Radial compressor for a charging device of an internal combustion engine, charging device and lamellas for an iris diaphragm mechanism, and method for producing such lamella

Patent metadata

Field	Value
Publication number	US-11255252-B2
Application number	US-202016818194-A
Country	US
Kind code	B2
Filing date	Mar 13, 2020
Priority date	Sep 14, 2017
Publication date	Feb 22, 2022
Grant date	Feb 22, 2022

Abstract

A radial compressor has an iris diaphragm mechanism for a pressure-charging device of an internal combustion engine. The radial compressor has a bearing assembly, in which a rotor shaft is rotatably mounted, having a compressor impeller arranged in a compressor housing for conjoint rotation on the rotor shaft and having a fresh air supply channel for carrying a fresh air mass flow to the compressor impeller. The iris diaphragm mechanism is upstream of the compressor impeller, allowing variable adjustment of a flow cross section for the fresh air mass flow for admission to the compressor impeller, at least over a partial region. For this purpose, the iris diaphragm mechanism has multiple lamellae which each have a plate style lamella main body and a pin style actuating element as integral constituent parts of the respective lamella.

First claim

The invention claimed is:

1. A method for producing a lamella comprising:
providing a plate style lamella semi-finished part composed of sheet metal, which has a lamella main body with an outer edge and a bearing element for the rotatable mounting of the lamella, wherein a protuberance is formed which projects beyond the edge; and
bending the projecting protuberance relative to the lamella main body such that the protuberance extends perpendicular to a main extent plane defined by the lamella main body, and thus an actuating element is formed as an integral constituent part of the lamella.

2. The method for producing a lamella as claimed in claim 1 , wherein the protuberance projecting beyond the edge has a central piece with two oppositely situated limbs projecting from the central piece, and
wherein the bending of the projecting protuberance relative to the lamella main body such that the protuberance extends perpendicular to a main extent plane defined by the lamella main body is followed by the bending of the projecting limb such that an actuating element in the form of a slotted cylinder is formed as an integral constituent part of the lamella.

3. A lamella for an iris diaphragm mechanism of a radial compressor, wherein the lamella has a plate style lamella main body, a bearing element for the rotatable mounting of the lamella, and a pin style actuating element for actuating the respective lamella, the main body and the actuating element are integral parts of the lamella,
wherein the actuating element of the lamella is formed from a protuberance on the lamella main body to extend perpendicularly with respect to a main extent plane defined by the lamella main body, and
wherein the lamella main body is formed from sheet metal, and the actuating element is manufactured by bending of the protuberance.

4. A radial compressor for a supercharging device of an internal combustion engine comprising:
a rotor shaft rotatably mounted in a bearing assembly;
a compressor impeller arranged in a compressor housing for conjoint rotation on the rotor shaft;
an air supply channel for carrying an air mass flow to the compressor impeller;
an iris diaphragm mechanism to at least partially close and open a diaphragm aperture allowing variable adjustment of a flow cross section for the air mass flow for admission to the compressor impeller, at least over a partial region of the cross section; and
a plurality of lamellae respectively rotatable about a center of rotation and each having a lamella main body and an actuating element for actuating the respective lamella, wherein the main body and the actuating element are integral to the respective lamella,
wherein the actuating element of at least one lamella is formed from a protuberance on the lamella main body to extend perpendicularly with respect to a main extent plane defined by the lamella main body, and
wherein the lamella main body is formed from sheet metal, and the actuating element is manufactured by bending of the protuberance.

5. The radial compressor as claimed in claim 4 , wherein the protuberance is formed to project beyond an outer edge of the lamella main body such that the actuating element is arranged at the outer edge of the lamella main body.

6. The radial compressor as claimed in claim 4 , wherein the protuberance is formed to project beyond an outer edge of the lamella main body such that the actuating element is arranged outside the lamella main body and spaced apart from the outer edge of the lamella main body.

7. The radial compressor as claimed in claim 4 , wherein the projecting protuberance body is formed such that the actuating element has a shape of a slotted cylinder which extends perpendicular to the main extent plane.

8. The radial compressor as claimed in claim 4 , wherein the actuating element is formed from the lamella main body by deep drawing sheet metal.

9. The radial compressor as claimed in claim 4 , further comprising a bearing element in an end region of the lamella situated opposite the actuating element, wherein the lamella is rotatably mounted to a bearing ring of the iris diaphragm mechanism with the bearing element.

10. The radial compressor as claimed in claim 9 , wherein the bearing element is a bore mountable on a bearing pin fixed in the bearing ring.

11. The radial compressor as claimed in claim 9 , wherein the bearing element is a pin element that extends perpendicular to a main extent plane defined by the lamella main body in an opposite direction in relation to the actuating element and mountable on a bore defined by the bearing ring.

12. The radial compressor as claimed in claim 4 , wherein the iris diaphragm mechanism has a fixed bearing ring and an adjusting ring arranged concentrically thereto and rotatable about a common axis, wherein each lamella is mounted rotatably about its center on the bearing ring.

13. The radial compressor as claimed in claim 12 , further comprising a groove defined by the adjusting ring and corresponding to each lamella, wherein the groove runs obliquely in relation to the radial direction of the adjusting ring such that the actuating element of the respective lamella is guided for actuation.

14. The radial compressor as claimed in claim 4 , wherein the actuating element is a pin style actuating element.

15. The radial compressor as claimed in claim 4 , wherein the radial compressor is located in a supercharging device which is one of: an exhaust-gas turbocharger, a supercharger operated by electric motor, and as a supercharger operated via a mechanical coupling to the internal combustion engine.

Assignees

• Vitesco Tech Gmbh

Inventors

• Bogner Mathias
• Schäfer Christoph
• Slavic Sasa

Classifications

• F04D29/4213

  suction ports · CPC title

• F05D2250/51

  Inlet · CPC title

• F04D17/10

  for compressing or evacuating · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F02B33/40 Primary

  of non-positive-displacement type · CPC title