Nickel-based solder alloy

Patent metadata

Field	Value
Publication number	US-9346131-B2
Application number	US-201113808053-A
Country	US
Kind code	B2
Filing date	Jun 16, 2011
Priority date	Jul 3, 2010
Publication date	May 24, 2016
Grant date	May 24, 2016

Abstract

Solder alloy based on nickel is composed of a mixture with a first soldering material, a second soldering material, and a base material, wherein the base material is a nickel-based material which corresponds to the material to be soldered and is present in a proportion of 45-70% by weight in the mixture, the first soldering material is a nickel-based material including chromium, cobalt, tantalum, aluminum and boron, and is present in a proportion of 15-30% by weight in the mixture, and the second soldering material is a nickel-based material including chromium, cobalt, molybdenum, tungsten, boron and hafnium, and is present in a proportion of 15-25% by weight in the mixture.

First claim

The invention claimed is:

1. Method for producing a solder alloy for soldering a component made of a nickel-based material in which nickel is the largest alloy component by weight, the method comprising the following steps:
providing three components composed of a first soldering material, a second soldering material, and a base material, wherein
the base material is a nickel-based powder material, which has the same composition as the nickel-based material of the component to be soldered and is present in a proportion of 45-70% by weight in the total weight of the three components,
the first soldering material is a nickel-based powder material which has nickel as the largest alloy component by weight and further comprises chromium, cobalt, tantalum, aluminum and boron and is present in a proportion of 15-30% by weight in the total weight of the three components, and
the second soldering material is a nickel-based powder material which has nickel as the largest alloy component by weight and further comprises chromium, cobalt, molybdenum, tungsten, boron and hafnium and is present in a proportion of 15-25% by weight in the total weight of the three components,
wherein both the chromium content and also the cobalt content are higher in the case of the first soldering material than in the case of the second soldering material, and

mixing together the base material powder, the first soldering material powder and the second soldering material powder, thereby forming the solder alloy in a powder form.

2. Method according to claim 1 , further comprising the step of using the solder alloy for soldering the component to be soldered when the solder alloy is in the form of a powder.

3. Method according to claim 1 , further comprising the following steps:
forming a paste using the solder alloy in powder form; and
using the solder alloy for soldering the component to be soldered when the solder alloy is in the form of the paste.

4. The method of claim 1 , further comprising the step of using the solder alloy to repair the component to be repaired, wherein the component to be soldered is a gas turbine-component.

5. The method of claim 4 , wherein the gas turbine component is an airplane engine component.

6. The method of claim 1 , wherein the nickel-based alloy of the component to be soldered is a nickel-based superalloy and the base material is a powder of the same nickel-based superalloy.

7. The method of claim 1 , wherein the first soldering material has a composition of 14% by weight of chromium, 10% by weight of cobalt, 2.75% by weight of tantalum, 3.5% by weight of aluminum, 2.75% by weight of boron and 0.1% by weight of yttrium and nickel as the remainder.

8. The method of claim 1 , wherein the second soldering material has a composition of 2.9% by weight of chromium, 5.5% by weight of cobalt, 1.1% by weight of molybdenum, 7.4% by weight of tungsten, 0.3% by weight of niobium, 0.8% by weight of aluminum, 2.9% by weight of boron, 3% by weight of hafnium, 1.1% by weight of palladium and nickel as the remainder.

Assignees

• Waltemathe Markus
• Seidel Frank
• Rösing Jürgen
• Krappitz Harald
• MTU Aero Engines AG

Inventors

• Waltemathe Markus
• Seidel Frank
• Rösing Jürgen
• Krappitz Harald

Classifications

• B23K35/304

  with Cr as the next major constituent · CPC title

• B23K2201/001

  Operations & Transport · mapped topic

• C22C1/02

  by melting {(C22C1/1036 takes precedence)} · CPC title

• B23K35/3033 Primary

  Ni as the principal constituent · CPC title

• F05B2230/238

  Soldering · CPC title