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    • 15. 发明申请
    • REINFORCEMENT SYSTEM UTILIZING A HOLLOW CARRIER
    • 使用中空载体的加固系统
    • US20060267378A1
    • 2006-11-30
    • US11421562
    • 2006-06-01
    • Michael CzaplickiJon Riley
    • Michael CzaplickiJon Riley
    • B62D25/00
    • B62D29/002B29C44/18B29C70/745B62D29/04
    • A system and method for reinforcing at least a portion of a structural member, including at least one hollow carrier, having an exterior shell and an interior portion, which substantially conforms to the dimensions and geometry of the structural member being reinforced; and a lightweight, low density material for filling the interior portion of one or more of the carriers. The material filling one or more of the carriers of the present invention can be a reinforcement material, self-curing material, or a heat activated expandable material. The carrier can be produced by blow molding or rotational molding and has an adhesive material disposed along at least a portion of the exterior shell used to place, adhere, and affix the carrier to a targeted portion of the structural member selected to be structurally reinforced.
    • 一种用于加强包括至少一个中空载体的结构构件的至少一部分的系统和方法,所述至少一个中空载体具有外壳和内部部分,其基本上符合被加固的结构构件的尺寸和几何形状; 以及用于填充一个或多个载体的内部的轻质,低密度材料。 填充本发明的一个或多个载体的材料可以是增强材料,自固化材料或热活化的可膨胀材料。 载体可以通过吹塑或旋转模塑制造,并且具有沿着外壳的至少一部分设置的粘合材料,其用于将载体放置,粘附并固定到被选择为结构增强的结构构件的目标部分。