Internally cooled turbine blisk and method of manufacture

Patent metadata

Field	Value
Publication number	US-9903214-B2
Application number	US-201514721681-A
Country	US
Kind code	B2
Filing date	May 26, 2015
Priority date	May 26, 2015
Publication date	Feb 27, 2018
Grant date	Feb 27, 2018

Abstract

A method of manufacturing an internally cooled blisk by additive manufacturing processes to provide weight reduction and power-to-weight ratio improvement, leading to improved efficiency, a decrease in fuel burn and lifecycle costs in an engine employing the internally cooled blisk. The method of manufacturing including defining a configuration for the internally cooled blisk, the configuration comprising a disk, an annular array of angularly spaced blades extending about a periphery of the disk and one or more internal cooling features defined within the internally cooled blisk. The method further including the step of programming the configuration into an additive manufacturing system. A powder is deposited into a chamber and an energy source is applied to the deposited powder to consolidate the powder into a cross-sectional shape corresponding to the defined configuration. Additionally provided is an internally cooled blisk.

First claim

The invention claimed is:

1. A method of manufacturing an internally cooled blisk comprising:
defining a configuration for the internally cooled blisk comprising a disk, an annular array of angularly spaced blades extending about a periphery of the disk and internal cooling features, wherein the internal cooling features include having a first portion of a cooling fluid flow providing cooling to the angularly spaced blades via a plurality of cooling channels defined in each of the angularly spaced blades and the first portion exiting an effusion blade surface defined on each of the angularly spaced blades and having a second portion of the cooling fluid flow bypassing the plurality of cooling channels to cool a downstream side of the disk via one or more passages defining a plurality of discrete branch structures between the disk and each of the angularly spaced blades;
programming the configuration into an additive manufacturing system;
depositing a powder into a chamber;
applying an energy source to the deposited powder; and
consolidating the powder into a cross-sectional shape corresponding to the defined configuration.

2. The method of claim 1 , further including at least one of a plurality of passages defined in the disk and one or more cooling plates defined in the internally cooled blisk.

3. The method of claim 2 , wherein the one or more passages defining a plurality of discrete branch structures includes a web transition.

4. The method of claim 1 , wherein the powder comprises a metal powder.

5. The method of claim 4 , wherein the powder comprises a nickel-based or cobalt-based superalloy.

6. The method of claim 1 , wherein the powder comprises a ceramic powder.

7. The method of claim 1 , wherein the powder comprises a composite powder.

8. The method of claim 1 , further comprising repeating the depositing, applying, and consolidating steps to construct the internally cooled blisk having the defined configuration.

9. The method of claim 1 , wherein the internally cooled blisk is not axisymmetric.

10. A method of manufacturing an internally cooled blisk comprising:
defining a configuration for the internally cooled blisk, the configuration comprising
a disk,
an annular array of angularly spaced blades extending about a periphery of the disk and
cooling fluid flow features in fluid communication with an input of a cooling fluid flow,
wherein the cooling fluid flow features comprise
one or more cooling plates,
one or more discrete branch structures in a web transition area where the disk meets each of the angularly spaced blades,
one or more cooling channels within angularly spaced blades,
one or more passages defined on a downstream side of the disk and
an effusion blade surface defined on one or more of the angularly spaced blades;

having a first portion of the cooling fluid flow provide cooling to the one or more cooling channels and exiting the effusion blade surface, and
having a second portion of the cooling fluid flow bypass the one or more cooling channels to the one or more passages via the one or more discrete branch structures in the web transition area;

programming the configuration into an additive manufacturing system;
depositing a powder into a chamber;
applying an energy source to the deposited powder; and
consolidating the powder into a cross-sectional shape corresponding to the defined configuration.

11. The method of claim 10 , wherein the powder comprises at least one of a metal powder, a ceramic powder and a composite powder.

12. The method of claim 10 , further comprising repeating the depositing, applying, and consolidating steps to construct the internally cooled blisk having the defined configuration.

13. An internally cooled blisk comprising:
a disk having a peripheral rim;
an annular array of blades spaced apart around the peripheral rim of the disk, each of said blades comprising an airfoil extending outwardly from the peripheral rim of the disk in a radial direction; and
a cooling fluid flow in fluid communication with cooling features comprising
one or more cooling plates,
one or more discrete branch structures in a web transition area where the disk meets each of the blades,
one or more cooling channels within the blades,
one or more passages defined on a downstream side of the disk and an effusion blade surface defined on one or more of the blades;

wherein the disk and the annular array of blades are integrally formed as a single component; and
wherein the cooling fluid flow comprises having a first portion configured to flow from an input, to the one or more cooling channels within the blades and exiting the effusion blade surface and having a second portion of the cooling fluid flow bypassing the one or more cooling channels to the one or more passages via the one or more discrete branch structures in the web transition area.

14. The internally cooled blisk of claim 13 , wherein the disk and the annular array of blades comprise a powder consolidated into an integral structure having defined therein the one or more cooling fluid flow passages by an additive manufacturing process.

15. The internally cooled blisk of claim 14 , wherein the powder comprises at least one of a metal powder, a ceramic powder and a composite powder.

16. The internally cooled blisk of claim 15 , wherein the metal powder comprises a nickel-based or cobalt-based superalloy.

17. The internally cooled blisk of claim 13 , wherein the internally cooled blisk is not axisymmetric.

Assignees

• Gen Electric

Inventors

• Kenyon Ross Hartley
• Joshi Narendra Digamber

Classifications

• B22F10/28

  Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title

• F05D2230/22

  by sintering · CPC title

• F05D2300/175

  Superalloys · CPC title

• F05D2230/31

  Layer deposition · CPC title

• B23K2203/26

  Operations & Transport · mapped topic