IP Library Granted Patent US 9,664,056
Granted Patent B2
US 9,664,056 · App. 13/974,150 · Granted May 30, 2017

Turbine system and adapter

Inventors: Nicholas Alvin Hogberg (Greenville, SC); Andres Jose Garcia-Crespo (Greenville, SC)
Assignee: General Electric Company
F01D5/3015F01D5/3007F01D5/3084F01D5/326
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Quick Facts
Patent No.
US 9,664,056
App. No.
13/974,150
Granted
May 30, 2017
Kind
B2
Abstract

A turbine system and adapter are disclosed. The adapter includes a turbine attachment portion having a first geometry arranged to receive a corresponding geometry of a wheelpost of a turbine rotor, and a bucket attachment portion having a second geometry arranged to receive a corresponding geometry of a root portion of a non-metallic turbine bucket. Another adapter includes a turbine attachment portion arranged to receive a plurality of wheelposts of a turbine rotor, and a bucket attachment portion arranged to receive a plurality of non-metallic turbine buckets having single dovetail configuration root portions. The turbine system includes a turbine rotor wheel configured to receive metal buckets, at least one adapter secured to at least one wheelpost on the turbine rotor wheel, and at least one non-metallic bucket secured to the at least one adapter.

Claims (30)

1. An adapter comprising:

a single turbine attachment portion on a first mating side of the adapter, the single turbine attachment portion having a first geometry arranged to contact and receive a corresponding geometry of a single wheelpost of a turbine rotor comprising a plurality of wheelposts comprising the single wheelpost, the plurality of wheelposts defining and separating a plurality of receiving portions of the turbine rotor; and

a single bucket attachment portion on a second mating side opposite the first mating side, the single bucket attachment portion having a second geometry arranged to receive and retain a corresponding geometry of a single root portion of a single non-metallic turbine bucket comprising the single root portion.

2. The adapter of claim 1 , wherein the single turbine attachment portion having the first geometry comprises a turbine rotor interface.

3. The adapter of claim 1 , wherein the single bucket attachment portion having a second geometry comprises a bucket interface.

4. The adapter of claim 1 , wherein the single bucket attachment portion is arranged to receive the second geometry of the single non-metallic turbine bucket, wherein the second geometry corresponds to a zero skew angle dovetail.

5. The adapter of claim 1 , wherein the single bucket attachment portion is arranged to receive the second geometry of the single non-metallic turbine bucket, wherein the second geometry corresponds to a non-zero skew angle dovetail.

6. The adapter of claim 1 , wherein the single bucket attachment portion is arranged to receive the second geometry of the single non-metallic turbine bucket, wherein the second geometry corresponds to a curved dovetail.

7. The adapter of claim 1 , comprising a wheelpost locking tab in the single turbine attachment portion.

8. The adapter of claim 1 , comprising a dovetail locking tab in the single bucket attachment portion.

9. The adapter of claim 1 , comprising a lockwire for axial retention in the single turbine attachment portion and the single bucket attachment portion.

10. The adapter of claim 1 , comprising a wear couple on at least one of the first mating side and the second mating side of the adapter.

11. The adapter of claim 1 , comprising a wear resistant coating applied over at least one of the first mating side and the second mating side of the adapter.

12. An adapter comprising:

a plurality of turbine attachment portions on a first mating side of the adapter, each of the plurality of turbine attachment portions being arranged to contact and receive one of a plurality of wheelposts of a turbine rotor, the plurality of wheelposts defining and separating a plurality of receiving portions of the turbine rotor; and

a plurality of bucket attachment portions on a second mating side opposite the first mating side, each of the plurality of bucket attachment portions being arranged to receive and retain a single dovetail root portion of one of a plurality of non-metallic turbine buckets having the single dovetail configuration root portions;

wherein the plurality of turbine attachment portions are equal in number to the plurality of bucket attachment portions.

13. The adapter of claim 12 , further comprising material selected from the group consisting of metal, ceramic, ceramic matrix composite, intermetallic material and metal matrix composite.

14. A turbine system comprising:

a turbine rotor wheel configured to receive metal buckets, the turbine rotor wheel comprising a plurality of wheelposts defining and separating a plurality of receiving portions of the turbine rotor;

at least one adapter contacting, receiving, and secured to at least one wheelpost of the plurality of wheelposts of the turbine rotor wheel on a first mating side of the at least one adapter; and

at least one non-metallic bucket having a root portion secured to the at least one adapter on a second mating side of the at least one adapter opposite the first mating side;

wherein the at least one adapter radially aligns each of the root portions with one of the at least one wheelpost; and

wherein the at least one non-metallic bucket is selected from the group of materials consisting of ceramic, ceramic matrix composite, intermetallic material, and metal matrix composite.

15. The turbine system of claim 14 , wherein the at least one adapter positions the at least one non-metallic bucket radially outward from the turbine rotor wheel.

16. The turbine system of claim 15 , wherein the at least one non-metallic bucket comprises a short shank bucket.

17. The turbine system of claim 16 , wherein a flow path of the turbine system remains unchanged.

18. The turbine system of claim 17 , wherein the metal buckets further comprise a fir tree-type root portion.

19. The turbine system of claim 17 , wherein the at least one adapter reduces a cooling air flow of the turbine system.

20. The turbine system of claim 17 , wherein the at least one adapter is resistant to bending moments applied to the at least one non-metallic bucket.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 17, 2023
From: GENERAL ELECTRIC COMPANY
To: GE INFRASTRUCTURE TECHNOLOGY LLC
Reel/Frame 065727/0001 →
CONFIRMATORY LICENSE Recorded Jun 7, 2018
From: GENERAL ELECTRIC GLOBAL RESEARCH CTR
To: UNITED STATES DEPARTMENT OF ENERGY
Reel/Frame 046314/0156 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 23, 2013
From: HOGBERG, NICHOLAS ALVIN; GARCIA-CRESPO, ANDRES JOSE
To: GENERAL ELECTRIC COMPANY
Reel/Frame 031067/0945 →
Continuity (1)
Related Publication 20150056080A1 · Feb 26, 2015