Variable-geometry exhaust turbine

Patent metadata

Field	Value
Publication number	US-10006355-B2
Application number	US-201314759365-A
Country	US
Kind code	B2
Filing date	Feb 21, 2013
Priority date	Feb 21, 2013
Publication date	Jun 26, 2018
Grant date	Jun 26, 2018

Abstract

An object is to provide a variable-geometry exhaust turbine whereby it is possible to prevent deformation and damage to a nozzle support under a high temperature. A variable-geometry exhaust turbine includes: a nozzle mount, a nozzle support including a first end portion joined to the first surface of the nozzle mount, a nozzle plate including the first surface joined to the second end portion of the nozzle support 6 and supported so as to face the nozzle mount at a distance, and the opposite second surface facing an exhaust—as channel through which exhaust gas flows, and a plurality of nozzle vanes supported rotatably between the nozzle mount and the nozzle plate. The nozzle support is capable of tilting along a radial direction so as to absorb a relative displacement in the radial direction between the nozzle mount and the nozzle plate due to thermal expansion.

First claim

The invention claimed is:

1. A variable-geometry exhaust turbine, comprising:
a nozzle mount including a first surface and a second surface;
a nozzle support including a first end portion and a second end portion, the first end portion being joined to the first surface of the nozzle mount;
a nozzle plate including a first surface and a second surface, the first surface of the nozzle plate being joined to the second end portion of the nozzle support and supported so as to face the nozzle mount and to be spaced from the nozzle mount, and the second surface of the nozzle plate facing an exhaust gas channel through which exhaust gas flows; and
at least one nozzle vane supported rotatably between the nozzle mount and the nozzle plate,
wherein the nozzle support includes a mechanism for tilting along a radial direction so as to absorb a relative displacement in the radial direction between the nozzle mount and the nozzle plate due to thermal expansion.

2. The variable-geometry exhaust turbine according to claim 1 ,
wherein at least one of the first end portion or the second end portion of the nozzle support comprises an end portion formed in a spherical shape, and
wherein a housing-and-retaining part is formed on at least one of the nozzle mount or the nozzle plate, the housing-and-retaining part slidably housing the end portion formed in the spherical shape.

3. The variable-geometry exhaust turbine according to claim 2 ,
wherein the end portion formed in the spherical shape of the nozzle support is housed in the housing-and-retaining part, by swaging an insertion inlet of the housing-and-retaining part while the end portion formed in the spherical shape is inserted from the insertion inlet to be disposed in the housing-and-retaining part, the insertion inlet being an opening into which the end portion formed in the spherical shape is loosely insertable.

4. The variable-geometry exhaust turbine according to claim 3 ,
wherein the housing-and-retaining part includes a mount-side housing-and-retaining part formed on the nozzle mount and a plate-side housing-and-retaining part formed on the nozzle plate, and the nozzle support is formed in a spherical shape at both of the first end portion and the second end portion, and
wherein the insertion inlet of the mount-side housing-and-retaining part is formed on the first surface of the nozzle mount facing the nozzle plate, and the insertion inlet of the plate-side housing-and-retaining part is formed on the first surface of the nozzle plate facing the nozzle mount.

5. The variable-geometry exhaust turbine according to claim 3 ,
wherein a housing-and-retaining part forming body is fixed to at least one of the nozzle mount or the nozzle plate, the housing-and-retaining part forming body being formed as a separate member from the nozzle mount and the nozzle plate, and including the housing-and-retaining part formed inside.

6. The variable-geometry exhaust turbine according to claim 2 ,
wherein the end portion formed in the spherical shape of the nozzle support is housed in the housing-and-retaining part, by fixing a retaining member formed as a separate member from the nozzle mount and the nozzle plate into an insertion inlet of the housing-and-retaining part while the end portion formed in the spherical shape is inserted from the insertion inlet to be disposed in the housing-and-retaining part, the insertion inlet being an opening into which the end portion formed in the spherical shape is loosely insertable.

