Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: There is provided a method of securing a strut portion to an I-beam of a vehicle, the securing mechanism comprising a pair of opposed clamps, each including a gripping portion, a securing portion, an abutting portion and a fastener adapted to apply tension on the clamps toward each other for moving the clamps toward each other and compress the strut portion to the I-beam.

Abstract: 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.

Abstract: 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.

Abstract: There is provided a method of securing a strut portion to an I-beam of a vehicle, the securing mechanism comprising a pair of opposed clamps, each including a gripping portion, a securing portion, an abutting portion and a fastener adapted to apply tension on the clamps toward each other for moving the clamps toward each other and compress the strut portion to the I-beam.

Abstract: Aerodynamic skirt systems are used to reduce air drag of a vehicle. The present aerodynamic skirt system comprises a skirt panel, a plurality of struts, each strut comprising an upper portion for securing an upper portion of the skirt panel to the trailer, a strut member connected, at a first end thereof, to the upper portion of the strut, a lower portion for securing a lower portion of the skirt panel, the lower portion being connected to the strut member at a second end thereof, the strut member including a concave portion adapted to sustain a force applied by air routing on the aerodynamic skirt in an aerodynamic configuration thereof, the strut member being adapted to buckle and bend when a force exceeding a buckling threshold is applied on the aerodynamic skirt to move the aerodynamic skirt in an object avoidance configuration. A kit and a method of use thereof is also presented.

Abstract: There is provided a securing mechanism for securing a strut portion to an I-beam, the securing mechanism comprising a pair of clamps, each including a gripping portion, a securing portion, an abutting portion and a fastener for applying tension on the clamps toward each other for moving the clamps toward each other. A kit thereof and a method of installing the securing mechanism are also contemplated in the present application.

Abstract: An apparatus for reducing air drag on a vehicle is hereby presented, the apparatus is comprising a panel including a surface thereof disposed between a first surrounding flow of air about the vehicle, on a first side of the panel, and a second surrounding flow of air about the vehicle, on a second side of the panel, the first surrounding flow of air being proximally located in respect with the longitudinal axis of the vehicle, the second surrounding flow of air being distally located in respect with the longitudinal axis of the vehicle, the first surrounding flow of air including a lower air velocity than the second surrounding flow of air, the panel including a serrated trailing edge thereof for creating vortexes and reducing air drag of the vehicle when the vehicle is moving forward.

Abstract: There is provided a securing mechanism for securing a strut portion to an I-beam, the securing mechanism comprising a pair of clamps, each including a gripping portion, a securing portion, an abutting portion and a fastener for applying tension on the clamps toward each other for moving the clamps toward each other. A kit thereof and a method of installing the securing mechanism are also contemplated in the present application.

Abstract: Aerodynamic skirt systems are used to reduce air drag of a vehicle. The present aerodynamic skirt system comprises a skirt panel, a plurality of struts, each strut comprising an upper portion for securing an upper portion of the skirt panel to the trailer, a strut member connected, at a first end thereof, to the upper portion of the strut, a lower portion for securing a lower portion of the skirt panel, the lower portion being connected to the strut member at a second end thereof, the strut member including a concave portion adapted to sustain a force applied by air routing on the aerodynamic skirt in an aerodynamic configuration thereof, the strut member being adapted to buckle and bend when a force exceeding a buckling threshold is applied on the aerodynamic skirt to move the aerodynamic skirt in an object avoidance configuration. A kit and a method of use thereof is also presented.

Abstract: This invention relates to a gap-reducer for reducing a gap between a road tractor and a trailer attached thereto, the gap-reducer comprising a top portion and a bottom portion, the bottom portion being located further forward than the top portion when the gap-reducer is secured on the trailer in an operating position. The gap-reducer extending over the width of the trailer to reduce the drag of the trailer.

Abstract: This invention relates to a gap-reducer for reducing a gap between a road tractor and a trailer attached thereto, the gap-reducer comprising a top portion and a bottom portion, the bottom portion including a flange sized and designed to match and secure an uneven front trailer surface. The gap-reducer can also be equipped of matching corners adapted to match corresponding corners of the trailer.