A resilient or flexible skirt panel assembly having an integral bracing system is provided. In operation, the bracing system need not attach directly to a trailer base rail. The innovation includes straight, straight-angled and curved skirt panel orientations. Additionally, angled braces, ‘v-braces,’ ‘v-wings,’ and integral rib bracing mechanisms are provided. 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.
Aerodynamic skirt assembly
2017-02-21
Patent
Electronic Resource
English
IPC: | B62D MOTOR VEHICLES , Motorfahrzeuge |