Valve device for a turbocharger

US11047296B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11047296-B2
Application numberUS-201816129304-A
CountryUS
Kind codeB2
Filing dateSep 12, 2018
Priority dateMar 16, 2016
Publication dateJun 29, 2021
Grant dateJun 29, 2021

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A valve device for an exhaust-gas bypass path of a turbocharger, including: a plate-like valve element, movable between a closed position and an open position and which has a shaft, which is connected to a valve element carrier for limited movement in the shaft direction; a rotatably held spindle, to which the valve element carrier is fixedly connected; a valve seat for the valve element, which valve seat surrounds an exhaust-gas through-opening; and an annular sheet-metal spring element, which has an opening through which the valve element shaft extends, an outer ring region, an inner ring region, which is axially offset relative to the outer ring region and adjoins the spring element opening, and an annular transition region therebetween; the width of the spring element transition region being variable around the spring element opening such that the valve element can be adapted to the valve seat as easily as possible.

First claim

Opening claim text (preview).

The invention claimed is: 1. A valve device for an exhaust-gas bypass path of a turbocharger, said valve device having: a plate-like valve element, which has a sealing surface lying in a plane and a shaft extending away from the sealing surface and is movable between a closed position and an open position; a valve element carrier, to which the valve element is connected by means of its shaft so that the valve element is movable to a limited extent relative to the valve element carrier in a direction perpendicular to the valve element sealing surface; a spindle, which is held so as to be rotatable about a spindle longitudinal axis and is fixedly connected to the valve element carrier, such that the valve element is movable between its closed position and its open position by rotation of the spindle; a valve seat surrounding an exhaust-gas through-opening, against which valve seat the valve element sealing surface bears with a sealing pressure in an at least substantially gastight manner in the closed position of the valve element; and a substantially annular spring element produced from a sheet metal and having an opening through which the valve element shaft extends, wherein by means of the valve element carrier, the valve element is held in such a way that, as considered in the direction of the spindle longitudinal axis, by rotating the spindle the plane defined by the valve element sealing surface is pivotable about the spindle longitudinal axis through a pivot angle range, the range limits of which are defined by the closed position and the open position of the valve element and which defines a pivot angle plane extending perpendicularly to the spindle longitudinal axis and to the plane of the valve element sealing surface, in which pivot angle plane the longitudinal axis of the valve element shaft lies; wherein with respect to the axis of its opening and as considered in the direction of this axis, the spring element has a radially outer ring region, a radially inner ring region adjoining the spring element opening, and therebetween an annular transition region, such that the radially outer ring region is offset relative to the radially inner ring region in the direction of the axis of the spring element opening such that play in the direction of the longitudinal axis of the valve element shaft between the valve element and the valve element carrier is at least mostly eliminated by the spring element, wherein the radially inner and the radially outer ring region are at least substantially flat and lie in planes perpendicular to the axis of the spring element opening, wherein, as considered in the direction of the axis of the spring element opening, the radially inner ring region has an elongate non-elliptical shape defined by two curved convex ends connected by two substantially straight and parallel sides, and wherein the spring element is held on the valve element shaft substantially non-rotatably relative to the valve element carrier, and, with respect to the axis of the spring element opening and as considered in the axial direction, the radial width of the spring element transition region and thus the rigidity of the transition region with respect to pressing forces oriented in the direction of the axis of the spring element opening varies around the spring element opening, and wherein the transition region has two first longitudinal portions, in which the transition region has its greatest width and which are traversed by the pivot angle plane and are arranged opposite one another with respect to the spring element opening. 2. The valve device according to claim 1 , wherein each first longitudinal portion is arranged at least substantially symmetrically with respect to the pivot angle plane. 3. The valve device according to claim 2 , wherein said substantially straight and parallel sides are arranged opposite one another with respect to the opening axis, and in a circumferential direction of the spring element opening between said substantially straight and parallel sides, the two first longitudinal portions of the spring element transition region are arranged. 4. The valve device according to claim 1 , wherein the spring element has a half bead, the flank of which is formed by the spring element transition region. 5. The valve device according to claim 4 , wherein the flank of the half bead in the at least one first longitudinal portion of the spring element transition region is more heavily inclined relative to the axis of the spring element opening than in the other longitudinal portions of the spring element transition region. 6. The valve device according to claim 1 , wherein, as considered in a direction perpendicular to the valve element sealing surface, the valve element and the spring element have a circular outer edge, the radially outer spring element ring region has the form of a circular ring, the spring element opening has an oval form and the radially inner spring element ring region adjoining the spring element opening has the same width everywhere. 7. A spring element for a wastegate valve of a turbocharger, which is substantially plate-like and is produced from a sheet metal and is provided with a central opening, wherein, with respect to the axis of its opening and as considered in the direction of this axis, the spring element has a radially outer ring region with a circular outer edge, a radially inner ring region adjoining the spring element opening, and therebetween an annular transition region, such that the radially outer ring region is offset relative to the radially inner ring region in the direction of the axis of the spring element opening, wherein the radially inner and the radially outer ring region are at least substantially flat and lie in planes perpendicular to the axis of the spring element opening, wherein, as considered in the direction of the axis of the spring element opening, the radially inner ring region has an elongate non-elliptical shape defined by two curved convex ends connected by two substantially straight and parallel sides, wherein the transition region is formed by a half bead surrounding the spring element opening and having a radially outer bead foot transitioning into the radially outer ring region, a radially inner bead foot transitioning into the radially inner ring region, and a bead flank connecting the two bead feet to one another, wherein, as considered in the direction of the axis of the spring element opening, the width of the spring element transition region varies around the spring element opening such that the transition region has two first longitudinal portions of greatest average width arranged opposite one another with respect to the spring element opening, and between these two first longitudinal portions has two second longitudinal portions of smallest average width likewise arranged opposite one another with respect to the spring element opening, and wherein the bead flank in the first longitudinal portions of the transition region is more heavily inclined relative to the axis of the spring element opening than in the second longitudinal portions. 8. The spring element according to claim 7 , wherein, in each cross-section through the spring element containing the axis of the spring element opening, the bead flank is inclined relative to the axis of the spring element opening in such a way that the radially outer bead foot has a greater spacing from the opening axis than the radially inner bead foot. 9. The spring element according to claim 7 , wherein, said substantially straight and parallel sides are arranged opposite one another with respect to the opening axis, and in a circumferential direction of the spring element opening between said substantially

Assignees

Inventors

Classifications

  • F02B37/186Primary

    Arrangements of actuators or linkage for bypass valves · CPC title

  • Improving ICE efficiencies · CPC title

  • Arrangements of bypass valves or actuators therefor · CPC title

  • Belleville-type springs (friction-clutch diaphragm springs F16D13/583) · CPC title

  • by bypassing exhaust {from the inlet to the outlet of turbine or to the atmosphere} · CPC title

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What does patent US11047296B2 cover?
A valve device for an exhaust-gas bypass path of a turbocharger, including: a plate-like valve element, movable between a closed position and an open position and which has a shaft, which is connected to a valve element carrier for limited movement in the shaft direction; a rotatably held spindle, to which the valve element carrier is fixedly connected; a valve seat for the valve element, which…
Who is the assignee on this patent?
Elringklinger Ag
What technology area does this patent fall under?
Primary CPC classification F02B37/186. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jun 29 2021 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).