Dual-walled ceramic matrix composite (CMC) component with integral cooling and method of making a CMC component with integral cooling

Patent metadata

Field	Value
Publication number	US-9896954-B2
Application number	US-201514881864-A
Country	US
Kind code	B2
Filing date	Oct 13, 2015
Priority date	Oct 14, 2014
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

A dual-walled ceramic matrix composite (CMC) component comprises: a CMC core having a hollow shape enclosing at least one interior channel; and a CMC outer layer overlying and spaced apart from the CMC core by a ceramic slurry-cast architecture positioned therebetween. Each of the CMC core and the CMC outer layer comprises ceramic fibers in a ceramic matrix. The CMC core further includes a plurality of through-thickness inner cooling holes in fluid communication with the at least one interior channel. The ceramic slurry-cast architecture defines a cooling fluid path over an outer surface of the CMC core that connects the interior channel(s) to an external environment of the dual-walled CMC component. The CMC outer layer may also include a plurality of through-thickness outer cooling holes in fluid communication with the cooling fluid path, thereby extending the cooling fluid path through the CMC outer layer.

First claim

The invention claimed is:

1. A method of forming a CMC component with integral cooling, the method comprising:
positioning a preform comprising a rigidized framework of ceramic fibers within a mold having an inner surface comprising a plurality of protrusions, the preform having a hollow shape enclosing at least one interior channel;
introducing into the mold a slurry comprising particulate solids in a flowable carrier, the slurry (a) infiltrating the rigidized framework of ceramic fibers and (b) flowing over an outer surface of the preform and around the plurality of protrusions;
removing the flowable carrier from the slurry, the particulate solids (a) remaining in the rigidized framework of ceramic fibers and (b) being deposited on the outer surface of the preform between the protrusions, thereby forming a porous slurry-cast architecture on the outer surface of the preform;
removing the mold;
forming a plurality of through-thickness cooling holes in the preform, the cooling holes forming a flow path from the at least one interior channel through the porous slurry-cast architecture and out of the preform.

2. The method of claim 1 , further comprising, after removing the mold, infiltrating the preform with a molten material, thereby forming a CMC core.

3. The method of claim 1 , wherein the porous slurry-cast architecture comprises slurry-cast pedestal features separated by recessed regions defined by the protrusions of the mold.

4. The method of claim 1 , further comprising machining the porous slurry-cast architecture.

5. The method of claim 1 , further comprising, after removing the mold, bonding a ceramic outer layer to the preform.

6. The method of claim 5 , wherein the bonding comprises wrapping a prepreg tape around the porous slurry-cast architecture and then heating the prepreg tape.

7. The method of claim 5 , further comprising infiltrating the ceramic outer layer with a molten material, thereby forming a CMC outer layer.

8. The method of claim 7 , wherein infiltration of the preform and infiltration of the ceramic outer layer with a molten material are carried out simultaneously after the bonding, thereby forming a dual-walled CMC component comprising a CMC outer layer bonded to a CMC core.

9. The method of claim 8 , further comprising forming a plurality of through-thickness cooling holes in the CMC outer layer, thereby extending the flow path from the interior channel through the CMC outer layer.

10. The method of claim 1 , wherein infiltration of the preform and infiltration of a ceramic outer layer with a molten material are carried out separately to independently form a CMC core and a CMC outer layer.

11. The method of claim 10 , further comprising bonding the CMC outer layer to the CMC core, thereby forming a dual-walled CMC component.

12. The method of claim 11 , wherein the bonding comprises reactive brazing or diffusion bonding.

13. The method of claim 12 , further comprising forming a plurality of through-thickness cooling holes in the CMC outer layer, thereby extending the flow path from the interior channel through the CMC outer layer.

14. The method of claim 1 , wherein the introduction of the slurry into the mold comprises injection molding or gel-casting.

15. The method of claim 1 , wherein the CMC component comprises a blade or vane of a gas turbine engine.

Assignees

• Rolls Royce Corp

Inventors

• Walston Jeffrey A
• Landwehr Sean

Classifications

• F01D5/284

  Selection of ceramic materials · CPC title

• B32B5/26

  another layer {next to it} also being fibrous or filamentary {(relative arrangement of fibres or filaments of different layers B32B5/12)} · CPC title

• B32B2255/20

  Inorganic coating · CPC title

• B32B2581/00

  Seals; Sealing equipment; Gaskets · CPC title

• B32B2603/00

  Vanes, blades, propellers, rotors with blades · CPC title