Actuator and exhaust gas recirculation valve, wastegate or variable turbine geometry device of a turbocharger comprising an actuator
AssigneeCooper-Standard Automotive (Deutschland) GmbH
InventorsBernhard Klipfel, Christoph Thiery
Life of this patent
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Abstract
An actuator comprising a drive, at least one rotatable threaded element and at least one output element driven in translation thereby is described, characterized in that 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.
Claims15
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.
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.
Dependencies are inferred from the claim text.