Methods utilizing cold spray techniques for repairing and protecting rotary components of aviation propulsion systems

Patent metadata

Field	Value
Publication number	US-9394063-B2
Application number	US-201313840396-A
Country	US
Kind code	B2
Filing date	Mar 15, 2013
Priority date	Mar 15, 2013
Publication date	Jul 19, 2016
Grant date	Jul 19, 2016

Abstract

A method of repairing a component comprises identifying a non-compliant surface of the component, wherein the non-compliant surface is not within an allowable tolerance, cold spraying a powder comprising a metal onto the non-compliant surface, and forming a coating comprising the metal over the non-compliant surface, wherein an outer surface of the coating is within an allowable tolerance. In an embodiment, the method of repairing an outer component further comprises machining the outer surface of the coating. In an embodiment, the component is a shaft, a rotor mast, an input quill, or a bearing. In an embodiment, the component contains electronic equipment during the cold spraying, and wherein the cold spraying does not damage the electronic equipment. In an embodiment, the component is repaired without subjecting the component to a hydrogen embrittlement bake.

First claim

What is claimed is:

1. A method, comprising:
identifying a non-compliant surface of a component, the component comprising temperature sensitive material and at least one of electronic equipment, optical equipment, or fluid sensing devices, wherein the non-compliant surface is not within an allowable tolerance;
cold spraying a powder comprising a metal onto the non-compliant surface, wherein the cold spraying comprises restricting heat to the non-compliant surface and avoiding one or more undamaged portions of the component by masking off one or more portions of the non-compliant surface from the undamaged portions of the component with a thermally insulating masking material, wherein the cold spraying does not damage the electronic equipment, the optical equipment, or the fluid sensing devices;
localizing heat generated by the cold spraying away from the temperature sensitive material; and
forming a coating comprising the metal over the non-compliant surface, wherein an outer surface of the coating is within an allowable tolerance.

2. The method of claim 1 , wherein the non-compliant surface is not within the allowable tolerance because of surface wear, fretting, fabrication error, an accident during transport, assembly, disassembly, or repair of the component, or any combination thereof.

3. The method of claim 1 , wherein the cold spraying comprises spraying a mixture of a gas and the powder comprising the metal at a temperature of less than 1300° F. onto the noncompliant surface.

4. The method of claim 3 , wherein the cold spraying further comprises spraying a mixture of a gas and the powder comprising metal at temperatures of less than 1000° F. onto the non-compliant surface.

5. The method of claim 1 , wherein the component is repaired without subjecting the component to a hydrogen embrittlement bake.

6. The method of claim 1 , wherein the metal comprises stainless steel.

7. The method of claim 1 , wherein the metal is substantially the same material as the component.

8. The method of claim 1 , wherein the component is a rotor mast.

9. The method of claim 1 , wherein the component is an aircraft component.

10. The method of claim 1 , further comprising machining the outer surface of the coating.

11. The method of claim 1 , wherein the cold spraying comprises substantially limiting application of the cold spray to areas defined by the non-compliant surface.

12. The method of claim 1 , wherein a design tolerance of the component is ± about 3×10−4 inches.

13. A method, comprising:
cold spraying a powder comprising a metal onto an undamaged portion of a component, wherein the cold spraying comprises restricting heat to the undamaged portion and avoiding other portions of the component by masking off the undamaged portion from the other portions of the component with a thermally insulating masking material, the component comprising temperature sensitive material and at least one of electronic equipment, optical equipment, or fluid sensing devices, wherein the cold spraying does not damage the electronic equipment, the optical equipment, or the fluid sensing devices;
localizing heat generated by the cold spraying away from the temperature sensitive material; and
forming a coating comprising the metal over the undamaged portion of the component.

14. The method of claim 13 , wherein the component is a rotor mast.

15. The method of claim 13 , wherein the coating comprises an anti-corrosion coating.

16. The method of claim 13 , wherein the coating comprises chrome, stainless steel, or combinations thereof.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Jackson Kenneth Myron
• Riley Walter West

Classifications

• B64D33/00

  Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for · CPC title

• Y10T29/49746

  by applying fluent material, e.g., coating, casting · CPC title

• Y10T428/12063

  Nonparticulate metal component · CPC title

• B64D2045/009

  Fire detection or protection; Erosion protection, e.g. from airborne particles · CPC title

• B32B15/011 Primary

  all layers being formed of iron alloys or steels · CPC title