Turbine intrusion loss reduction system

Patent metadata

Field	Value
Publication number	US-2016281518-A1
Application number	US-201615171094-A
Country	US
Kind code	A1
Filing date	Jun 2, 2016
Priority date	Oct 2, 2012
Publication date	Sep 29, 2016
Grant date	—

Abstract

Systems and devices configured to reduce windage and mixing losses in a turbine by redirecting and/or aligning a direction of a leakage flow with the flowpath of the main flow of a turbine are disclosed. In one embodiment, a device includes: a base configured to connect to a diaphragm of a turbine; and a radial portion connected to the base and extending radially inboard from the base toward a rotor of the turbine, the radial portion oriented to adjust a direction of travel of a leakage flow of working fluid radially inboard at an angle complementary to a primary working fluid path of the turbine.

First claim

What is claimed is:

1 . A device comprising:
a member configured to connect to an outermost diaphragm of a turbine and oriented to adjust a direction of a leakage flow of working fluid to a radially inboard direction at an angle complementary to a primary working fluid path of the turbine; and a first set of ridges extending from the member in an upstream direction relative to the member, each ridge in the first set of ridges circumferentially distanced from one another.

2 . The device of claim 1 , wherein the first set of ridges is disposed on an upstream facing surface of the member, the first set of ridges oriented substantially radially and is distanced radially inboard from the diaphragm.

3 . The device of claim 2 , further comprising:
a second set of ridges oriented substantially radially and extending in an upstream direction relative to the member, the second set of ridges disposed on the upstream facing surface of the member radially inboard of the first set of ridges and physically distinct from the first set of ridges.

4 . The device of claim 1 , wherein the first set of ridges are oriented at least one of:
straight, inclined, or curved.

5 . The device of claim 1 , wherein the member is located axially upstream relative at least one nozzle.

6 . The device of claim 1 , wherein the first set of ridges includes:
a first flange; a central portion connected to the first flange, the central portion extending circumferentially; and a second flange connected to the central portion, the second flange located substantially opposite the first flange.

7 . The device of claim 1 , wherein each ridge in the set of ridges has a first radial length substantially equal to a second radial length of the member.

8 . A turbine diaphragm system comprising:
an outer ring; a set of nozzles disposed circumferentially about an interior of the outer ring, the set of nozzles extending radially inboard; a member connected to an inner surface of the outer ring and extending circumferentially about the outer ring adjacent to a portion of the set of nozzles, the member oriented to adjust a direction of a leakage flow of working fluid radially inboard direction at an angle complementary to a primary working fluid path of a turbine; and a first set of ridges extending from the member in an upstream direction relative to the member, each ridge in the first set of ridges circumferentially distanced from one another; and an inner ring radially inboard of the outer ring and connected to the set of nozzles.

9 . The turbine diaphragm system of claim 8 , wherein the member extends continuously along a circumference of the outer ring.

10 . The turbine diaphragm system of claim 8 , wherein the member includes a plurality of members disposed intermittently about a circumference of the outer ring.

11 . The turbine diaphragm system of claim 8 , wherein the first set of ridges is disposed on an upstream facing surface of the member, the first set of ridges is oriented substantially radially and is distanced radially inboard from the outer ring.

12 . The turbine diaphragm system of claim 11 , further comprising:
a second set of ridges oriented substantially radially and extending in an upstream direction relative to the member, the second set of ridges disposed on the upstream facing surface of the member radially inboard of the first set of ridges and physically distinct from the first set of ridges.

13 . The turbine diaphragm system of claim 8 , wherein the first set of ridges is oriented at least one of: straight, inclined, or curved.

14 . The turbine diaphragm system of claim 8 , wherein the member is located axially upstream relative to at least one nozzle in the set of nozzles.

15 . The turbine diaphragm system of claim 8 , wherein the first set of ridges includes:
a first flange; a central portion connected to the first flange, the central portion extending circumferentially; and a second flange connected to the central portion, the second flange located substantially opposite the first flange.

16 . A turbine, comprising:
a stator; a turbine diaphragm system disposed within the stator, the turbine diaphragm system including:
an outer ring;
a set of nozzles disposed circumferentially about an interior of the outer ring, the set of nozzles extending radially inboard;
a member connected to an inner surface of the outer ring and extending circumferentially along the outer ring adjacent a portion of the set of nozzles, the member oriented to adjust a direction of a leakage flow of working fluid to a radially inboard direction at an angle complementary to a working fluid passage;
a first set of ridges extending from the member in an upstream direction relative to the member, each ridge in the first set of ridges circumferentially distanced from one another; and
an inner ring radially inboard of the outer ring and connected to the set of nozzles; and
a rotor configured radially inboard of the working fluid passage.

17 . The turbine of claim 16 , wherein the a first set of ridges is disposed on an upstream facing surface of the member, the first set of ridges is oriented substantially radially and is distanced radially inboard from the outer ring.

18 . The turbine of claim 17 , a second set of ridges oriented substantially radially and extending in an upstream direction relative to the member, the second set of ridges disposed on the upstream facing surface of the member radially inboard of the first set of ridges and physically distinct from the first set of ridges.

19 . The turbine of claim 17 , wherein the first set of ridges is oriented at least one of: straight, inclined, or curved.

20 . The turbine of claim 16 , wherein the first set of ridges includes:
a first flange; a central portion connected to the first flange, the central portion extending circumferentially; and a second flange connected to the central portion, the second flange located substantially opposite the first flange.

Assignees

• Gen Electric

Inventors

• Modachur Krishnan Prabakaran
• Barb Kevin Joseph
• Deshpande Srikanth
• Subramaniyan Moorthi

Classifications

• F05D2240/126

  Baffles or ribs · CPC title

• F01D9/04

  forming ring or sector · CPC title

• F01D5/145

  Means for influencing boundary layers or secondary circulations (for compressors F04D29/68) · CPC title

• F01D11/08

  for sealing space between rotor blade tips and stator (specially-shaped blade tips therefor F01D5/20) · CPC title

• Y02E20/16

  Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT] · CPC title