Nozzle device and exhaust turbocharger

Patent metadata

Field	Value
Publication number	US-11713709-B2
Application number	US-201917442025-A
Country	US
Kind code	B2
Filing date	Mar 28, 2019
Priority date	Mar 28, 2019
Publication date	Aug 1, 2023
Grant date	Aug 1, 2023

Abstract

A nozzle device according to some embodiments includes an annular nozzle plate, an annular nozzle mount defining a nozzle flow passage between the nozzle mount and one surface of the nozzle plate, at least one nozzle support coupling the nozzle plate and the nozzle mount, and fixed to at least the nozzle plate by caulking, and at least one nozzle vane supported between the nozzle plate and the nozzle mount. The nozzle plate has a through hole into which an end portion of the at least one nozzle support is inserted. The through hole includes a straight portion extending from the one surface toward another surface of the nozzle plate, an enlarged diameter portion formed on a side of the another surface of the nozzle plate and having a larger diameter than the straight portion, and a relief processing portion which is formed in a part of the straight portion continuing into the enlarged diameter portion and has a larger diameter than another part of the straight portion where the relief processing portion is not formed.

First claim

The invention claimed is:

1. A nozzle device, comprising:
an annular nozzle plate;
an annular nozzle mount defining a nozzle flow passage between the nozzle mount and one surface of the nozzle plate;
at least one nozzle support coupling the nozzle plate and the nozzle mount, and fixed to at least the nozzle plate by caulking; and
at least one nozzle vane supported between the nozzle plate and the nozzle mount,
wherein the nozzle plate has a through hole into which an end portion of the at least one nozzle support is inserted, and
wherein the through hole includes:
a straight portion extending from the one surface toward another surface of the nozzle plate;
an enlarged diameter portion formed on a side of the another surface of the nozzle plate and having a larger diameter than the straight portion; and
a relief processing portion which is formed in a part of the straight portion continuing into the enlarged diameter portion and has a larger diameter than another part of the straight portion where the relief processing portion is not formed, the relief processing portion having a constant diameter and extending along an extending direction of the through hole.

2. The nozzle device according to claim 1 ,
wherein a surface forming the enlarged diameter portion is formed into a tapered shape.

3. The nozzle device according to claim 1 ,
wherein the nozzle mount is fixed to a bearing housing, and
wherein the nozzle plate is supported by the nozzle mount via the nozzle support.

4. An exhaust turbocharger, comprising:
the nozzle device according to claim 1 .

5. A nozzle device, comprising:
an annular nozzle plate;
an annular nozzle mount defining a nozzle flow passage between the nozzle mount and one surface of the nozzle plate;
at least one nozzle support coupling the nozzle plate and the nozzle mount, and fixed to at least the nozzle plate by caulking; and
at least one nozzle vane supported between the nozzle plate and the nozzle mount,
wherein the nozzle plate has a through hole into which an end portion of the at least one nozzle support is inserted,
wherein the through hole includes:
a straight portion extending from the one surface toward another surface of the nozzle plate; and
an enlarged diameter portion formed on a side of the another surface of the nozzle plate and having a larger diameter than the straight portion, and

wherein the at least one nozzle support includes:
a caulking portion which contacts a surface forming the enlarged diameter portion; and
a non-caulking portion which is disposed with a gap between the non-caulking portion and a surface forming a part of the straight portion continuing into the enlarged diameter portion.

6. The nozzle device according to claim 5 ,
wherein a surface forming the enlarged diameter portion is formed into a tapered shape.

7. The nozzle device according to claim 5 ,
wherein the nozzle mount is fixed to a bearing housing, and
wherein the nozzle plate is supported by the nozzle mount via the nozzle support.

8. The nozzle device according to claim 5 ,
wherein the nozzle plate has a thermal expansion coefficient which is larger than a thermal expansion coefficient of the nozzle support.

9. An exhaust turbocharger, comprising:
the nozzle device according to claim 5 .

10. A nozzle device, comprising:
an annular nozzle plate;
an annular nozzle mount defining a nozzle flow passage between the nozzle mount and one surface of the nozzle plate;
at least one nozzle support coupling the nozzle plate and the nozzle mount, and fixed to at least the nozzle plate by caulking; and
at least one nozzle vane supported between the nozzle plate and the nozzle mount,
wherein the nozzle plate has a through hole into which an end portion of the at least one nozzle support is inserted, and
wherein the through hole includes:
a straight portion extending from the one surface toward another surface of the nozzle plate;
an enlarged diameter portion formed on a side of the another surface of the nozzle plate and having a larger diameter than the straight portion; and
a relief processing portion which is formed in a part of the straight portion continuing into the enlarged diameter portion and has a larger diameter than another part of the straight portion where the relief processing portion is not formed,

wherein,
when L1 is a distance between a center of the through hole and the radially outermost position, with respect to the nozzle plate, in a relief processing portion forming surface forming the relief processing portion,
when L2 is a distance between the center of the through and the radially innermost position, with respect to the nozzle plate, in the relief processing portion forming surface, and
wherein a relationship L1<L2 is satisfied.

11. The nozzle device according to claim 10 ,
wherein a center of the relief processing portion is at a position offset to the radially inner side of the nozzle plate relative to the center of the through hole.

12. A nozzle device, comprising:
an annular nozzle plate;
an annular nozzle mount defining a nozzle flow passage between the nozzle mount and one surface of the nozzle plate;
at least one nozzle support coupling the nozzle plate and the nozzle mount, and fixed to at least the nozzle plate by caulking; and
at least one nozzle vane supported between the nozzle plate and the nozzle mount,
wherein the nozzle plate has a through hole into which an end portion of the at least one nozzle support is inserted, and
wherein the through hole includes:
a straight portion extending from the one surface toward another surface of the nozzle plate;
an enlarged diameter portion formed on a side of the another surface of the nozzle plate and having a larger diameter than the straight portion; and
a relief processing portion which is formed in a part of the straight portion continuing into the enlarged diameter portion and has a larger diameter than another part of the straight portion where the relief processing portion is not formed, and

wherein the relief processing portion has an inner diameter A 2 which is not less than 1.1×A 1 and not greater than 1.5×A 1 , where A 1 is an outer diameter of the nozzle support.

13. A nozzle device, comprising:
an annular nozzle plate;
an annular nozzle mount defining a nozzle flow passage between the nozzle mount and one surface of the nozzle plate;
at least one nozzle support coupling the nozzle plate and the nozzle mount, and fixed to at least the nozzle plate by caulking; and
at least one nozzle vane supported between the nozzle plate and the nozzle mount,
wherein the nozzle plate has a through hole into which an end portion of the at least one nozzle support is inserted, and
wherein the through hole includes:
a straight portion extending from the one surface toward another surface of the nozzle plate;
an enlarged diameter portion formed on a side of the another surface of the nozzle plate and having a larger diameter than the straight portion; and
a relief processing portion which is formed in a part of the straight portion continuing into the enlarged diameter portion and has a larger diameter than another part of the straight portion where the relief processing portion is not formed, and

wherein the nozzle plate has a thermal expansion coefficient which is larger than a thermal expansion coefficient of the nozzle support.

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Sakamoto Keigo
• Katou Eigo
• Sakurai Tsuyoshi
• Sakuma Shigeyoshi
• Dammoto Yosuke
• Akiyama Yoji

Classifications

• F02B37/24 Primary

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

• F16B17/006

  of rods or tubes to sheets or plates · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title