Variable displacement turbocharger and assembly method of variable nozzle mechanism

Patent metadata

Field	Value
Publication number	US-9790949-B2
Application number	US-201214232563-A
Country	US
Kind code	B2
Filing date	Sep 7, 2012
Priority date	Sep 28, 2011
Publication date	Oct 17, 2017
Grant date	Oct 17, 2017

Abstract

It is provided with: a variable nozzle mechanism for regulating a flow of exhaust gas to a turbine rotor; a link mechanism for converting reciprocal displacement from an actuator that operates a variable nozzle mechanism into rotational displacement and transmitting the rotational displacement to an inner section of a bearing housing; and an engaging part for engaging an output section of the link mechanism and an input section of the variable nozzle mechanism, and the engaging part is constituted by a pin and a pin insertion slot where the pin is inserted, and a smooth surface is formed around an insertion position of the pin so as to guide a tip of the pin to the insertion position.

First claim

The invention claimed is:

1. A variable displacement turbocharger comprising:
a turbine housing into which exhaust gas from an internal combustion engine is introduced;
a turbine rotor which is provided in the turbine housing and is configured to be rotated by the exhaust gas;
a turbine shaft having one end inserted in the turbine housing, and the turbine rotor being attached to the end;
a bearing which is configured to support the turbine shaft;
a bearing housing which houses the bearing and is formed with a cylindrical wall part protruding in an axial direction toward a turbine housing side from an outer peripheral part of a rear surface of the bearing housing, the rear surface extending in a radial direction;
a variable nozzle mechanism which is assembled and housed in an annular recess formed radially inside the cylindrical wall part of the bearing housing on the rear surface of the bearing housing and is configured to regulate a flow of the exhaust gas to the turbine rotor;
a link mechanism which is configured to convert reciprocal displacement from an actuator that operates the variable nozzle mechanism into rotational displacement and transmit the rotational displacement to an inner section of the annular recess of the bearing housing, the link mechanism extending through the rear surface; and
an engaging part which is configured to engage an output section of the link mechanism and art input section of the variable nozzle mechanism,
wherein the engaging part is constituted by a pin insertion part which comprises a pin and a pin insertion hole or a pin insertion slot into which the pin is inserted, and a smooth surface is formed around an insertion position of the pin so as to guide a tip of the pin to the insertion position,
wherein the pin projects from a side surface of the drive ring on an outer peripheral side of the drive ring constituting the variable nozzle mechanism, and the pin insertion part comprises a two-fork portion formed at an end of an output lever constituting the link mechanism and the insertion slot formed on an inner side of the two-fork portion, the pin insertion part having the, smooth surface on a side face of the two-fork portion,
wherein a cross-sectional shape of the two-fork portion has an L-shape and the two-fork portion is configured to engage with the pin such that a left tip and a right tip of the two-fork portion face an inner wall surface of the cylindrical wall part of the bearing housing from radially inside on the rear surface, a corner of each of the left tip and the right tip of the two-fork portion is rounded to avoid contact with the inner wall surface of the cylindrical wall part at rotation.

2. The variable displacement turbocharger, according to claim 1 , wherein a peripheral edge portion of the pin insertion hole or the pin insertion slot of the pin insertion part is rounded to facilitate insertion of the pin.

