Additive layer repair of a metallic component

Patent metadata

Field	Value
Publication number	US-10487659-B2
Application number	US-201615154474-A
Country	US
Kind code	B2
Filing date	May 13, 2016
Priority date	May 21, 2015
Publication date	Nov 26, 2019
Grant date	Nov 26, 2019

Abstract

A method of repairing a metallic component (formed from a first material) by powder feeding laser deposition, comprises the step of depositing a plurality of first repair layers onto a repair surface of the component to form a first repair zone, the first of the plurality of first repair layers comprising a mixture of A/B by weight of the first material and a second material, each nth successive one of the plurality of first repair layers comprising a change in the proportion of the second material in the mixture, the last of the plurality of first repair layers comprising a mixture of C/D by weight of the first material and the second material.

First claim

What is claimed is:

1. A method of repairing a metallic component by powder feeding laser deposition, the metallic component being formed from a first material, the method comprising depositing a plurality of first repair layers onto a repair surface of the component to form a first repair zone, the first of the plurality of first repair layers comprising a mixture of A/B by weight of the first material and a second material, each n th successive one of the plurality of first repair layers comprising a change in the proportion of the second material in the mixture, the last of the plurality of first repair layers comprising a mixture of C/D by weight of the first material and the second material,
wherein the first material consists of at least one selected from the group consisting of a titanium alloy, a nickel alloy, a special steel and an aluminum alloy,
the first material is provided as a powder having a first mean particle size, and the second material is provided as a powder having a second mean particle size,
a distribution of the first mean particle size and the second mean particle size varies across the first repair zone in a thickness direction,
if the first mean particle size is smaller than the second mean particle size, then, for the same volume of material, a time required to melt the first material will be less than a time required to melt the second material, and
if the second mean particle size is smaller than the first mean particle size, then, for the same volume of material, the time required to melt the second material will be less than the time required to melt the first material.

2. The method as claimed in claim 1 , wherein the integer ‘n’ is in a range of 10 to 1,000.

3. The method as claimed in claim 1 , wherein a ratio A/B is in a range of 80/20 to 5/95.

4. The method as claimed in claim 1 , wherein a ratio C/D is in a range of 0/100 to 40/60.

5. The method as claimed in claim 1 , wherein the change in the proportion of the second material in the mixture comprises an increase in the proportion of the second material in the mixture.

6. The method as claimed in claim 1 , the method further comprising depositing a plurality of second repair layers of the second material onto the first repair zone to form a second repair zone.

7. The method as claimed in claim 6 , the method further comprising depositing a plurality of third repair layers of a third material onto the second repair zone to form a third repair zone.

8. The method as claimed in claim 7 , wherein the third material is metallurgically compatible with both the first material and the second material.

9. The method as claimed in claim 7 , wherein if the second mean particle size is smaller than the third mean particle size, then, for the same volume of material, the time required to melt the second material will be less than the time required to melt the third material, and
if the third mean particle size is smaller than the second mean particle size, then, for the same volume of material, the time required to melt the third material will be less than the time required to melt the second material.

10. The method as claimed in claim 1 , wherein the first material and the second material have the same metallurgical composition.

11. A method of repairing a metallic component by powder feeding laser deposition, the metallic component being formed from a first material, the method comprising:
depositing a plurality of second repair layers of a second material onto a repair surface of a first repair zone of the component to form a second repair zone; and
depositing a plurality of third repair layers of a third material onto the second repair zone to form a third repair zone,
wherein the first material consists of at least one selected from the group consisting of a titanium alloy, a nickel alloy, a special steel and an aluminum alloy,
the first material is provided as a powder having a first mean particle size, and the second material is provided as a powder having a second mean particle size,
a distribution of the first mean particle size and the second mean particle size varies across the first repair zone in a thickness direction,
if the first mean particle size is smaller than the second mean particle size, then, for the same volume of material, a time required to melt the first material will be less than a time required to melt the second material, and
if the second mean particle size is smaller than the first mean particle size, then, for the same volume of material, the time required to melt the second material will be less than the time required to melt the first material.

12. A metallic component comprising:
a base region formed from a first material; and
a first repair zone superposed on the base region, the first repair zone being formed from a plurality of first repair layers, the first of the plurality of first repair layers comprising a mixture of A/B by weight of the first material and a second material, each n th successive one of the plurality of first repair layers comprising a change in the proportion of the second material in the mixture, the last of the plurality of first repair layers comprising a mixture of C/D by weight of the first material and the second material,
wherein the first material consists of at least one selected from the group consisting of a titanium alloy, a nickel alloy, a special steel and an aluminum alloy,
the first material is provided as a powder having a first mean particle size, and the second material is provided as a powder having a second mean particle size,
a distribution of the first mean particle size and the second mean particle size varies across the first repair zone in a thickness direction,
if the first mean particle size is smaller than the second mean particle size, then, for the same volume of material, a time required to melt the first material will be less than a time required to melt the second material, and
if the second mean particle size is smaller than the first mean particle size, then, for the same volume of material, the time required to melt the second material will be less than the time required to melt the first material.

13. The metallic component as claimed in claim 12 , wherein the integer ‘n’ is in a range of 10 to 1,000.

14. The metallic component as claimed in claim 12 , wherein a ratio A/B is in a range of 80/20 to 5/95.

15. The metallic component as claimed in claim 12 , wherein a ratio C/D is in a range of 0/100 to 40/60.

16. The metallic component as claimed in claim 12 , wherein the change in the proportion of the second material in the mixture comprises an increase in the proportion of the second material in the mixture.

17. The metallic component as claimed in claim 12 , further comprising a second repair zone superposed on the first repair zone, the second repair zone comprising a plurality of second repair layers of the second material.

18. The metallic component as claimed in claim 17 , further comprising a third repair zone superposed on the second repair zone, the third repair zone comprising a plurality of third repair layers of a third material.

Assignees

• Rolls Royce Plc

Inventors

• Heason Christopher P
• Baxter Gavin J

Classifications

• B22F10/25

  Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS] · CPC title

• B23P6/007 Primary

  using only additive methods, e.g. build-up welding · CPC title

• B23K26/144

  the fluid stream containing particles, e.g. powder · CPC title

• F05D2230/80

  Repairing, retrofitting or upgrading methods · CPC title

• B23K2101/001

  Turbines · CPC title