发明名称 AERODYNAMIC SKIRT ASSEMBLY
摘要 A resilient or flexible skirt panel assembly having an integral bracing system is disclosed. In operation, the bracing system need not attach to a trailer base rail. The innovation discloses straight, straight-angled and curved skirt panel orientations. Additionally, angled braces, ‘v-braces,’ ‘v-wings,’ and integral rib bracing mechanisms are disclosed. In aspects, the skirt panel and bracing mechanisms can absorb (or bend) under force while effectively having a ‘memory’ to return to their original shape upon removal of the force. The skirt assembly can include a hem along the bottom edge of the skirt panel thereby enhancing performance and longevity of the assembly. Additionally, an “anti-skid” clamping assembly can be employed to connect the skirt assemblies to the trailer I-beam, base rail or cross-members.
申请公布号 US2015183473(A1) 申请公布日期 2015.07.02
申请号 US201514656231 申请日期 2015.03.12
申请人 Grandominico Gary Alan;Grandominico Dominic Plauche;McDonald, JR. Raymond Augustus;Moss Bret Jameson 发明人 Grandominico Gary Alan;Grandominico Dominic Plauche;McDonald, JR. Raymond Augustus;Moss Bret Jameson
分类号 B62D35/02;B62D65/16;B62D35/00 主分类号 B62D35/02
代理机构 代理人
主权项 1. A system that facilitates aerodynamics, comprising: a skirt panel configured for installation upon a trailer; and a brace that provides structural support to the skirt panel, wherein the structural support resists wind deflection and wherein the brace comprises a vertical portion with a height at least half of the height of the skirt panel and wherein the vertical portion is wholly positioned within an interior portion of the skirt panel.
地址 Galena OH US