3. An assembly method for assembling a variable displacement turbocharger comprising:
preparing the variable displacement turbocharger including,
a turbine housing into which exhaust gas from an internal combustion engine is introduced;
a turbine rotor which provided in the turbine housing and is configured to be rotated by the exhaust gas;
a turbine shaft having one end inserted in the turbine housing, and the turbine rotor being attached to the end;
a bearing which is configured to support the turbine shaft;
a bearing housing which houses the bearing and is formed with a cylindrical wall part protruding in an axial direction toward a turbine housing side from an outer peripheral part of a rear surface of the bearing housing, the rear surface extending in a radial direction;
a variable nozzle mechanism which is assembled and housed in an annular recess formed radially inside the cylindrical wall part of the bearing housing on the rear surface of the bearing housing and is configured to regulate a flow of the exhaust gas to the turbine rotor;
a link mechanism which is configured to convert reciprocal displacement from an actuator that operates the variable nozzle mechanism into rotational displacement and transmit the rotational displacement to an inner section of the annular recess of the bearing housing, the link mechanism extending through the rear surface; and
an engaging part which is configured to engage an output section of the link mechanism and an input section of the variable nozzle mechanism,
wherein the engaging part is constituted by a pin insertion part which comprises a pin and a pin insertion hole or a pin insertion slot into which the pin is inserted, and a smooth surface is formed around, an insertion position of the pin so as to guide a tip of the pin to the insertion position,
wherein the pin projects from a side surface of the drive ring on an outer peripheral side of the drive ring constituting the variable nozzle mechanism, and the pin insertion part comprises a two-fork portion formed at an end of an output lever constituting the link mechanism and the insertion slot formed on an inner side of the two-fork portion, the pin insertion part having the smooth surface on a side face of the two-fork portion, and
wherein a cross-sectional shape of the two-fork portion has an L-shape and the two-fork portion is configured to engage with the pin such that a left tip and a right tip of the two-fork portion face an inner wall surface of the cylindrical wall part of the bearing housing from radially inside the rear surface, a corner of each of the left tip and the right tip of the two-fork portion is rounded to avoid contact with the inner wall surface of the cylindrical wall part at rotation;

preparing the bearing housing to which the link mechanism is assembled; and
assembling the variable nozzle mechanism to the bearing housing,
wherein the assembling step comprises the substeps of:
placing the pin of the engaging part against the smooth surface;
moving a tip portion of the pin along the smooth surface so as to position the tip portion in the insertion position; and then
pushing the variable nozzle mechanism toward the bearing housing.

4. An assembly method for assembling a variable displacement turbocharger, comprising:
preparing the variable displacement turbocharger including,
a turbine housing into which exhaust gas from an internal combustion engine is introduced;
a turbine rotor which is provided in the turbine housing and is configured to be rotated by the exhaust gas;
a turbine shaft having one end inserted in the turbine housing, and the turbine rotor being attached to the end;
a bearing which is configured to support the turbine shaft;
a bearing housing which houses the bearing and is formed with a cylindrical wall part protruding in an axial direction toward a turbine housing side from an outer peripheral part of a rear surface of the bearing housing, the rear surface extending in a radial direction;
a variable nozzle mechanism which is assembled and housed in an annular recess formed radially inside the cylindrical wall part of the bearing housing on the rear surface of the bearing housing and is configured to regulate a flow of the exhaust gas to the turbine rotor;
a link mechanism which is configured to convert reciprocal displacement from an actuator that operates the variable nozzle mechanism into rotational displacement and transmit the rotational displacement to an inner section of the annular recess of the bearing housing, the link mechanism extending through the rear surface; and
an engaging part which is configured to engage an output section of the link mechanism and an input section of the variable nozzle mechanism,
wherein the engaging part is constituted by a pin insertion part which comprises a pin and a pin insertion hole or a pin insertion slot into which the pin is inserted, and a smooth surfac

Assignees

• Tashiro Naoto
• Jinnai Yasuaki
• ARIMIZU Hiroyuki
• Mitsubishi Heavy Ind Ltd

Inventors

• Tashiro Naoto
• Jinnai Yasuaki
• ARIMIZU Hiroyuki

Classifications

• F05D2250/27

  hyperboloid · CPC title

• F02B37/24 Primary

  by using pumps or turbines with adjustable guide vanes · CPC title

• F05D2250/711

  convex · CPC title

• F05D2250/293

  lathed, e.g. rotation symmetrical · CPC title

• F05D2220/40

  in turbochargers · CPC title