Method and apparatus for repairing gas turbine components made of ceramic composite materials

Patent metadata

Field	Value
Publication number	US-9527170-B2
Application number	US-201113811597-A
Country	US
Kind code	B2
Filing date	Jul 14, 2011
Priority date	Jul 20, 2010
Publication date	Dec 27, 2016
Grant date	Dec 27, 2016

Abstract

Method for repairing a gas turbine component, which at least at the spot to be repaired consists of a ceramic composite material, where an energy beam locally heats the gas turbine component in a zone, and where one or more auxiliary materials and optionally fibers and/or particles are fed to this zone, wherein a ceramic is generated in the melting zone through the one or more auxiliary materials, and, optionally, the one or more auxiliary materials together with the fibers and/or particles forms a ceramic composite material.

First claim

The invention claimed is:

1. A method for repairing a gas turbine component, comprising:
heating a portion of a gas turbine component via an energy beam in a melting zone,
wherein the energy beam is directed onto a surface of the portion of the gas turbine component,
wherein a base material of the gas turbine component, at least at a spot to be repaired, comprises:
a first ceramic composite material,

wherein the spot to be repaired is in the melting zone;
feeding one or more auxiliary materials to the melting zone,
wherein a ceramic is generated, at least at the spot to be repaired, in the melting zone from the one or more auxiliary materials,
wherein the one or more auxiliary materials completely or partially react to generate the ceramic in a chemical reaction in the melting zone; and
feeding fibers and/or particles to the melting zone,
wherein a second ceramic composite material is generated in the melting zone from the one or more auxiliary materials and the fibers and/or particles,
wherein the second ceramic composite material is in contact with the base material of the gas turbine component, at least at the spot to be repaired.

2. The method according to claim 1 ,
wherein the one or more auxiliary materials comprise a metal and a non-metal, and
wherein the metal and the non-metal react in the chemical reaction to generate the ceramic.

3. The method according to claim 2 ,
wherein a proportion of the metal is higher than a proportion of the non-metal.

4. The method according to claim 3 ,
wherein the proportion of the metal is 20% to 40% higher than the proportion of the non-metal.

5. The method according to claim 1 ,
wherein the first ceramic composite material comprises a first ceramic, and
wherein the first ceramic is the same as the ceramic.

6. The method according to claim 1 ,
wherein the second ceramic composite material is the same as the first ceramic composite material.

7. The method according to claim 1 ,
wherein feeding the one or more auxiliary materials to the melting zone comprises pre-depositing the one or more auxiliary materials to the melting zone.

8. The method according to claim 1 ,
wherein feeding the fibers and/or the particles to the melting zone comprises pre-depositing the fibers and/or the particles to the melting zone.

9. The method according to claim 1 ,
wherein feeding the one or more auxiliary materials to the melting zone comprises feeding the one or more auxiliary materials to the melting zone via one or more feeders.

10. The method according to claim 1 ,
wherein feeding the fiber and/or the particles to the melting zone comprises feeding the fiber and/or the particles to the melting zone via one or more feeders.

11. The method according to claim 1 ,
wherein the energy beam is a laser beam.

12. The method according to claim 1 ,
wherein the energy beam is an electron beam.

13. The method according to claim 1 ,
wherein the energy beam is an induction field.

14. The method according to claim 1 ,
wherein feeding the one or more auxiliary materials to the melting zone comprises feeding the one or more auxiliary materials to the melting zone via a flux cored wire.

15. The method according to claim 1 ,
wherein feeding the one or more auxiliary materials and the fibers and/or the particles to the melting zone comprises feeding the one or more auxiliary materials and the fibers and/or the particles to the melting zone via a flux cored wire.

16. The method according to claim 15 ,
wherein the flux cored wire comprises an outer sheath, wherein the outer sheath encloses an interior.

17. The method according to claim 16 ,
wherein a material of the outer sheath comprises at least a first portion of the one or more auxiliary materials.

18. The method according to claim 17 ,
wherein at least a second portion of the one or more auxiliary materials is located in the interior.

19. The method according to claim 16 ,
wherein at least a portion of the fibers and/or the particles is located in the interior.

20. The method according to claim 16 ,
wherein a gas stream is provided in the interior.

21. The method according to claim 1 ,
wherein the base material of the gas turbine component, at least at the spot to be repaired, is the first ceramic composite material.

22. The method according to claim 1 ,
wherein the second ceramic composite material adjoins to the base material of the gas turbine component, at least at the spot to be repaired.

23. The method according to claim 1 , wherein the one or more auxiliary materials comprise a material that is the same as the ceramic.

Assignees

• Czerner Stefan
• Lufthansa Technik Ag

Inventors

• Czerner Stefan

Classifications

• B23K26/34

  Laser welding for purposes other than joining · CPC title

• Y10T29/49318

  Repairing or disassembling · CPC title

• B23K2203/50

  Operations & Transport · mapped topic

• B23K2203/16

  Operations & Transport · mapped topic

• F01D5/005

  Repairing methods or devices · CPC title