Electrospark deposition process for oxidation resistant coating of cooling hole

Patent metadata

Field	Value
Publication number	US-9789557-B2
Application number	US-201514816527-A
Country	US
Kind code	B2
Filing date	Aug 3, 2015
Priority date	Aug 14, 2012
Publication date	Oct 17, 2017
Grant date	Oct 17, 2017

Abstract

A method of providing an oxidation resistant coating is disclosed. The method includes providing a substrate having a first surface and cooling holes. A portable coating device includes electro-spark deposition (ESD) equipment and an ESD torch connected with the ESD equipment. The ESD torch has an inert gas source and a rotary electrode conductive material. The rotary electrode is positioned within the ESD torch, and is shielded by an inert gas. The rotary electrode applies a compositionally controlled protective coating to the first surface of the substrate. Then the rotary electrode is inserted into the cooling hole and generates an electrospark between rotary ESD electrode and the substrate to form a rounded edge and deposit a coating of electrode material alloy at a cooling hole edge.

First claim

What is claimed is:

1. A method for providing a coating comprising:
providing a substrate having a first surface and at least one cooling hole formed in the first surface;
providing a portable coating device including:
electro-spark deposition (ESD) equipment, and
an ESD torch electrically connected with the ESD equipment, the ESD torch including:
an inert gas source; and
a rotary electrode including a conductive material, the rotary electrode disposed within the ESD torch, the rotary electrode shielded by an inert gas, wherein rotary electrode applies a compositionally controlled protective coating to the first surface of the substrate;

inserting the rotary electrode at least partially into the cooling hole;
generating an electrospark between the rotary ESD electrode and the substrate to only form a rounded edge as a result of deformation of material from the substrate at an edge of the cooling hole and deposit a coating of electrode material alloy having a thickness of 3 mils or less over the rounded edge.

2. The method of claim 1 , further comprising pressing the rotary electrode into contact with the substrate in the at least one cooling hole.

3. The method of claim 1 , wherein the step of inserting the rotary electrode further comprises inserting a tip portion of the rotary electrode into the at least one cooling hole.

4. The method of claim 3 , further comprising providing a transition portion on the tip portion, the transition portion transitioning from a diameter of the rotary electrode larger than a diameter of the at least one cooling hole to a tip portion having a diameter less than the diameter of the at least one cooling hole to permit partial insertion of tip portion.

5. The method of claim 4 , wherein the transition portion comprises a geometry for forming the cooling hole edge.

6. The method of claim 5 , wherein the geometry is a rounded edge.

7. The method of claim 1 , further comprising providing an inert gas curtain around a deposition site at the cooling hole edge by directing a first shielding gas flow at the rotary electrode.

8. The method of claim 1 , further comprising providing a second shielding gas flow at the rotary electrode from a bottom surface of the substrate.

9. The method of claim 1 , further comprising applying force to the rotary electrode to make contact with the substrate in the at least one cooling hole.

10. The method of claim 1 , further comprising forming a metallurgical bond between the substrate and the alloyed coating on an exit edge of the at least one cooling hole.

Assignees

• Gen Electric

Inventors

• Lin Dechao
• Ucok Ibrahim
• Onal Kivilcim

Classifications

• F01D5/185

  Liquid cooling (F01D5/181 takes precedence) · CPC title

• F05D2230/90

  Coating; Surface treatment · CPC title

• F05D2260/202

  by film cooling · CPC title

• B23K9/04 Primary

  Welding for other purposes than joining, e.g. built-up welding · CPC title

• F01D9/023

  Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings · CPC title