Active aerodynamic system with offset actuator
The invention relates to an active aerodynamic system ( 1 ) for vehicles which comprises a moulded plastics structure ( 2 ) arranged to receive movable elements ( 3; 4 ) and an actuator ( 7 ) off-centre with respect to the structure ( 2 ). The system ( 1 ) of the invention comprises a force transmission member ( 5 ) which connects series of movable elements ( 3; 4 ) to each other. The force transmission member ( 5 ) also makes it possible to distribute the forces within the system ( 1 ).
1. An active aerodynamic system for vehicles,
comprising:
a molded plastics structure comprising an upper part and a lower part, the structure being arranged to receive movable components,
at least a first set of movable components and a second set of movable components each comprising at least one movable component,
an actuator that is offset with respect to the structure and configured such that it can set into motion at least one of the movable components of the first set of movable components,
a force transmission member connected to the first set of movable components and to the second set of movable components, said force transmission member configured to transmit forces of one set of movable components to the other, the force transmission member embodying a plane P,
and wherein the force transmission member is connected to the upper part and to the lower part of the structure by pivot connections configured to permit only translational displacements of the force transmission member in a plane parallel to the plane P and such that the force transmission member distributes forces within the system,
wherein the force transmission member is connected to the upper part and to the lower part of the structure by connecting rods forming pivot connections between the force transmission member and the structure.
2. An active aerodynamic system according to claim 1 , wherein the actuator has an output axis and the movable component set in motion by the actuator has an axis of rotation, the output axis and the axis of rotation coinciding.
3. An active aerodynamic system according to claim 1 , wherein two connecting rods together form two collinear pivot connections between the force transmission member and the upper part of the structure and wherein two connecting rods together form two collinear pivot connections between the force transmission member and the lower part of the structure.
4. An active aerodynamic system according to claim 3 , wherein each of the sets of movable components is connected to the force transmission member at least by a pivot connection.
5. An active aerodynamic system according to claim 4 , wherein each movable component is connected to the force transmission member at least by a pivot connection.
6. An active aerodynamic system according to claim 5 , wherein the first set of movable components has a first axis and the second set of movable components has a second axis, the first axis and the second axis intersecting with each other.
7. An active aerodynamic system according to claim 6 , wherein each of the sets of movable components is connected to the force transmission member by a ball joint having freedom along a translation axis.
8. An active aerodynamic system according to claim 7 , wherein one of the movable components of at least one set of movable components is connected directly to another of the movable components of the same set of movable components by a connecting rod.
9. An assembly of a vehicle bodywork part and of an active aerodynamic system for a vehicle according claim 1 , wherein the vehicle bodywork part is a front face of a vehicle.