Method of Soldering Repair of a Component in a Vacuum and Adjusted Partial Oxygen Pressure and Global Pressure
Simple SummaryContent extracted from patent full text and abstract with AI.
This patent describes a method for repairing cracks or defects in high-performance metal components (such as those used in turbines) using a soldering technique in a special vacuum environment with strictly controlled low oxygen partial pressure. The method leverages specialized nickel-based solder alloys with precise compositions to ensure strong and reliable repairs without inducing unwanted oxidation or material evaporation. The process is particularly suitable for components made from nickel-, cobalt-, or iron-based superalloys, often found in turbine blades and combustion chamber elements.
Use CasesContent extracted from patent full text and abstract with AI.
- Repair of turbine blades in gas or steam turbines for aerospace or energy generation industries.
- Reconditioning of high-temperature combustion chamber components.
- Maintenance and refurbishment of components made from nickel-based superalloys.
- Restoration of single-crystal or directionally solidified metal parts exposed to extreme thermal stress.
- Crack sealing and structural repair in advanced engine components to extend their service life.
BenefitsContent extracted from patent full text and abstract with AI.
- Reduces oxidation and evaporation risks during high-temperature soldering repairs by using low oxygen partial pressures.
- Produces strong, durable repairs that can withstand high operational temperatures and mechanical stresses.
- Enables re-use and life extension of expensive, high-performance components, saving costs and reducing waste.
- Compatible with intricate and sophisticated metal parts, including single-crystal and directionally solidified structures.
- Provides flexibility in solder alloy compositions for optimal mechanical properties and process adaptability.
Technical Classifications (CPCs)
Main Classifications
Chemistry & Materials Science
Manufacturing & Transport
Mechanical Eng. & Systems
Sub Classifications
Machine Tools & Metal-Working
Machines & Engines (General)
Metallurgy & Alloys (Non-Ferrous)
CPC Codes
Inventors & Applicants
Inventors
Applicants
Mtu Aero Engines Gmbh
Univ Friedrich Alexander Er
Patent Abstract
Repair of cracks (7) in components (1) using solder (10) is carried out in a process chamber in which the partial pressure of oxygen is below 3.5 x 10 ->6>mbar.
Key Information
Publication No.
EP2117756A1
Family ID
38294164
Publication Date
2009-11-18
Application No.
EP08709017A
Application Date
2008-02-15
Priority Date
2008-02-15
Granted
Yes (1/5)
Possible Cooperation
For further information please contact the transfer office.