Waste gate valve for turbocharger

Patent metadata

Field	Value
Publication number	US-10975760-B2
Application number	US-201815953625-A
Country	US
Kind code	B2
Filing date	Apr 16, 2018
Priority date	Dec 1, 2017
Publication date	Apr 13, 2021
Grant date	Apr 13, 2021

Abstract

A waste gate valve for a turbocharger is provided that improves control responsivity, wear resistance and the flow uniformity of diverted exhaust gas by improving the operational structure thereof. The waste gate valve includes a turbine housing in which a portion of a bypass passage is formed along the inner circumferential surface of a discharge passage. A mixer ring includes bypass apertures therein that are arranged along the bypass passage formed in the inner circumferential surface of the discharge passage. Additionally, a control valve is configured to open or close the bypass apertures based on movement thereof.

First claim

What is claimed is:

1. A waste gate valve for a turbocharger, comprising:
a turbine housing that accommodates a turbine wheel therein and includes a bypass passage formed therein to divert exhaust gas introduced into the turbine wheel to a discharge passage, a portion of the bypass passage being formed along an inner circumferential surface of the discharge passage;
a mixer ring formed to block a region between the bypass passage and the discharge passage and including therein bypass apertures arranged along the bypass passage formed in an inner circumferential surface of the discharge passage;
a control valve configured to switch a state of the bypass apertures to an open state or a closed state via movement thereof to regulate an opening degree of the bypass apertures;
an actuator configured to supply rotational force to the control valve in a circumferential direction,
wherein the control valve includes overlap apertures therein formed in the circumferential direction thereof to be disposed at positions that are same as positions of the bypass apertures and to have a shape that corresponds is equal to a shape of the bypass apertures,

wherein, when the control valve rotates in the circumferential direction, the overlap apertures overlap the bypass apertures or move away from the bypass apertures to regulate an opening degree of the bypass apertures, and
wherein the bypass passage includes:
a first passage formed between an introduction pipe through which exhaust gas is introduced into the turbine housing and a discharge pipe through which exhaust as is discharged; and
a second passage that communicates with the first passage and is formed in a shape of a recess that extends along an inner circumferential surface of the discharge pipe,

wherein the bypass apertures formed in the mixer ring are disposed between the second passage and the discharge passage.

2. The waste gate valve according to claim 1 , wherein the mixer ring is fixedly inserted into the discharge pipe, and the control valve is movably inserted between an outer circumferential surface of the mixer ring and the inner circumferential surface of the discharge pipe.

3. The waste gate valve according to claim 1 , wherein the bypass apertures are arranged at equidistant intervals from each other in a circumferential direction of the mixer ring.

4. The waste gate valve according to claim 3 , wherein the opening degree of each of the bypass apertures is identical to the opening degree of all other bypass apertures when the control valve moves.

5. The waste gate valve according to claim 1 , wherein the turbine housing includes a knob aperture therein, and wherein the control valve includes a knob that penetrates the knob aperture, the knob having a first end fixed to the control valve and a second end connected to the actuator.

6. The waste gate valve according to claim 1 , wherein the recess that defines the second passage is formed with a circumference of a first side thereof, disposed adjacent to the turbine wheel, having a smaller inner diameter than a circumference of a second side thereof, disposed distant from the turbine wheel,
wherein a support flange is formed along the circumference of the first side of the recess disposed adjacent to the turbine wheel, and wherein an end of the mixer ring is supported by the support flange.

Assignees

• Hyundai Motor Co Ltd
• Kia Motors Corp

Inventors

• Jin Seok Beom

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F16K3/262

  with a transverse bore in the valve member · CPC title

• F16K3/24

  with cylindrical valve members · CPC title

• F02B37/183 Primary

  Arrangements of bypass valves or actuators therefor · CPC title

• F01D17/105

  by passing part of the fluid · CPC title