Solder alloy and method for repairing a part
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
Inventors & Applicants
Inventors
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
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