Turbine bucket having outlet path in shroud

Patent metadata

Field	Value
Publication number	US-11078797-B2
Application number	US-201916683659-A
Country	US
Kind code	B2
Filing date	Nov 14, 2019
Priority date	Oct 27, 2015
Publication date	Aug 3, 2021
Grant date	Aug 3, 2021

Abstract

A turbine bucket according to embodiments includes: a base; a blade coupled to base and extending radially outward from base, blade including: a body having: a pressure side; a suction side opposing pressure side; a leading edge between pressure side and suction side; and a trailing edge between pressure side and suction side on a side opposing leading edge; and a plurality of radially extending cooling passageways within body; and a shroud coupled to blade radially outboard of blade, shroud including: a plurality of radially extending outlet passageways fluidly connected with a first set of the plurality of radially extending cooling passageways within body; and an outlet path extending at least partially circumferentially through shroud and fluidly connected with all of a second, distinct set of the plurality of radially extending cooling passageways within body.

First claim

What is claimed is:

1. A turbine bucket comprising:
a base;
a blade coupled to the base and extending radially outward from the base, the blade including:
a body having:
a pressure side; a suction side opposing the pressure side; a leading edge between the pressure side and the suction side; and a trailing edge between the pressure side and the suction side on a side opposing the leading edge; and

a shroud coupled to the blade radially outboard of the blade, the shroud including:
a notch between a leading half and a trailing half of the shroud;

a first plurality of radially extending cooling passageways within the body on the leading half of the shroud;
a second plurality of radially extending cooling passageways within the body on the trailing half of the shroud; and
a first outlet path comprising outlet passageways extending radially through the shroud on the trailing half of the shroud; and
a second outlet path extending at least partially circumferentially through the trailing half of the shroud at the trailing edge of the body wherein the second outlet path exits the blade only at the trailing half of the shroud, wherein an entirety of cooling fluid passing through the first plurality of radially extending cooling passageways and an entirety of cooling fluid passing through the second plurality of radially extending cooling passageways exits only the first outlet path and the second outlet path.

2. The turbine bucket of claim 1 , further comprising a chamber, wherein the chamber is fluidly connected to the first outlet path, the second outlet path and the first plurality of radially extending cooling passageways.

3. The turbine bucket of claim 1 , wherein the second outlet path includes at least one rib/guide vane proximate the trailing edge for guiding a flow of cooling fluid exiting the body at a location adjacent the shroud.

4. The turbine bucket of claim 1 , further comprising a chamber fluidly connected to the first outlet path and the second outlet path.

5. The turbine bucket of claim 1 , wherein the notch delineates an approximate mid-point between the leading half and the trailing half of the shroud.

6. A turbine blade comprising:
a blade coupled to a base and extending radially outward from the base, the blade including:
a body having:
a pressure side; a suction side opposing the pressure side; a leading edge between the pressure side and the suction side; and a trailing edge between the pressure side and the suction side on a side opposing the leading edge; and

a shroud coupled to the blade radially outboard of the blade, the shroud including:
a notch between a leading half and a trailing half of the shroud;

a first plurality of radially extending cooling passageways within the body on the leading half of the shroud;
a second plurality of radially extending cooling passageways within the body on the trailing half of the shroud; and
a first outlet path comprising outlet passageways extending radially through the shroud on the trailing half of the shroud; and
a second outlet path extending at least partially circumferentially through the trailing half of the shroud at the trailing edge of the body wherein the second outlet path exits the blade only at the trailing half of the shroud, wherein an entirety of cooling fluid passing through the first plurality of radially extending cooling passageways and an entirety of the cooling fluid passing through the second plurality of radially extending cooling passageways exits only the first outlet path and the second outlet path.

7. The turbine blade of claim 6 , further comprising a chamber, wherein the chamber is fluidly connected to the first outlet path, the second outlet path and the first plurality of radially extending cooling passageways.

8. The turbine blade of claim 6 , wherein the second outlet path includes at least one rib/guide vane proximate the trailing edge for guiding a flow of cooling fluid exiting the body at a location adjacent the shroud.

9. The turbine blade of claim 6 , further comprising a chamber fluidly connected to the first outlet path and the second outlet path.

10. The turbine blade of claim 6 , wherein the notch delineates an approximate mid-point between the leading half and the trailing half of the shroud.

11. A turbine comprising:
a stator; and
a rotor contained within the stator, the rotor having:
a spindle; and
a plurality of buckets extending radially from the spindle, at least one of the plurality of buckets including:
a base;

a blade coupled to the base and extending radially outward from the base, the blade including:
a body having:
a pressure side; a suction side opposing the pressure side; a leading edge between the pressure side and the suction side; and a trailing edge between the pressure side and the suction side on a side opposing the leading edge; and

a shroud coupled to the blade radially outboard of the blade, the shroud including:
a notch between a leading half and a trailing half of the shroud;

a first plurality of radially extending cooling passageways within the body on the leading half of the shroud;
a second plurality of radially extending cooling passageways within the body on the trailing half of the shroud; and
a first outlet path comprising outlet passageways extending radially through the shroud on the trailing half of the shroud; and

a second outlet path extending at least partially circumferentially through the trailing half of the shroud at the trailing edge of the body wherein the second outlet path exits the blade only at the trailing half of the shroud, wherein an entirety of cooling fluid passing through the first plurality of radially extending cooling passageways and an entirety of cooling fluid passing through the second plurality of radially extending cooling passageways exits only the first outlet path and the second outlet path.

12. The turbine of claim 11 , further comprising a chamber, wherein the chamber is fluidly connected to the first outlet path, the second outlet path and the first plurality of radially extending cooling passageways.

13. The turbine of claim 11 , wherein the second outlet path includes at least one rib/guide vane proximate the trailing edge for guiding a flow of cooling fluid exiting the body at a location adjacent the shroud.

14. The turbine of claim 11 , further comprising a chamber fluidly connected to the first outlet path and the second outlet path.

15. The turbine of claim 11 , wherein the notch delineates an approximate mid-point between the leading half and the trailing half of the shroud.

Assignees

• Gen Electric

Inventors

• Chouhan Rohit
• Jaiswal Shashwat Swami
• Siden Gunnar Leif
• Taylor Zachary James

Classifications

• F01D1/32 Primary

  with pressure velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor, {e.g. Heron turbines (the working fluid being a combustion products F02C3/165; jet propulsion plants per se F02K)} · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F01D5/225

  by shrouding · CPC title

• F05D2240/30

  Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor · CPC title

• F01D5/02

  Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title