Control device of an exhaust gas-conducting section of an exhaust gas turbocharger

Patent metadata

Field	Value
Publication number	US-12180883-B2
Application number	US-202218287480-A
Country	US
Kind code	B2
Filing date	Jun 8, 2022
Priority date	Jul 1, 2021
Publication date	Dec 31, 2024
Grant date	Dec 31, 2024

Abstract

A control device of an exhaust gas-conducting section of a turbocharger includes a pivotable closing device with a closing element and an element lever. A first element portion thereof opens and closes a first flow cross-section of a flow connection and a second element portion opens and closes a second flow cross-section of a bypass duct of the exhaust gas-conducting section. The element lever includes a lever end portion engaging into a cavity of the closing element. A holding element is fixedly connected to the closing element. The lever end portion includes a first contact surface and, axially spaced apart, a second contact surface. The first contact surface includes an axially-extending first partial surface and a radially-extending second partial surface connected to one another by a third partial surface. The partial surfaces are designed to be able to effect contact with the closing element.

First claim

The invention claimed is:

1. A control device of an exhaust gas-conducting section of an exhaust gas turbocharger, comprising:
a closing device ( 9 ) comprising
a closing element ( 10 ) and
an element lever ( 11 ),
wherein the closing device ( 9 ) is configured to pivot about an axis of rotation ( 19 ), and
wherein the closing element ( 10 ) is configured to open and close a first flow cross-section ( 13 ) of the exhaust gas-conducting section ( 1 ),
wherein the first flow cross-section ( 13 ) is formed in a partition wall lying between a first spiral channel ( 4 ) of the exhaust gas-conducting section ( 1 ) and a second spiral channel ( 5 ) of the exhaust gas-conducting section ( 1 ), and
wherein the exhaust gas-conducting section ( 1 ) comprises a second flow cross-section ( 17 ) of a bypass duct ( 18 ) formed in the exhaust gas-conducting section ( 1 ), the bypass duct is configured to bypass a flow against a turbine wheel formed in the exhaust gas-conducting section ( 1 ), and
wherein the closing element ( 10 ) comprises
a first element portion ( 15 ) configured to close the first flow cross-section ( 13 ) and
a second element portion ( 16 ) configured to close the second flow cross-section ( 17 ), and

wherein the element lever ( 11 ) comprises a lever end portion ( 23 ) engaging into a cavity ( 20 ) of the closing element ( 10 ), and
wherein the closing element ( 10 ) comprises a holding element ( 21 ) fixedly connected thereto and encompassed by the lever end portion ( 23 ), and
wherein the lever end portion ( 23 ) comprises
a first contact surface ( 26 ) and
a second contact surface ( 27 ) axially spaced apart from the first contact surface ( 26 ) with respect to a longitudinal axis ( 22 ) of the closing element ( 10 ),
wherein the first contact surface ( 26 ) comprises an axially-extending first partial surface ( 30 ) and a radially-extending second partial surface ( 31 ),
wherein the axially-extending first partial surface ( 30 ) and the radially-extending second partial surface ( 31 ) are connected to one another by a third partial surface ( 32 ) formed between the axially-extending first partial surface ( 30 ) and the radially-extending second partial surface ( 31 ),
wherein each of the partial surfaces ( 30 , 31 , 32 ) is configured to contact the closing element ( 10 ), and
wherein each of the partial surfaces ( 30 , 31 , 32 ) and a base ( 29 ) of the closing element ( 10 ) are planar, and
wherein the three partial surfaces ( 30 , 31 , 32 ) are formed contiguously and opposite an inner wall ( 28 ) and the base ( 29 ), and

wherein the lever end portion ( 23 ) further comprises
a first partial portion ( 33 ), comprising the first partial surface ( 30 ), and
a second partial portion ( 34 ) comprising the second partial surface ( 31 ) and the third partial surface ( 32 ),
wherein the second partial portion ( 34 ) is frustoconical.

2. The control device as claimed in claim 1 , wherein the first partial surface ( 30 ) and the third partial surface ( 32 ) are annular.

3. The control device as claimed in claim 1 , wherein the third partial surface ( 32 ) is inclined with respect to the longitudinal axis ( 22 ).

4. The control device as claimed in claim 3 , wherein a first distance (A 1 ) of the third partial surface ( 32 ) from the longitudinal axis ( 22 ), is smaller than a second distance (A 2 ) of the third partial surface ( 32 ) from the longitudinal axis ( 22 ).

5. The control device as claimed in claim 1 , wherein the second contact surface ( 27 ) is spaced apart from the longitudinal axis ( 22 ) unequally to the first contact surface ( 26 ).

6. The control device as claimed in claim 1 , wherein the inner wall ( 28 ) defines the cavity ( 20 ) and comprises at least one step ( 37 ).

7. The control device as claimed in claim 1 , wherein between the closing element ( 10 ) and the lever end portion ( 23 ) during maximum tilting of the closing element ( 10 ) relative to the lever end portion ( 23 ), the first contact surface ( 26 ) comprises at least one first contact point ( 38 ) and one second contact point ( 39 ), and
wherein the at least one first contact point ( 38 ) and the at least one second contact point ( 39 ) are spaced apart from each other axially and radially with respect to the longitudinal axis ( 22 ).

8. The control device as claimed in claim 1 , wherein, between the closing element ( 10 ) and the lever end portion ( 23 ) during maximum tilting of the closing element ( 10 ) relative to the lever end portion ( 23 ), the second contact surface ( 27 ) comprises at least one third contact point ( 40 ).

9. The control device as claimed in claim 1 , wherein an element ring ( 35 ) of the lever end portion ( 23 ) is formed on an annular surface ( 41 ), and
wherein the annular surface is transverse to the second contact surface ( 27 ), so as to provide a fourth contact point ( 42 ).

10. The control device as claimed in claim 1 , wherein the holding element ( 21 ) comprises a securing element ( 43 ) disposed on an element end ( 46 ) remote from the base ( 29 ) of the closing element ( 10 ).

11. The control device as claimed in claim 1 , wherein a lever arm ( 44 ) of the element lever ( 11 ), receiving the lever end portion ( 23 ), is curved at an end ( 45 ) facing the lever end portion ( 23 ).

Assignees

• Ihi Charging Systems Int Gmbh
• Mercedes Benz Group Ag

Inventors

• Guthörle Manfred
• Dick Viktor
• Weniger Stephan
• Reif Zdenek
• Brinkert Nils
• Weeber Jürgen
• Knieps Thomas

Classifications

• F02B37/025

  Multiple scrolls or multiple gas passages guiding the gas to the pump drive · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F16K1/2014

  Shaping of the valve member · CPC title

• F02B37/18 Primary

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

• F02B37/183 Primary

  Arrangements of bypass valves or actuators therefor · CPC title