Variable nozzle device and variable-geometry type exhaust turbocharger

Patent metadata

Field	Value
Publication number	US-11015518-B2
Application number	US-201716326633-A
Country	US
Kind code	B2
Filing date	Mar 16, 2017
Priority date	Mar 16, 2017
Publication date	May 25, 2021
Grant date	May 25, 2021

Abstract

A variable nozzle device includes: a first plate-shaped member having a first plate portion having an annular shape and being fixed to a bearing housing; a second plate-shaped member having a second plate portion which has an annular shape and which defines a nozzle flow passage between the first plate portion and the second plate portion, the second plate portion having a surface disposed so as to face the first plate portion and another surface disposed so as to face at least partially a scroll flow passage formed inside a turbine housing; at least one nozzle support having, with respect to an axial direction of the nozzle support, an end coupled to the first plate portion and another end coupled to the second plate portion; at least one nozzle vane rotatably supported between the first plate portion and the second plate portion; and a variable nozzle mechanism configured to change a vane angle of the at least one nozzle vane. The second plate portion is formed to have a larger thickness than the first plate portion.

First claim

The invention claimed is:

1. A variable nozzle device, comprising:
a first plate-shaped member having a first plate portion having an annular shape and being fixed to a bearing housing;
a second plate-shaped member having a second plate portion which has an annular shape and which defines a nozzle flow passage between the first plate portion and the second plate portion, the second plate portion having a surface disposed so as to face the first plate portion and another surface disposed so as to face at least partially a scroll flow passage formed inside a turbine housing;
at least one nozzle support having, with respect to an axial direction of the nozzle support, an end coupled to the first plate portion and another end coupled to the second plate portion;
at least one nozzle vane rotatably supported between the first plate portion and the second plate portion; and
a variable nozzle mechanism configured to change a vane angle of the at least one nozzle vane, the variable nozzle mechanism including a drive ring disposed so as to rotatable relative to the first plate-shaped member and at least one lever plate which has an end coupled to a nozzle shaft of the nozzle vane and another end coupled to the drive ring,
wherein the second plate portion is formed to have a larger thickness than the first plate portion,
wherein the first plate portion includes a radially inner portion supporting the nozzle vane and a radially outer portion positioned on a radially outer side of the radially inner portion,
wherein the radially inner portion is formed to have a larger thickness than the radially outer portion,
wherein the second plate portion is formed to have a larger thickness than the radially inner portion of the first plate portion, and
wherein the nozzle support includes a body portion positioned between the first plate-shaped member and the second plate-shaped member, the body portion having a small diameter portion which is formed in a center part with respect to the axial direction and which has two end portions and a smaller shaft diameter than both end portions of the body portion.

2. The variable nozzle device according to claim 1 ,
wherein a thickness dimension ratio T 1 /T 2 is 1.3-1.8, where T 1 is a thickness dimension of the second plate portion and T 2 is a thickness dimension of the first plate portion.

3. The variable nozzle device according to claim 1 ,
wherein the small diameter portion is formed to have a shaft diameter that increases from a side of the center part towards sides of both end portions in the axial direction.

4. The variable nozzle device according to claim 1 ,
wherein the nozzle support includes a second plate-shaped member side large diameter portion disposed continuously from the small diameter portion at a side of the second plate-shaped member, and formed to have a larger diameter than a second plate-shaped member side coupling portion coupled to the second plate-shaped member, and
wherein a shaft diameter ratio D 3 /D 2 is 0.6-0.9, where D 3 is a minimum diameter of the small diameter portion and D 2 is a diameter of the second plate-shaped member side large diameter portion.

5. The variable nozzle device according to claim 4 ,
wherein the nozzle support includes a first plate-shaped member side large diameter portion disposed continuously from the small diameter portion at a side of the first plate-shaped member, and formed to have a larger diameter than a first plate-shaped member side coupling portion coupled to the first plate-shaped member,
wherein a length dimension ratio H/L is 0.1-0.3, where H is a length dimension of the second plate-shaped member side large diameter portion in the axial direction and L is a total length dimension of the first plate-shaped member side large diameter portion, the second plate-shaped member side large diameter portion, and the small diameter portion in the axial direction, and
wherein a shaft diameter ratio D 1 /D 2 is 0.6-0.8, where D 1 is a diameter of the second plate-shaped member side coupling portion.

6. A variable-geometry type exhaust turbocharger, comprising the variable nozzle device according to claim 1 .

Assignees

• Mitsubishi Heavy Ind Ltd
• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Sakamoto Keigo
• Sakuma Shigeyoshi
• Katou Eigo
• Dammoto Yosuke
• Akiyama Yoji
• Seike Nariaki
• ARIMIZU Hiroyuki

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F02B37/24 Primary

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

• Y02T10/12

  Improving ICE efficiencies · CPC title

• 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

• F05D2240/128

  Nozzles · CPC title