16
    • Russell J. Fisher
    • Russell J. Fisher
    • B32B526
    • B32B5/26B32B5/024B32B17/02B32B27/12B32B27/304B32B2315/085B32B2605/18B65D88/14B65D90/325F42B39/14Y10S428/911Y10T442/3325Y10T442/335Y10T442/3358Y10T442/3537Y10T442/3569Y10T442/365Y10T442/3707
    • A blast resistant laminate composite container wall construction is provided for a bomb-resistant airline baggage container for withstanding gas-expansion explosives. A PVC substrate core (26) of sufficient thickness, at least about 0.5 inch, is used to provide a substantially rigid container wall. A first layer (28) of 0.02 inch thick woven roving fiberglass is on one side of the core, a second layer (30) of 0.02 inch thick woven roving fiberglass is on the first layer, a third layer (32) of 0.02 inch thick woven roving fiberglass is on the second layer, a fourth layer of 0.03 inch thick random chopped strand fiberglass is on the third layer, a fifth layer of 0.03 inch thick random chopped strand fiberglass is on the fourth layer, a sixth layer of 0.02 inch thick woven roving fiberglass is on the other side of the core, a seventh layer of 0.02 inch thick woven roving fiberglass is on the sixth layer, an eighth layer of 0.02 inch thick woven roving fiberglass is on the seventh layer, a ninth layer of 0.03 inch thick random chopped strand fiberglass is on the eighth layer, and a tenth layer of 0.03 inch thick random chopped strand fiberglass is on the ninth layer.
    • 提供防爆层压复合容器壁结构,用于承受气体膨胀炸药的防弹航空行李箱。 使用具有至少约0.5英寸的足够厚度的PVC基底芯(26)来提供基本上刚性的容器壁。 0.02英寸厚的编织粗纱玻璃纤维的第一层(28)位于纤芯的一侧,在第一层上有0.02英寸厚的编织粗纱玻璃纤维的第二层(30),0.02英寸厚的第三层(32) 编织粗纱玻璃纤维在第二层上,第三层0.03英寸厚的随机短切玻璃纤维在第三层上,第五层0.03英寸厚的随机短切玻璃纤维在第四层上,第六层为0.02英寸厚 编织粗纱玻璃纤维在芯的另一侧,第七层0.02英寸厚的编织粗纱玻璃纤维在第六层上,第八层0.02英寸厚的编织粗纱玻璃纤维在第七层上,第九层为0.03英寸 粗的随机短切玻璃纤维在第八层,第九层为0.03英寸厚的无规短切玻璃纤维层。