Variable geometry turbocharger

Patent metadata

Field	Value
Publication number	US-11092068-B2
Application number	US-201616088539-A
Country	US
Kind code	B2
Filing date	Mar 30, 2016
Priority date	Mar 30, 2016
Publication date	Aug 17, 2021
Grant date	Aug 17, 2021

Abstract

A variable geometry turbocharger includes: a turbine rotor; and a variable nozzle mechanism for adjusting a flow of exhaust gas to the turbine rotor from a scroll flow passage formed on a radially outer side of the turbine rotor. The variable nozzle mechanism includes: a nozzle vane disposed in an exhaust gas flow passage for guiding the exhaust gas to the turbine rotor from the scroll flow passage; a support wall forming a flow passage wall on a first side of the exhaust gas flow passage with respect to an axial direction of the turbine rotor and supporting the nozzle vane rotatably in a cantilever fashion; and a non-support wall forming a flow passage wall on a second side of the exhaust gas flow passage with respect to the axial direction. Of an end surface of the nozzle vane on a side of the non-support wall, an edge portion on a side of a pressure surface includes a non-support-wall side linear portion formed to have a linear shape.

First claim

The invention claimed is:

1. A variable geometry turbocharger, comprising:
a turbine rotor; and
a variable nozzle mechanism for adjusting a flow of exhaust gas to the turbine rotor from a scroll flow passage formed on a radially outer side of the turbine rotor,
wherein the variable nozzle mechanism includes:
a nozzle vane disposed in an exhaust gas flow passage for guiding the exhaust gas to the turbine rotor from the scroll flow passage;
a support wall forming a flow passage wall on a first side of the exhaust gas flow passage with respect to an axial direction of the turbine rotor and supporting the nozzle vane rotatably in a cantilever fashion; and
a non-support wall forming a flow passage wall on a second side of the exhaust gas flow passage with respect to the axial direction, and

wherein, of an end surface of the nozzle vane on a side of the non-support wall, an edge portion on a side of a pressure surface includes a non-support-wall side linear portion formed to have a linear shape, and
wherein the non-support-wall side linear portion, extending in a longitudinal direction of the vane, that is parallel to a chord length of the nozzle vane, has a length which is not smaller than a half of the chord length of the nozzle vane.

2. The variable geometry turbocharger according to claim 1 , wherein, of the edge portion on the side of the pressure surface, the non-support-wall side linear portion is formed in a range including a position where a chord directional distance from a trailing edge of the nozzle vane is ¼ of the chord length of the nozzle vane.

3. The variable geometry turbocharger according to claim 1 ,
wherein an end portion of the nozzle vane on a side of the non-support wall includes a non-support-wall side rib shaped portion protruding toward a pressure surface of the nozzle vane, and
wherein the non-support-wall side linear portion is formed on a tip portion of the non-support-wall side rib shaped portion.

4. The variable geometry turbocharger according to claim 3 ,
wherein, in a view taken in a direction of a rotational axis of the nozzle vane, the non-support-wall side rib shaped portion is disposed so as to protrude from the pressure surface, and wherein the non-support-wall side linear portion extends on the tip portion of non-support-wall side rib shaped portion.

5. The variable geometry turbocharger according to claim 1 ,
wherein an end portion of the nozzle vane on a side of the non-support wall includes a non-support-wall side inclined surface connecting the end surface of the nozzle vane on the side of the non-support wall and the pressure surface,
wherein the non-support-wall side inclined surface includes an inclined surface from the pressure surface to the end surface of the nozzle vane on the side of the non-support wall, and
wherein the non-support-wall side linear portion is formed on a boundary position between the non-support-wall side inclined surface and the end surface on the side of the non-support wall.

6. The variable geometry turbocharger according to claim 1 ,
wherein, of an end surface of the nozzle vane on a side of the support wall, an edge portion on a side of a suction surface has a support-wall side linear portion formed to have a linear shape.

7. The variable geometry turbocharger according to claim 6 ,
wherein the support-wall side linear portion and the non-support-wall side linear portion are formed to be parallel to each other.

8. The variable geometry turbocharger according to claim 6 , wherein the support-wall side linear portion is formed in a range including a position where a chord directional distance from a trailing edge of the nozzle vane is ¼ of the chord length of the nozzle vane.

9. The variable geometry turbocharger according to claim 6 , wherein the support-wall side linear portion has a length which is not smaller than a half of the chord length of the nozzle vane.

10. The variable geometry turbocharger according to claim 6 ,
wherein the non-support-wall side linear portion is longer than the support-wall side linear portion.

11. The variable geometry turbocharger according to claim 6 ,
wherein the end portion of the nozzle vane on the side of the support wall includes a support-wall side rib shaped portion protruding toward a suction surface of the nozzle vane, and
wherein the support-wall side linear portion is formed on the support-wall side rib shaped portion.

12. The variable geometry turbocharger according to claim 6 ,
wherein the end portion of the nozzle vane on the side of the support wall includes a support-wall side inclined surface connecting the end surface of the nozzle vane on the side of the support wall and the pressure surface,
wherein the support-wall side inclined surface includes an inclined surface from the suction surface to the end surface of the nozzle vane on the side of the support wall, and
wherein the support-wall side linear portion is formed on a boundary position between the support-wall side inclined surface and the end surface on the side of the support wall.

13. The variable geometry turbocharger according to claim 6 ,
wherein the nozzle vane is configured such that, when the nozzle vane is inclined due to a hydrodynamic force, the support-wall-side linear portion makes contact with the support wall before the non-support-wall side linear portion makes contact with the non-support wall.

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Yokoyama Takao
• Hoshi Toru
• Tojo Masaki

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F02C6/12

  Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F02C9/16

  Control of working fluid flow (F02C9/48 takes precedence; control of air-intake flow F02C7/057) · CPC title

• F05D2240/128

  Nozzles · CPC title