Flow path structure and gas turbine exhaust diffuser

Patent metadata

Field	Value
Publication number	US-9732674-B2
Application number	US-201013991796-A
Country	US
Kind code	B2
Filing date	Dec 24, 2010
Priority date	Dec 24, 2010
Publication date	Aug 15, 2017
Grant date	Aug 15, 2017

Abstract

A flow path structure includes a wall surface in which a flow path is formed, a structure configured to extend in a direction intersecting a main stream direction of a fluid flowing through the flow path from the wall surface, and a concave section forming region formed throughout a range including the structure in the main stream direction and having a concave section formed in the wall surface. As the structure occupies a partial range of the flow path in the flow path cross section intersecting the main stream, a cross-sectional area of the flow path is varied in accordance with positional variation in the main stream direction.

First claim

The invention claimed is:

1. An exhaust diffuser of a gas turbine comprising:
a wall surface in which an annular flow path is formed;
a structure configured to extend in a direction intersecting a main stream direction of a fluid flowing through the flow path from the wall surface; and
a concave section forming region formed throughout a range comprising the structure in the main stream direction and in a circumferential direction of the wall surface and having a concave section formed in the wall surface,
wherein the concave section, in a flow path cross section, gradually deepens and then gradually becomes shallow from one side toward the other side in the circumferential direction, and
the concave section, in the flow path cross section, is configured to be the deepest in the circumferential direction of the flow path at a position from which the structure of the wall surface extends, and
wherein, as the structure occupies a partial range of the flow path in the flow path cross section intersecting the main stream, a cross-sectional area of the flow path is varied in accordance with positional variation in the main stream direction.

2. The exhaust diffuser according to claim 1 , wherein the concave section is configured such that a portion of a trajectory of a variation in cross-sectional area of the flow path in accordance with positional variation in the main stream direction within a range where the structure is provided is disposed between a trajectory of the variation in cross-sectional area of the flow path in case that the structure and the concave section are not prepared and a trajectory of the variation in cross-sectional area of the flow path in case that the concave section is not prepared.

3. The exhaust diffuser according to claim 2 , wherein the concave section is formed at a range from a position of an upstream side spaced a distance of 0.4 L from a front edge to a position of a downstream side spaced a distance of 0.4 L from a rear edge when a length from the front edge to the rear edge of the structure in the main stream direction is L.

4. The exhaust diffuser according to claim 3 , wherein the concave section is formed at a range from a position of the upstream side spaced a distance of 0.2 L from the front edge and a position of the downstream side spaced a distance of 0.2 L from the rear edge.

5. The exhaust diffuser according to claim 1 , wherein the concave section is formed at a range from a position of an upstream side spaced a distance of 0.4 L from a front edge to a position of a downstream side spaced a distance of 0.4 L from a rear edge when a length from the front edge to the rear edge of the structure in the main stream direction is L.

6. The exhaust diffuser according to claim 5 , wherein the concave section is formed at a range from a position of the upstream side spaced a distance of 0.2 L from the front edge and a position of the downstream side spaced a distance of 0.2 L from the rear edge.

7. The exhaust diffuser according to claim 1 , wherein
the concave section forming region includes two regions that are an upstream concave section forming region and a downstream concave section forming region being in a position downstream of the upstream concave section forming region.

8. The exhaust diffuser according to claim 7 , further comprising:
an exhaust casing connected to a turbine casing; and
a protection casing installed in the exhaust casing,
wherein the structure includes:
a plurality of struts extending from the exhaust casing to the inside of the protection casing; and
a manhole disposed at a downstream side of the plurality of struts, and
wherein the upstream concave section forming region covers a range in which the plurality of struts is provided, and
the downstream concave section forming region covers a range in which the manhole is provided.

Assignees

• Sakamoto Yasuro
• Ito Eisaku
• Wakazono Susumu
• Mitsubishi Hitachi Power Sys

Inventors

• Sakamoto Yasuro
• Ito Eisaku
• Wakazono Susumu

Classifications

• F01D5/143

  Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour · CPC title

• F05D2250/712

  concave · CPC title

• F01D25/30 Primary

  Exhaust heads, chambers, or the like · CPC title

• F02C7/00 Primary

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title

• F01D25/162

  Bearing supports · CPC title