Method of Soldering Repair of a Component in a Vacuum and Adjusted Partial Oxygen Pressure and Global Pressure

Publication: EP2117756A1
Published: 2009-11-18
Family Size: 5
Granted: Yes (1/5)

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

B23K1/0018B23K1/008B23K1/206B23K35/30B23K35/304C22C19/05C22C19/057F01D5/005

Inventors & Applicants

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.