Flip cover assembly and a flip cover actuating structure for the flip cover assembly
US-11673466-B2 · Jun 13, 2023 · US
US11927045B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11927045-B2 |
| Application number | US-202017252885-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 28, 2020 |
| Priority date | Aug 8, 2019 |
| Publication date | Mar 12, 2024 |
| Grant date | Mar 12, 2024 |
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A fuel filler flap module of a motor vehicle includes a carrier, a fuel filler flap which is pivotably mounted on the carrier and is designed to be movable between a closed position and an open position, and a movement mechanism designed to move the fuel filler flap from the closed position into the open position and back into the closed position. The movement mechanism has a mechanical deployment element which is arranged on the carrier and which is designed to exert a deployment force acting into the open position on the fuel filler flap, wherein the movement mechanism has a motor-driven deployment means which is designed to push the fuel filler flap with an auxiliary force from the closed position up to an initial deployment position, which lies between the closed position and the open position, wherein the auxiliary force is greater than the deployment force.
Opening claim text (preview).
The invention claimed is: 1. A fuel filler flap module of a motor vehicle, comprising a carrier, a fuel filler flap and a movement mechanism, wherein the fuel filler flap is pivotably mounted on the carrier and is designed to be movable between a closed position and an open position, wherein the movement mechanism is configured to move the fuel filler flap from the closed position into the open position and back into the closed position, wherein the movement mechanism has a mechanical deployment element, wherein the mechanical deployment element is arranged on the carrier and is configured to exert a deployment force acting into the open position on the fuel filler flap, wherein the movement mechanism has a motor-driven deployment element configured to push the fuel filler flap with an auxiliary force from the closed position up to an initial deployment position, wherein the initial deployment position lies between the closed position and the open position, wherein the auxiliary force generated by the motor-driven deployment element is greater than the deployment force generated by the mechanical deployment element. 2. The fuel filler flap module according to claim 1 , wherein the fuel filler flap is pivotably mounted about a pivot axis mounted on the carrier, the initial deployment position being a position moved out of the closed position in the direction of the open position, wherein in the initial deployment position the fuel filler flap is arranged pivoted by 2° to 10° about the pivot axis in the direction of the open position with respect to the closed position. 3. The fuel filler flap module according to claim 2 , wherein the mechanical deployment element is a torsion spring wound around the pivot axis, wherein the torsion spring comprises a first spring arm and a second spring arm, wherein the first spring arm is supported on the fuel filler flap and the second spring arm is supported on the carrier. 4. The fuel filler flap module according to claim 2 , wherein the motor-driven deployment element is drive-connected to an output shaft and drives the output shaft, wherein the motor-driven deployment element is mounted on the carrier, wherein the output shaft is mounted on the carrier at a distance from the pivot axis, wherein an eccentric contour is integrally formed on the output shaft, wherein the eccentric contour interacts with the fuel filler flap from the closed position to the initial deployment position if the deployment force of the mechanical deployment element does not push the fuel filler flap from the closed position into the initial deployment position. 5. The fuel filler flap module according to claim 4 , wherein the eccentric contour is designed having a radius, wherein the radius increases with respect to the output shaft, and wherein the radius, during the rotation of the output shaft, is designed to abut on a pivoting arm of the fuel filler flap and to push against the pivoting arm and thereby to push the fuel filler flap into the initial deployment position. 6. The fuel filler flap module according to claim 4 , wherein the eccentric contour is arranged at a distance from the pivoting arm of the fuel filler flap from the initial deployment position up to the open position. 7. The fuel filler flap module according to claim 4 , wherein a disc element is formed on the output shaft and a cable element is provided, wherein the cable element is fixed with a first end to the disc element, and wherein a second end of the cable element is fastened to the fuel filler flap. 8. The fuel filler flap module according to claim 7 , wherein the cable element is connected to the fuel filler flap in such a way that the cable element is designed to guide the movement of the fuel filler flap during the movement of the fuel filler flap from the initial deployment position into the open position against the deployment force of the mechanical deployment element. 9. The fuel filler flap module according to claim 7 , wherein the disc element has a winding contour designed for rolling up and unrolling the cable element. 10. The fuel filler flap module according to claim 9 , wherein the winding contour is designed having at least two different radii continuously merging into one another or is designed to be eccentric.
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