7. The variable-geometry exhaust turbine according to claim 2 ,
wherein the end portion formed in the spherical shape of the nozzle support is housed in the housing-and-retaining part, by press fitting the end portion formed in the spherical shape from a press-fit inlet of the housing-and-retaining part, the press-fit inlet being an opening into which the end portion formed in the spherical shape is not loosely insertable.

8. The variable-geometry exhaust turbine according to claim 2 ,
wherein the nozzle support includes two segments, which are a first-end-side segment having the first end portion formed in the spherical shape and a second-end-side segment having the second end portion formed in the spherical shape, and
wherein the first-end-side segment and the second-end-side segment are joined to each other while the first end portion of the first-end-side segment is housed in a mount-side housing-and-retaining part formed on the nozzle mount and the second end portion of the second-end-side segment is housed in a plate-side housing-and-retaining part formed on the nozzle plate.

9. The variable-geometry exhaust turbine according to claim 1 ,
wherein the nozzle support includes a nozzle support body, and a joint part including a trunk portion having a rod shape and protruding from at least one of end surfaces of the nozzle support body and a head portion disposed on a distal end side of the trunk portion, the head portion having a cross section larger than that of the trunk portion, and
wherein a through hole into which the trunk portion of the joint part is loosely inserted is formed on at least one of the nozzle mount or the nozzle plate, and a joint housing part in which the head portion of the joint part is slidably disposed is formed in a recess shape on the second surface of the at least one of the nozzle mount or the nozzle plate.

10. The variable-geometry exhaust turbine according to claim 9 ,
wherein the joint part includes a fastening member joined to one of the end surfaces of the nozzle support body.

11. The variable-geometry exhaust turbine according to claim 10 ,
wherein a spherical washer is disposed on the joint housing part, and
wherein the fastening member includes a spherical convex portion formed so as to be slidable with respect to a spherical concave seating surface of the spherical washer, between the head portion and the trunk portion.

12. The variable-geometry exhaust turbine according to claim 11 ,
wherein a spherical section formed in a spherical shape is formed on the first surface of at least one of the nozzle mount or the nozzle plate, and
wherein at least one of the end surfaces of the nozzle support body is formed so as to be slidable with respect to the spherical section.

13. The variable-geometry exhaust turbine according to claim 9 ,
wherein the head portion of the joint part is formed by swaging a distal end of the trunk portion, while the trunk portion is loosely inserted into the through hole and a distal end side of the trunk portion is protruded from the joint housing part.

14. The variable-geometry exhaust turbine according to claim 9 ,
wherein the joint housing part is formed in a spherical concave shape, and
wherein the head portion of the joint part is formed in a spherical convex shape at a side adjacent to the trunk portion so as to fit slidably with the joint housing part formed in a spherical concave shape.

15. The variable-geometry exhaust turbine according to claim 14 ,
wherein a second elastic member is disposed between at least one of the end surfaces of the nozzle support body and the first surface of at least one of the nozzle mount or the nozzle plate.

16. The variable-geometry exhaust turbine according to any one of claim 14 ,
wherein a slit for allowing tilting of the nozzle support body along the radial direction is formed on at least one of end portions of the nozzle support body.

17. The variable-geometry exhaust turbine according to claim 9 ,
wherein the joint housing part is formed in a conical concave shape, and
wherein an elastic m

Assignees

• Mitsubishi Heavy Ind Ltd

Inventors

• Hayashi Noriyuki
• Himeno Takamitsu
• Arai Takashi
• NAGAYO Yukihide
• Aiba Mitsuru
• Yokoyama Takao
• Hoshi Toru
• ARIMIZU Hiroyuki
• Sakon Toshio

Classifications

• F02B39/00

  Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00 · CPC title

• F02B37/24 Primary

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

• Y02T10/144

  Cross-Sectional Technologies · mapped topic

• F01D17/165

  for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line (F01D17/167 takes precedence) · CPC title

• F05D2220/40

  in turbochargers · CPC title