Laser additive repairing of nickel base superalloy components

Patent metadata

Field	Value
Publication number	US-9527162-B2
Application number	US-201313891314-A
Country	US
Kind code	B2
Filing date	May 10, 2013
Priority date	Nov 7, 2011
Publication date	Dec 27, 2016
Grant date	Dec 27, 2016

Abstract

Ni base superalloy components containing relatively large amounts of Al and Ti are known to be difficult to build up by a weld build up process without cracking. As the Al and Ti content of the superalloy is increased to improve the strength, the susceptibility to cracking is increased. It is shown herein that reducing the γ′ phase in the additive built up material improves robustness against cracking. A stepwise, controlled heating and cooling process is described to be used in cooperation with an additive build up process to reduce the γ′ present and thereby reduce cracking.

First claim

What is claimed is:

1. A method of repair additive build up of a nickel (Ni) base superalloy with significant titanium (Ti) and aluminum (Al) content comprising:
a) preplacing a Ni base superalloy powder having significant Ti and Al content onto a substrate of the same composition as the Ni base superalloy powder;
b) preheating the preplaced powder to a temperature above 1200 deg. C. with a first heat source;
c) melting the preplaced powder with one or more passes of a directed energy beam second heat source so as to produce a heat affected zone having a width less than 100 microns, removing the second heat source when melting is completed;
d) performing a controlled step and hold cooling of the melted preplaced powder with the first heat source such that no more than 20 weight percent of γ′ phase is formed during the step and hold cooling.

2. A method as in claim 1 wherein the thickness of the additive build up is in the range from 1 millimeter to 10 millimeters.

3. A method as in claim 1 wherein the preplaced powder has a particle size in the range from 10 microns to 100 microns.

4. A method as in claim 1 wherein the superalloy of said nickel base superalloy is selected from the group consisting of: 713C, 247, PW1480, MARM200, R77, PW1483, R80, U720, 738 and mixtures thereof.

5. A method as in claim 1 wherein the controlled step and hold cooling from an initial temperature T 1 to room temperature consists of a plurality of steps:
a. Holding at T 1 for a time in the range from 1 min to 3 min;
b. Cooling to a temperature T 2 lower than T 1 and hold for a time in the range from 2 min to 15 min so as to produce less than 20 weight percent γ′ phase;
c. Cooling to a temperature T 3 lower than T 2 and hold for a time in the range from 2 min to 30 min so as to produce less than 20 weight percent γ′ phase;
d. Cooling to a temperature T 4 lower than T 3 and hold for a time in the range from 6 min to 120 min so as to produce less than 20 weight percent γ′ phase; and
e. Cooling to room temperature in a plurality of cooling steps from T 4 to room temperature wherein the temperature at each step is maintained from 1 hour to 20 hours, so as to produce less than 20 weight percent γ′.

6. A method of additive build up of a nickel (Ni) base superalloy with significant titanium (Ti) and aluminum (Al) content comprising:
a) placing a Ni base super alloy powder on a substrate of the same composition;
b) preheating the preplaced powder to a temperature above 1200 deg. C. with a first heat source;
c) melting the preplaced powder with one or more passes of a directed energy beam second heat source so as to produce a heat affected zone having a width less than 100 microns, removing the second heat source when melting is completed;
d) performing a controlled step and hold cooling of the melted preplaced powder with the first heat source such that no more than 20 weight percent of γ′ phase is formed during the step and hold cooling.

Assignees

• Ozbaysal Kazim
• Siemens Energy Inc

Inventors

• Ozbaysal Kazim

Classifications

• B22F12/46

  with translatory movement · CPC title

• B22F12/13

  to preheat the material · CPC title

• B22F10/32

  of the atmosphere, e.g. composition or pressure in a building chamber · CPC title

• B22F10/25

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

• B23K35/3033

  Ni as the principal constituent · CPC title