Aerodynamic skirt securing connector comprising a stabilizer
A strut member to be secured to the floor structure includes a top skirt-contacting portion for the aerodynamic skirt panel to be secured thereto, a lower skirt-contacting portion for the aerodynamic skirt panel to be secured thereto distant from the top skirt-contact portion, and a strut portion connecting the top skirt-contact portion to the lower skirt-contacting portion. The strut member provides a clearance in which the skirt panel is free of contact with the strut member between the top skirt-contact portion and the lower skirt-contacting portion. The strut portion is configured to resiliently buckle between a buckled position upon the skirt panel undergoing a force exceeding a threshold value toward the strut member and an original position when no force is applied and when the skirt panel is undergoing a force that is less than the threshold value.
1. A strut member for securing an aerodynamic skirt panel thereto and to be mounted to a floor structure of a vehicle, the strut member comprising:
a vehicle-contacting portion to be secured to the floor structure;
a top skirt-contacting portion for the aerodynamic skirt panel to be secured thereto;
a lower skirt-contacting portion for the aerodynamic skirt panel to be secured thereto distant from the top skirt-contact portion; and
a strut portion connecting the top skirt-contact portion to the lower skirt-contacting portion,
wherein the strut member provides a clearance in which the skirt panel is free of contact with the strut member between the top skirt-contact portion and the lower skirt-contacting portion when the skirt panel is secured thereto, and wherein the strut portion is configured to resiliently buckle between a buckled position upon the skirt panel undergoing a force exceeding a threshold value toward the strut member and an original position when no force is applied and when the skirt panel is undergoing a force that is less than the threshold value.
2. The strut member of claim 1 , wherein the strut portion comprises a first segment having a concave portion facing the aerodynamic skirt panel when assembled to the aerodynamic skirt panel.
3. The strut member of claim 1 , wherein the strut portion comprises a portion that is non parallel to the aerodynamic skirt panel when operatively secured thereto.
4. The strut member of claim 1 , wherein the strut portion comprises a first segment having two co-planar edges and a curved portion connecting the two co-planar edges.
5. The strut member of claim 1 , wherein the top skirt-contacting portion and the lower skirt-contacting portion include co-planar surfaces.
6. The strut member of claim 1 , wherein the strut member resiliently buckles when a force of less than 600 Newtons is applied thereto.
7. The strut member of claim 1 , wherein the strut member resiliently buckles when a force of between about 400 Newtons and about 600 Newtons is applied thereto.
8. The strut member of claim 1 , wherein the lower skirt-contacting portion is for the aerodynamic skirt panel to be non-slidingly secured thereto.
9. The strut member of claim 2 , wherein the strut member has a length, and wherein the first segment extends over at least 30 percent of the strut portion.
10. The strut member of claim 1 , wherein the strut portion next to the top skirt-contacting portion and next to the lower skirt-contacting portion has a constant width.
11. The strut member of claim 1 , wherein the vehicle is a trailer.
12. A strut member for securing an aerodynamic skirt panel thereto and to be mounted to a floor structure of a vehicle, the strut member comprising:
a vehicle-contacting portion to be secured to the floor structure;
a top skirt-contacting portion for the aerodynamic skirt panel to be secured thereto;
a lower skirt-contacting portion for the aerodynamic skirt panel to be secured thereto distant from the top skirt-contacting portion; and
a strut portion connecting the top skirt-contacting portion to the lower skirt-contacting portion, the strut portion comprising a first segment featuring a concave skirt-facing face adapted to resiliently buckle between a buckled position upon the skirt panel undergoing a force exceeding a threshold value toward the strut member and an original position when no force is applied and when the skirt panel is undergoing a force that is less than the threshold value,
wherein the first segment of the strut portion is contact-free from the skirt panel when the skirt panel is secured to the strut member.
13. The strut member of claim 12 , wherein the first segment further comprises a convex face that is for facing in a direction opposed to the aerodynamic skirt panel.
14. The strut member of claim 12 , wherein the strut member provides a clearance in which the skirt panel is free of contact with the strut member between the top skirt-contact portion and the lower skirt-contacting portion.
15. The strut member of claim 12 , wherein the top skirt-contacting portion and the lower skirt-contacting portion include co-planar surfaces.
16. The strut member of claim 12 , wherein the lower skirt-contacting portion is for the aerodynamic skirt panel to be non-slidingly secured thereto.
17. The strut member of claim 12 , wherein the strut portion next to the top skirt-contacting portion and next to the lower skirt-contacting portion has a constant width.