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.
AERODYNAMIC SKIRT ASSEMBLY
2019-09-19
Patent
Electronic Resource
English
IPC: | B62D MOTOR VEHICLES , Motorfahrzeuge / F16M Rahmen, Gehäuse oder Grundplatten von Kraftmaschinen oder anderen Maschinen oder von Apparaten, nicht auf eine besondere Art von Maschine oder Apparat eingeschränkt, die anderweitig vorgesehen ist , FRAMES, CASINGS, OR BEDS, OF ENGINES OR OTHER MACHINES OR APPARATUS, NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUS PROVIDED FOR ELSEWHERE |