Repair process
AssigneeUnited Technologies Corporation
InventorMonika D. Kinstler
Life of this patent
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Abstract
In accordance with the present invention, a process for repairing metal workpieces, such as turbine engine components, is provided. The process comprises the steps of forming a braze paste containing a first nickel base alloy material containing boron and chromium and a second nickel base alloy material containing chromium and cobalt, applying the brazing paste to an area of the metal workpiece containing at least one crack, and subjecting the workpiece and the brazing paste to a brazing cycle by heating the brazing paste and the workpiece, preferably to a temperature in the range of from 2000 to 2200 degrees Fahrenheit. During the brazing cycle, the brazing paste flows into and fills the at least one crack and thus repairs the metal workpiece.
Claims11
A process for repairing at least one crack in a metal workpiece comprising the steps of:
- forming a braze paste containing a first nickel base alloy material containing boron and chromium and a second nickel base alloy material containing chromium and cobalt;
- applying said brazing paste to an area of said metal workpiece containing said at least one crack;
- subjecting said brazing paste and said workpiece to a brazing cycle by heating said brazing paste and said workpiece;
- and
- wherein said braze paste forming step comprises mixing a first nickel base alloy material consisting from 14 wt % to 16 wt % chromium, from 2.4 wt % to 3.0 wt % boron, up to 0.15 wt % total other elements, and the remainder nickel and inevitable impurities and a second nickel base alloy material consisting of from 22 wt % to 23 wt % chromium, from 18.5 wt % to 19.5 wt % cobalt, from 3.5 to 4.0 wt % titanium, from 1.8 wt % to 2.2 wt % tungsten, from 1.7 wt % to 2.0 wt % aluminum, from 1.2 wt % to 1.5 wt % tantalum, from 0.8 wt % to 1.2 wt % niobium, from 0.13 wt % to 0.17 wt % carbon, up to 0.2 wt % manganese, up to 0.015 wt % phosphorous, up to 0.10 wt % copper, up to 0.25 wt % iron, up to 0.10 wt % silicon, up to 0.04 wt % zirconium, from 0.001 wt % to 0.008 wt % boron, up to 0.005 wt % sulfur, up to 0.005 wt % nitrogen, up to 0.003 wt % oxygen, up to 0.0005 wt % silver, up to 0.0005 wt % lead, up to 0.00005 wt % selenium, up to 0.00003 wt % bismuth, up to 0.00005 wt % tellurium, up to 0.00005 wt % thallium, and the balance nickel and inevitable impurities.
A process for repairing at least one crack in a metal workpiece comprising the steps of:
- forming a braze paste containing a first nickel base alloy material containing boron and chromium and a second nickel base alloy material containing chromium and cobalt;
- applying said brazing paste to an area of said metal workpiece containing said at least one crack;
- subjecting said brazing paste and said workpiece to a brazing cycle by heating said brazing paste and said workpiece;
- and
- wherein said braze paste forming step comprises mixing a first nickel base alloy material consisting from 14 wt % to 16 wt % chromium, from 2.4 wt % to 3.0 wt % boron, up to 0.15 wt % total other elements, and the remainder nickel and inevitable impurities and a second nickel base alloy material consisting of from 22 wt % to 23 wt % chromium, from 18.5 wt % to 19.5 wt % cobalt, from 3.5 to 4.0 wt % titanium, from 1.8 wt % to 2.2 wt % tungsten, from 1.7 wt % to 2.0 wt % aluminum, from 1.2 wt % to 1.5 wt % tantalum, from 0.8 wt % to 1.2 wt % niobium, from 0.13 wt % to 0.17 wt % carbon, and the balance nickel and inevitable impurities.
Dependencies are inferred from the claim text.