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 |
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代理人 |
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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 |