Granted Patent B2

US 9,670,833 · App. 13/208,258 · Granted Jun 6, 2017

Abstract

Claims (25)

1. An actuator for an exhaust gas recirculation valve, wastegate or variable turbine geometry device of a turbocharger, comprising:

a drive;

at least one rotatable threaded element;

at least one output element that can be driven in translation thereby, wherein the threaded element has at least two regions of differing pitch and a rotational axis of the threaded element is inclined relative to a translational axis of the output element;

wherein the two regions of differing pitch comprise a finer pitch region and a coarser pitch region, wherein the finer pitch region extends between a starting position at a first end of a thread of the threaded element and an ending position of between 40 degrees and 70 degrees; and

a transition region defined by a transition pitch that extends between the finer pitch region and the coarser pitch region, wherein the transition pitch increases continuously from the finer pitch region to the coarser pitch region.

2. The actuator according to claim 1 , wherein the transition region extends over a rotation of 90 to 100 degrees starting from the ending position of the finer pitch region.

3. The actuator according to claim 1 in combination with a wastegate or a variable turbine geometry device of a turbocharger.

4. An actuator for an exhaust gas recirculation valve, wastegate or variable turbine geometry device of a turbocharger, comprising:

a drive;

at least one rotatable threaded element;

at least one output element that can be driven in translation thereby, wherein the threaded element has at least two regions of differing pitch and a rotational axis of the threaded element is inclined relative to a translational axis of the output element;

wherein the two regions of differing pitch comprise a finer pitch region and a coarser pitch region, wherein the coarser pitch region is located at a rotation that begins at between 130 to 170 degrees and extends to at least 300 degrees relative to a starting position at a first end of a thread of the threaded element, wherein the finer pitch region extends between a starting position at a first end of a thread of the threaded element and an ending position of between 40 and 70 degrees; and

a transition region defined by a transition pitch that extends between the finer pitch region and the coarser pitch region, wherein the transition pitch increases continuously from the finer pitch region to the coarser pitch region.

5. The actuator according to claim 4 , wherein the thread has a finer pitch at the start than in other regions.

6. The actuator according to claim 4 , wherein the threaded element has a surface with which at least one portion of the output element is in contact and which is substantially perpendicular to the translational axis of the output element at least at the start of the thread.

7. The actuator according to claim 4 in combination with a wastegate or a variable turbine geometry device of a turbocharger.

8. The actuator according to claim 4 , wherein the transition region extends over a rotation of 90 to 100 degrees starting from the ending position of the finer pitch region.

9. The actuator according to claim 4 , further comprising an integral valve housing.

10. The actuator according to claim 9 , wherein the valve housing has at least one cooling duct.

11. The actuator according to claim 4 in combination with a valve element moved only in translation and not rotated.

12. The actuator according to claim 11 , wherein a point at which at least one portion of the output element is in contact with the threaded element is aligned at least substantially with a translational axis of the valve element moved in translation.

13. The actuator according to claim 12 , wherein the threaded element is connected to a spring element only rotated upon actuation of the valve.

14. The actuator according to claim 12 , wherein the valve element opens in a direction extending against the exhaust gas pressure.

15. The actuator according to claim 14 , wherein it has single-reduction gearing.

Assignments (8)