Solder Alloy and Method for Repairing a Component

Publication: WO2009018839A1
Published: 2009-02-12
Family Size: 1
Granted: No

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

This patent describes a new nickel-based solder alloy, which includes zirconium and preferably also germanium, and a method for repairing components made from high-performance materials, such as turbine blades. The solder alloy is designed to fill cracks or voids in components without the drawbacks of conventional welding, such as substrate damage or element evaporation, and is especially useful for nickel- or cobalt-based superalloy parts exposed to high temperatures.

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

  • Repairing cracks or voids in turbine blades used in gas or steam turbines.
  • Maintenance and refurbishment of combustion chamber components in power plants or aircraft engines.
  • Restoration of high-temperature resistant shield elements in turbines and other industrial machinery.
  • Repairing nickel- or cobalt-based superalloy components in aerospace, energy generation, or chemical processing equipment.
  • Fixing or refurbishing components with directionally solidified or single-crystal structures where traditional welding is unsuitable.

BenefitsContent extracted from patent full text and abstract with AI.

  • Allows repair of high-value components without damaging the underlying substrate material.
  • Operates at lower temperatures than traditional welding, minimizing risk of substrate elemental evaporation or structure loss.
  • Produces strong joints with high mechanical integrity even at elevated operating temperatures.
  • Can be tailored to match the crystal structure (e.g., polycrystalline, directionally solidified, or single crystal) of the repaired part.
  • The alloy composition can be adjusted to enhance corrosion resistance, mechanical strength, and compatibility with specific superalloys.
  • Extends the service life of expensive and critical turbine or engine parts, reducing maintenance costs and downtime.
  • Reduces the need for complete replacement of components, contributing to cost savings and sustainability efforts.

Technical Classifications (CPCs)

Main Classifications

Chemistry & Materials Science

Manufacturing & Transport

Sub Classifications

Machine Tools & Metal-Working

Metallurgy & Alloys (Non-Ferrous)

CPC Codes

B23K35/3033C22C19/05C22C19/051C22C19/057

Inventors & Applicants

Applicants

Siemens Ag

Univ Friedrich Alexander Er

Heinz Paul

Ott Michael

Patent Abstract

The invention relates to a solder alloy comprising at least nickel zircon and preferably also germanium.

Key Information

Publication No.

WO2009018839A1

Family ID

39273530

Publication Date

2009-02-12

Application No.

EP2007006942W

Application Date

2007-08-06

Priority Date

2007-08-06

Granted

No

Possible Cooperation

For further information please contact the transfer office.