Rotor rim impingement cooling

Patent metadata

Field	Value
Publication number	US-2016146016-A1
Application number	US-201414551592-A
Country	US
Kind code	A1
Filing date	Nov 24, 2014
Priority date	Nov 24, 2014
Publication date	May 26, 2016
Grant date	—

Abstract

A system and method of cooling a radially outer surface of a rotor wheel post of a turbine wheel and a rotor wheel space between a turbine bucket and a rotor wheel post, including a turbine bucket having at least one cooling passage that extends between an inner cooling channel of the turbine bucket and an outer surface of a shank portion of the turbine bucket that directly faces a radially upper surface of the rotor wheel post, and using the cooling passage to direct cooling flow towards the radially upper surface of the rotor wheel post.

First claim

What is claimed is:

1 . A turbine bucket comprising:
an airfoil portion; a platform portion that is radially inward of the airfoil portion; a shank portion that is radially inward of the platform portion; and a root portion that is radially inward of the shank portion; wherein the shank portion includes at least one cooling passage extending between an inner cooling pocket or channel internal to the turbine bucket and an outer surface of the shank portion wherein the outer surface is adjacent a junction between the shank portion and the root portion.

2 . The turbine bucket of claim 1 , wherein the root portion of the turbine bucket is configured to engage a rotor wheel post on a turbine wheel.

3 . The turbine bucket of claim 2 , wherein the cooling passage is adapted to direct cooling flow towards a top surface of the rotor wheel post and/or adjacent surfaces.

4 . The turbine bucket of claim 1 , wherein the cooling passage has a size of a ratio of Z/D, in which Z is a distance from an exit of the cooling passage to a surface of the shank portion, and D is the diameter of the cooling passage.

5 . The turbine bucket of claim 4 , wherein the cooling passage has a ratio of about 1 to about 9.

6 . The turbine bucket of claim 1 , wherein the cooling passage has an approach angle of between about 30 degrees to about 90 degrees.

7 . The turbine bucket of claim 1 , wherein the cooling passage slants in an axial direction.

8 . The turbine bucket of claim 1 , further comprising a plurality of cooling passages, and the cooling passages are distributed uniformly or non-uniformly along a length of the shank portion.

9 . The turbine bucket of claim 1 , further comprising a plurality of cooling passages, and the cooling passages have non-uniform lengths and non-uniform axial slants along a length of the shank portion.

10 . A method to cool a wheel rim gap between a turbine bucket and a rotor wheel post, comprising:
forming a plurality of cooling passages along a length of a shank portion of a turbine bucket, the cooling passages fluidly connects at least one inner cooling pocket or channel inside the turbine bucket and an outer surface of the shank portion that is immediately radially outward of the root portion of the turbine bucket; supplying a cooling gas flow to the inner cooling channel on the inside of the turbine bucket that is connected to the cooling passages; redirecting the cooling gas flow to pass through the cooling passages flow onto a radially outer surface of a rotor wheel post on a turbine wheel that is immediately abutting the cooling passages; and cooling the radially outer surface of a rotor wheel post using the cooling gas flow redirected by the cooling passages.

11 . The method of claim 10 , wherein the radially outer surface of a rotor wheel post is a dead rim of the turbine wheel.

12 . The method of claim 10 , wherein the cooling passage has a size of a ratio of Z/D, in which Z is a distance from an exit of the cooling passage to a surface of the shank portion, and D is the diameter of the cooling passage.

13 . The method of claim 10 , wherein the cooling passage has a ratio of about 1 to about 9.

14 . The method of claim 10 , wherein the cooling passage has an approach angle of between about 30 degrees to about 90 degrees.

15 . A turbine wheel and bucket assembly comprising:
a turbine wheel including a plurality of rotor wheel posts forming rotor wheel slots on a radially outer rim of the turbine wheel; turbine buckets extending radially outward from the outer rim of the turbine wheel, wherein each of the buckets includes an airfoil, a shank section and a root, wherein the root is seated in one of the rotor wheel slots; an cooling passage in the shank of each of the turbine buckets, wherein cooling passage extends between an inner cooling channel in the turbine bucket and an outer surface of the shank of the turbine bucket at a region of the shank that is abutting a radially outer surface of the rotor wheel posts; and a wheel rim gap between the turbine buckets and the rotor wheel posts; wherein the cooling passages are adapted to direct a cooling flow from the inner cooling channel onto the radially outer surface of the rotor wheel posts and into the wheel rim gap.

16 . The turbine wheel and bucket assembly of claim 15 , wherein the radially outer surface of a rotor wheel post is a dead rim of the turbine wheel.

17 . The turbine wheel and bucket assembly of claim 15 , wherein the cooling passage has a size of a ratio of Z/D, in which Z is a distance from an exit of the cooling passage to a surface of the shank portion, and D is the diameter of the cooling passage.

18 . The turbine wheel and bucket assembly of claim 15 , wherein the cooling passage has a ratio of about 1 to about 9.

19 . The turbine wheel and bucket assembly of claim 15 , wherein the cooling passage has an approach angle of between about 30 degrees to about 90 degrees.

20 . The turbine wheel and bucket assembly of claim 15 , further comprising a source of cooling flow drawn from an inner portion of the turbine wheel into the turbine bucket inner cooling channel.

Assignees

• Gen Electric

Inventors

• Johns David Richard
• Fedor Michael James
• Giametta Andrew Paul

Classifications

• F05D2260/201

  by impingement of a fluid · CPC title

• F01D5/187 Primary

  Convection cooling · CPC title

• F01D5/3023

  of radial insertion type, e.g. in individual recesses · CPC title

• F01D5/081

  Cooling fluid being directed on the side of the rotor disc or at the roots of the blades (F01D5/087 takes precedence) · CPC title

• F01D5/3007 Primary

  of axial insertion type · CPC title