Turbine casing, turbine, core for casting turbine casing, and method for producing turbine casing

• US 10,443,414 B2
• Filed: 07/03/2014
• Issued: 10/15/2019
• Est. Priority Date: 07/03/2014
• Status: Active Grant

• Current Assignee: Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. (Mitsubishi Heavy Industries, Ltd.)
• Original Assignee: Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. (Mitsubishi Heavy Industries, Ltd.)
• Inventors: Yokoyama, Takao, Akiyama, Yoji
• Primary Examiner(s): White, Dwayne J
• Assistant Examiner(s): Gillenwaters, Jackson N
• Application Number:
  US15/311,788
• Publication Number:
  US 20180223679A1
• Time in Patent Office: 1,930 Days
• CPC Class Codes: B22C 9/10 Cores; Manufacture or installation of cores breaker cores B22C9/084
• CPC Class Codes: F01D 25/24 Casings modified for heating or cooling F01D25/14; Casing parts, e.g. diaphragms, casing fastenings casings for rotary machines or engines in general F16M ; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045
• CPC Class Codes: F01D 9/026 Scrolls for radial machines or engines
• CPC Class Codes: F02B 37/025 Multiple scrolls or multiple gas passages guiding the gas to the pump drive
• CPC Class Codes: F02B 39/00 Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F05D 2230/21 by casting
• CPC Class Codes: F05D 2240/14 Casings or housings protecting or supporting assemblies within

Abstract

A turbine casing includes: a shroud of a cylindrical shape defining an operational flow path between the shroud and a hub of a turbine rotor; a scroll outer peripheral wall continuing from an end side of the shroud and extending along a circumferential direction of the shroud; and a partition wall disposed inside the scroll outer peripheral wall and dividing an inside of the scroll outer peripheral wall into a first scroll flow path and a second scroll flow path disposed adjacent to each other in an axial direction of the shroud. The shroud, the scroll outer peripheral wall, and the partition wall are formed integrally by casting. The partition wall has a widening section which partially increases a communication area between at least two of the first scroll flow path, the second scroll flow path, and the operational flow path, in the circumferential direction of the shroud.

Claims

1. A turbine casing, comprising:

a shroud of a cylindrical shape defining an operational flow path between the shroud and a hub of a turbine rotor;

a scroll outer peripheral wall continuing from an end side of the shroud and extending along a circumferential direction of the shroud; and

a partition wall disposed inside the scroll outer peripheral wall and dividing an inside of the scroll outer peripheral wall into a first scroll flow path and a second scroll flow path disposed adjacent to each other in an axial direction of the shroud,

wherein the shroud, the scroll outer peripheral wall, and the partition wall are formed integrally by casting,

wherein the partition wall, from a root end to a far end, is formed of molten metal poured into a runner formed between a main mold and a core,

wherein the partition wall has a widening section which partially increases a communication area between at least two of the first scroll flow path, the second scroll flow path, and the operational flow path, in the circumferential direction of the shroud,

wherein the widening section includes at least one cutout portion provided for an inner peripheral side of the partition wall, and

wherein the at least one cutout portion includes a plurality of cutout portions disposed rotationally symmetric with respect to an axis of the shroud.

4. A turbine comprising the turbine casing according to claim 1.

2. A turbine casing, comprising:

a shroud of a cylindrical shape defining an operational flow path between the shroud and a hub of a turbine rotor;

a scroll outer peripheral wall continuing from an end side of the shroud and extending along a circumferential direction of the shroud; and

a partition wall disposed inside the scroll outer peripheral wall and dividing an inside of the scroll outer peripheral wall into a first scroll flow path and a second scroll flow path disposed adjacent to each other in an axial direction of the shroud,

wherein the shroud, the scroll outer peripheral wall, and the partition wall are formed integrally by casting,

wherein the partition wall, from a root end to a far end, is formed of molten metal poured into a runner formed between a main mold and a core,

wherein the partition wall has a widening section which partially increases a communication area between at least two of the first scroll flow path, the second scroll flow path, and the operational flow path, in the circumferential direction of the shroud, and

wherein the partition wall includes a rectifying portion disposed around the at least one through hole.

5. A turbine comprising the turbine casing according to claim 2.

3. A turbine casing, comprising:

a shroud of a cylindrical shape defining an operational flow path between the shroud and a hub of a turbine rotor;

a scroll outer peripheral wall continuing from an end side of the shroud and extending along a circumferential direction of the shroud; and

a partition wall disposes inside the scroll outer peripheral wall and dividing an inside of the scroll outer peripheral wall into a first scroll flow path and a second scroll flow path disposed adjacent to each other in an axial direction of the shroud,

wherein the shroud, the scroll outer peripheral wall, and the partition wall are formed integrally by casting,

wherein the partition wall, from a root end to a far end, is formed of molten metal poured into a runner formed between a main mold and a core,

wherein the partition wall has a widening section which partially increases a communication area between at least two of the first scroll flow path, the second scroll flow path, and the operational flow path, in the circumferential direction of the shroud,

wherein the widening section includes at least one bend portion provided for an inner peripheral side of the partition wall, and

wherein the at least one bend portion includes;

at least one first bend portion widening a throat portion of the first scroll flow path facing the operational flow path; and

at least one second bend portion widening a throat portion of the second scroll flow path facing the operational flow path.

6. A turbine comprising the turbine casing according to claim 3.