Turbocharger for an internal combustion engine

Patent metadata

Field	Value
Publication number	US-10883418-B2
Application number	US-201716332189-A
Country	US
Kind code	B2
Filing date	Aug 1, 2017
Priority date	Sep 14, 2016
Publication date	Jan 5, 2021
Grant date	Jan 5, 2021

Abstract

A turbocharger for an internal combustion engine has a bearing housing, in which a rotor shaft is mounted in a rotatable manner. A compressor having a compressor wheel is arranged for conjoint rotation on the rotor shaft. A fresh air supply channel conducts a fresh air mass flow to the compressor wheel. The fresh air supply channel has a first flow cross section upstream of the compressor wheel. A flow control device is provided and is adjustable between an open position, in which the first flow cross section is opened up, and a closed position, in which the first flow cross section is reduced to a second flow cross section. The flow control device is fluidically coupled to a compressor channel of the compressor downstream of the compressor wheel, such that the flow control device is adjusted in a manner dependent on a pressure prevailing in the compressor channel.

First claim

The invention claimed is:

1. A turbocharger for a combustion machine, the turbocharger comprising:
a rotor shaft;
a bearing housing mounting said rotor shaft in a rotatable manner;
a compressor having a compressor wheel disposed for conjoint rotation on said rotor shaft, said compressor further having a compressor channel being a fresh-air volute;
a fresh air supply channel for conducting a fresh air mass flow to said compressor wheel, said fresh air supply channel having a first flow cross section upstream of said compressor wheel; and
a flow control device being adjustable between an open position, in which said first flow cross section is opened up, and a closed position, in which said first flow cross section is reduced to a second flow cross section, said flow control device is fluidically coupled to said compressor channel of said compressor downstream of said compressor wheel, such that said flow control device is adjusted in a manner dependent on a pressure prevailing in said fresh-air volute;
wherein said flow control device has a control cylinder which, for purposes of adjusting said flow control device, is mounted so as to be displaceable axially with respect to a rotor axis of rotation of said rotor shaft, and which is fluidically coupled to said compressor channel of said compressor downstream of said compressor wheel; and
wherein said flow control device has multiple guide vanes which are mounted rotatably on said control cylinder, wherein said guide vanes are adjustable between an open position and a closed position by displacement of said control cylinder.

2. The turbocharger according to claim 1 , wherein said control cylinder is displaceable between two axial end positions including a first axial end position which corresponds to the open position of said flow control device and a second axial end position which corresponds to the closed position of said flow control device.

3. The turbocharger according to claim 1 , wherein:
a compressor housing has a piston cavity formed therein; and
said control cylinder has an encircling piston ring that is guided in an axially displaceable fashion in said piston cavity.

4. The turbocharger according to claim 3 , further comprising at least one seal element configured for sealing off said piston ring with respect to said piston cavity.

5. The turbocharger according to claim 3 , further comprising at least one channel, said piston cavity is connected by means of said at least one channel to said compressor channel of said compressor.

6. The turbocharger according to claim 3 , wherein said flow control device has an axial spring element which is disposed so as to exert a spring force on said control cylinder in an axial direction with respect to the rotor axis of rotation counter to a pressure force exerted on said control cylinder by pressure prevailing in said compressor channel, such that said control cylinder is axially displaceable in a manner dependent on the spring force and the pressure force.

7. The turbocharger according to claim 1 , wherein said guide vanes, in the open position, are disposed such that said guide vanes open up the first flow cross section, and wherein, with axial displacement of said control cylinder, said guide vanes are displaced toward said compressor wheel and interact with said compressor housing such that said guide vanes are rotated in order to reduce the first flow cross section.

8. The turbocharger according to claim 7 , wherein said flow control device has a radial spring element which is disposed so as to impart a spring force to in each case a rear end of said guide vanes in a direction of the rotor axis of rotation, such that a front end of said guide vanes is pressed against said compressor housing.

9. The turbocharger according to claim 1 , wherein, in the closed position, said guide vanes are displaced axially in a direction of said compressor wheel and are rotated such that said guide vanes form a substantially closed conical ring with the second flow cross section.

10. The turbocharger according to claim 1 , wherein said guide vanes are shaped so as to have a tapering front end, which faces toward said compressor wheel.

11. The turbocharger according to claim 1 , wherein:
said compressor housing has two parts including a first part fastened to said bearing housing and surrounds said compressor wheel, and a second part fastened to said first part; and
said flow control device is disposed between said first and second parts.

Assignees

• Cpt Group Gmbh

Inventors

• Hiller Marc

Classifications

• F04D29/685

  Inducing localised fluid recirculation in the stator-rotor interface · CPC title

• F04D27/0215

  Arrangements therefor, e.g. bleed or by-pass valves · CPC title

• F05D2250/51

  Inlet · CPC title

• F05D2270/101

  Compressor surge or stall · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title