Solder alloy and method for repairing a part

Publication: EP1970156A1
Published: 2008-09-17
Family Size: 1
Granted: No

Simple SummaryContent extracted from patent full text and abstract with AI.

This patent describes a specialized solder alloy based primarily on nickel and containing gallium and/or germanium as essential elements. The alloy is designed for repairing metallic components, particularly those made from nickel or cobalt-based superalloys, often used in high-temperature environments like turbine blades and combustion chambers. The repair process uses the solder alloy at a minimum temperature of about 1140°C, efficiently filling cracks or voids without melting or harming the base material.

Use CasesContent extracted from patent full text and abstract with AI.

  • Repairing cracks or voids in turbine blades for gas or steam turbines.
  • Refurbishing combustion chamber elements in power plant or aerospace applications.
  • Maintenance and repair of nickel- or cobalt-based superalloy components exposed to high thermal stress.
  • Restoration of worn or damaged surfaces on industrial engine or aircraft engine components.
  • Metal joining in situations where high strength and compatibility with superalloys is required.

BenefitsContent extracted from patent full text and abstract with AI.

  • Allows high-strength repairs at temperatures lower than the melting point of base components, reducing the risk of damage.
  • Enhanced suitability for high-temperature superalloys, making it ideal for critical engine or turbine parts.
  • Avoids use of boron, silicon, and zirconium, reducing risk of undesirable phases and improving joint quality.
  • Supports both isothermal and temperature gradient soldering processes, increasing flexibility for different repair strategies.
  • Enables repair of both directionally solidified and single-crystal components, maintaining structural integrity in advanced engine parts.

Technical Classifications (CPCs)

Main Classifications

Chemistry & Materials Science

Manufacturing & Transport

Sub Classifications

Machine Tools & Metal-Working

Metallurgy & Alloys (Non-Ferrous)

CPC Codes

B23K35/3033C22C19/00C22C19/007

Inventors & Applicants

Applicants

Siemens Ag

Mtu Aero Engines Gmbh

Patent Abstract

Solder alloys comprise gallium and/or germanium, the remainder being nickel : An independent claim is included for a method for repairing components (1) using solder alloys (10) as described at a minimum temperature of 1140[deg] C, especially a minimum temperature of 1160[deg] C.

Key Information

Publication No.

EP1970156A1

Family ID

38180695

Publication Date

2008-09-17

Application No.

EP07005303A

Application Date

2007-03-14

Priority Date

2007-03-14

Granted

No

Possible Cooperation

For further information please contact the transfer office.