Turbine component, turbine blade, and turbine component fabrication process

Patent metadata

Field	Value
Publication number	US-9664052-B2
Application number	US-201213633928-A
Country	US
Kind code	B2
Filing date	Oct 3, 2012
Priority date	Oct 3, 2012
Publication date	May 30, 2017
Grant date	May 30, 2017

Abstract

A turbine component, a turbine blade, and a turbine component fabrication process are disclosed. The turbine component includes ceramic matrix composite plies and a feature configured for preventing interlaminar tension of the ceramic matrix composite plies. The feature is selected from the group consisting of ceramic matrix composite tows or precast insert tows extending through at least a portion of the ceramic matrix composite plies, a woven fabric having fiber tows or a precast insert preventing contact between a first set of the ceramic matrix composite plies and a second set of the ceramic matrix composite plies, and combinations thereof. The process includes laying up ceramic matrix composite plies in a preselected arrangement and securing a feature configured for interlaminar tension.

First claim

What is claimed is:

1. A turbine component, comprising:
a first set of ceramic matrix composite plies forming at least a portion of a first side of the turbine component;
a second set of ceramic matrix composite plies forming at least a portion of a second side of the turbine component opposite the first side; and
a woven fabric having fiber tows preventing contact between the first set of ceramic matrix composite plies and the second set of ceramic matrix composite plies;
wherein the woven fabric having fiber tows includes mechanically interlocking stitches running through a thickness of fabric layers of the woven fabric to tie the fabric layers together and provide enhanced interlaminar strength to the woven fabric and the fiber tows mechanically interlock in the woven fabric.

2. The turbine component of claim 1 , wherein the turbine component comprises a turbine blade, the turbine blade comprising an internal cavity, wherein the woven fabric forms a border of the internal cavity below a root of the turbine blade.

3. The turbine component of claim 1 , wherein the ceramic matrix composite plies include silicon carbide.

4. The turbine component of claim 1 , further comprising an environmental barrier coating positioned on the ceramic matrix composite plies.

5. The turbine component of claim 1 , wherein the woven fabric having fiber tows prevents contact between the first set of the ceramic matrix composite plies and the second set of the ceramic matrix composite plies at an edge of the turbine component to prevent interlaminar tension between the first set and the second set of ceramic matrix composite plies.

6. The turbine component of claim 1 further comprising a plurality of ceramic matrix composite tows extending in a transverse direction with respect to the ceramic matrix composite plies from and through at least a portion of the first set of ceramic matrix composite plies to and through at least a portion of the second set of ceramic matrix composite plies, the plurality of ceramic matrix composite tows serving as a transverse boundary to prevent interlaminar tension between the first set and the second set of ceramic matrix composite plies.

7. The turbine component of claim 1 further comprising a plurality of precast insert tows extending in a transverse direction with respect to the ceramic matrix composite plies from and through at least a portion of the first set of ceramic matrix composite plies to and through at least a portion of the second set of ceramic matrix composite plies, the plurality of precast insert tows serving as a transverse boundary to prevent interlaminar tension between the first set and the second set of ceramic matrix composite plies.

8. A turbine component fabrication process, comprising:
laying up a first set of ceramic matrix composite plies in a first preselected arrangement and a second set of ceramic matrix composite plies in a second preselected arrangement; and
securing a plurality of ceramic matrix composite tows extending in a transverse direction with respect to the ceramic matrix composite plies from and through at least a portion of the first set of ceramic matrix composite plies to and through at least a portion of the second set of ceramic matrix composite plies, the plurality of ceramic matrix composite tows serving as a transverse boundary to prevent interlaminar tension between the first set and the second set of ceramic matrix composite plies;
wherein the first set of ceramic matrix composite plies forms at least a portion of a first side of the turbine component and the second set of ceramic matrix composite plies forms at least a portion of a second side of the turbine component opposite the first side.

9. The turbine component fabrication process of claim 8 , wherein the turbine component is a turbine blade, wherein the first side comprises a suction skin of the turbine blade and the second side comprises a pressure skin of the turbine blade.

10. The turbine component fabrication process of claim 9 , wherein the ceramic matrix composite tows are positioned in a neck of the turbine blade.

11. The turbine component fabrication process of claim 9 , wherein the turbine blade is solid.

12. The turbine component fabrication process of claim 8 , further comprising rigidizing and densifying the ceramic matrix composite plies.

13. The turbine component fabrication process of claim 8 further comprising preventing contact between the first set of ceramic matrix composite plies and the second set of ceramic matrix composite plies with a precast insert.

14. A turbine component, comprising:
a first set of ceramic matrix composite plies forming at least a portion of a first side of the turbine component;
a second set of ceramic matrix composite plies forming at least a portion of a second side of the turbine component opposite the first side;
a plurality of precast insert tows extending in a transverse direction with respect to the ceramic matrix composite plies from and through at least a portion of the first set of ceramic matrix composite plies to and through at least a portion of the second set of ceramic matrix composite plies, the plurality of precast insert tows serving as a transverse boundary to prevent interlaminar tension between the first set and the second set of ceramic matrix composite plies.

15. The turbine component of claim 14 , wherein the precast insert tows mechanically interlock with the portion of the first set of ceramic matrix composite plies and the portion of the second set of ceramic matrix composite plies.

16. The turbine component of claim 14 further comprising a precast insert preventing contact between the first set of ceramic matrix composite plies and the second set of ceramic matrix composite plies.

17. The turbine component of claim 16 , wherein the precast insert is a precast monolithic ceramic or whisker ceramic fiber-reinforced ceramic.

18. The turbine component of claim 14 , wherein the turbine component comprises a turbine blade, wherein the first side comprises a suction skin of the turbine blade and the second side comprises a pressure skin of the turbine blade.

19. The turbine component of claim 18 , wherein the suction skin and the pressure skin are positioned in a radial orientation to reduce an out of plane load vector.

Assignees

• Gen Electric

Inventors

• Delvaux John Mcconnell
• Cairo Ronald Ralph
• Parolini Jason Robert

Classifications

• F05D2300/6012

  Woven fabrics · CPC title

• F05D2220/30

  in turbines · CPC title

• F01D5/282 Primary

  Selecting composite materials, e.g. blades with reinforcing filaments · CPC title

• F01D5/288

  Protective coatings for blades · CPC title

• F05D2300/6033

  Ceramic matrix composites [CMC] · CPC title