Aerodynamic skirt securing connector comprising a stabilizer
A skirt securing connector assembly for securing an aerodynamic skirt panel to a trailer is provided, the skirt securing connector assembly comprising an upper attachment portion adapted to secure the skirt securing connector assembly to the trailer, a lower attachment portion adapted to secure a lower portion of the aerodynamic skirt panel and a strut member connected, at a first end thereof, to the upper portion of the skirt securing connector assembly and connected, at a second end thereof, to the lower portion of the skirt securing connector assembly, the strut member including a longitudinal axis between the first end and the second end, the strut member including a concave portion extending along the longitudinal axis, the concave portion increasing an inertia moment of the strut member to sustain a force applied by air routing on the aerodynamic skirt.
1. A strut member for securing an aerodynamic panel thereto and to be mounted to a floor structure of a trailer, the strut member comprising:
a connector portion comprising a trailer-contacting portion configured to butt up against the floor structure;
a first skirt-contacting portion joined to the connector portion, the first skirt-contacting portion being configured for the aerodynamic skirt panel to be secured thereto;
a substantially linear strut portion joined to the connector portion distant to the first skirt-contacting portion, thereby defining a projection at the strut contacting portion; and
a stabilizer joined to the trailer-contacting portion, the stabilizer extending farther from the first skirt-contacting portion than the projection of the strut portion,
wherein the strut member is configured to be mounted through the connector portion to the floor structure in-between the skirt-contacting portion and the stabilizer,
wherein the connector portion is tapered toward the stabilizer.
2. The strut member of claim 1 , wherein the trailer-contacting portion comprises a surface configured for a securing mechanism to butt up against toward the floor structure to mount the strut member to the floor structure.
3. The strut member of claim 2 , wherein the trailer-contacting portion comprises openings providing passage to a portion of the securing mechanism to extend therethrough.
4. The strut member of claim 3 , wherein the stabilizer is wider than the distance between the openings perpendicular to a central vertical plane of the strut member.
5. The strut member of claim 3 , wherein the openings do not extend through the stabilizer.
6. The strut member of claim 1 , wherein the first skirt-contacting portion comprises a pair of wings that extend in opposed direction to the trailer-contacting portion.
7. The strut member of claim 1 , wherein the strut portion comprises, distant to the skirt contacting a second skirt-contacting portion adapted for the aerodynamic skirt panel to be secured thereto.
8. The strut member of claim 7 , wherein the securing portion and the strut portion define together a concave structure providing clearance between the strut member and the aerodynamic skirt panel to be secured thereto.
9. The strut member of claim 1 , wherein the strut portion extends at an angle of between 60 degrees and 80 degrees relative to the trailer-contacting portion toward the first skirt-contacting portion.
10. The strut member of claim 1 , wherein the securing portion comprises an alignment guided configured to extend beyond the trailer-contacting portion.
11. A skirt securing connector assembly for securing an aerodynamic panel thereto and to be mounted to an I-beam of a trailer, the skirt securing connector assembly comprising:
a strut member comprising:
a connector portion comprising a trailer-contacting portion configured to butt up against the I-beam;
a first skirt-contacting portion configured for the aerodynamic skirt panel to be secured thereto;
a substantially linear strut portion joined to the connector portion distant to the first skirt-contacting portion, thereby defining a projection at the strut contacting portion; and
a stabilizer joined to the trailer-contacting portion, the stabilizer extending farther from the first skirt-contacting portion than the projection of the strut portion; and
a securing mechanism configured to mount the strut member to the I-beam of the trailer,
wherein the strut member is configured to be mounted through the connector portion to the I-beam in-between the first skirt-contacting portion and the stabilizer,
wherein the strut portion comprises, distant to the first skirt-contacting portion, a second skirt-contacting portion adapted for the aerodynamic skirt panel to be secured thereto.
12. The skirt securing connector assembly of claim 11 , wherein the trailer-contacting portion comprises a surface configured for a securing mechanism to butt up against toward the I-beam to mount the strut member to the I-beam.
13. The skirt securing connector assembly of claim 12 , wherein the trailer-contacting portion comprises openings providing passage to a portion of the securing mechanism to extend therethrough.
14. The skirt securing connector assembly of claim 13 , wherein the stabilizer is wider than the distance between the openings perpendicular to a central vertical plane of the strut member.
15. The skirt securing connector assembly of claim 13 , wherein the openings do not extend through the stabilizer.
16. The skirt securing connector assembly of claim 13 , wherein the securing mechanism is adapted to clamp the I-beam.
17. The skirt securing connector assembly of claim 11 , wherein the securing portion and the strut portion define a concave structure providing clearance between the skirt securing connector and the aerodynamic skirt panel to be secured thereto.
18. The skirt securing connector assembly of claim 11 , wherein the strut portion extends at an angle of between 60 degrees and 80 degrees relative to the trailer-contacting portion toward the first skirt-contacting portion.
19. A strut member for securing an aerodynamic skirt panel thereto and to be mounted to a floor structure of a trailer, the strut member comprising:
a connector portion comprising a trailer-contacting portion configured to butt up against the floor structure;
a first skirt-contacting portion joined to the connector portion, the first skirt-contacting portion being configured for the aerodynamic skirt panel to be secured thereto;
a substantially linear strut portion joined to the connector portion distant to the first skirt-contacting portion, thereby defining a projection at the strut contacting portion; and
a stabilizer joined to the trailer-contacting portion, the stabilizer extending farther from the first skirt-contacting portion than the projection of the strut portion,
wherein the strut member is configured to be mounted through the connector portion to the floor structure in-between the skirt-contacting portion and the stabilizer,
wherein the first skirt-contacting portion comprises a pair of wings that extend in opposed direction to the trailer-contacting portion.
20. The strut member of claim 19 , wherein the trailer-contacting portion comprises a surface configured for a securing mechanism to butt up against toward the floor structure to mount the strut member to the floor structure.