Titanium-Steel Diffusion Bonding with Interlayers for Turbine Shafts

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Solution Overview

Problem

The assembly of titanium and steel parts in turbomachine components poses challenges due to unsatisfactory mechanical characteristics at titanium-steel junctions, particularly in high-torque applications where noise, consumption, and CO2 emissions need to be reduced without modifying the diameter or weight of the turbine shaft.

Innovation Solution

A diffusion welding process involving thin interlayers of niobium or vanadium on the titanium side and copper on the steel side, followed by hot isostatic compression and controlled cooling, along with specific heat treatment, to create strong intermetallic phases and maintain contact through differential thermal dilation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If diffusion welding is used to join titanium and steel parts, then the mechanical strength at the junction is improved, but intermetallic phases form that weaken the junction

Engineering Contradiction:
Improvemechanical strength at junctionVSAvoidjunction durability
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The patent introduces intermediate interlayer materials (niobium, vanadium, or copper layers) between the titanium and steel parts. These interlayers act as mediators that prevent direct contact and harmful intermetallic phase formation between titanium and steel, while still enabling effective stress transfer and achieving the required mechanical strength at the junction.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Strength

If hot isostatic compression is applied to assemble titanium and steel parts, then diffusion welding is achieved, but thermal dilation differences cause loss of contact between parts

Engineering Contradiction:
Improvewelding bond strengthVSAvoidcontact maintenance during heating
Core Design Contradiction:
StrengthVSStability of the object's composition

Solution Approach 1:

The patent explicitly accounts for and utilizes the differential thermal expansion between titanium and steel during hot isostatic compression. By designing the compression process and part geometry to compensate for these expansion differences, the patent maintains continuous contact between the parts throughout the heating and cooling cycles, ensuring proper diffusion bonding while preventing separation.

Inventive Principle:
Principle #37Thermal expansion

3Ease of manufacture

If titanium and steel parts are assembled by conventional welding, then the parts can be joined, but the junction presents unsatisfactory mechanical characteristics

Engineering Contradiction:
Improveassembly feasibilityVSAvoidjunction mechanical characteristics
Core Design Contradiction:
Ease of manufactureVSStrength

Solution Approach 1:

The patent replaces conventional welding processes with diffusion bonding through hot isostatic compression. This substitution eliminates the harmful effects of traditional welding (such as poor metallurgical compatibility and weak joints) by using a solid-state diffusion process that creates strong, reliable joints between titanium and steel parts with appropriate interlayers.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

4Device complexity

If the turbine shaft uses homogeneous material, then the manufacturing is simpler, but the torque transmission capability cannot be significantly increased without modifying diameter and weight

Engineering Contradiction:
Improvematerial composition simplicityVSAvoidtorque transmission capability
Core Design Contradiction:
Device complexityVSPower

Solution Approach 1:

The patent employs composite construction by assembling titanium and steel parts with different mechanical properties. The titanium central part provides lightweight strength while the steel end parts provide high torque transmission capability. The diffusion-bonded junctions with interlayers ensure effective stress transfer between the dissimilar materials, enabling significantly increased torque transmission without changing the overall diameter and weight of the turbine shaft.

Inventive Principle:
Principle #40Composite materials

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This process achieves high mechanical strength and durability at the titanium-steel junctions, enabling efficient torque transmission and extended service life without damage, while reducing environmental impact.

Implementation Method 1

the intercalases prevents migrate titanium in the Steel and that iron migrates in titanium

Methodology Applied
Scientific EffectDiffusion barrier: Diffusion Barrier

Implementation Method 2

the process by welding diffusion of pieces of a different nature, one in titanium and the other in steel

Methodology Applied
Scientific EffectDiffusion welding: Diffusion Welding

Implementation Method 3

to subject this set to a hot isostatic compression, at a temperature between 900 °C and 950 °C approximately and at a pressure between 1000 bars and approximately 1500 bars

Methodology Applied
Scientific EffectHot isostatic pressing: Hot Isostatic Pressing

Implementation Method 4

These forms take advantage of the difference in thermal dilation between titanium and steel during hot isostatic compression, to guarantee the maintenance of contact between the two parts during heating and cooling

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Data Source

PatentEP2340142B1Methof of joining a titanium workpiece with a steel workpiece through diffusion bonding
Publication Date: 2022.11.16 SAFRAN AIRCRAFT ENGINES SAS
  • EP2340142B1 patent drawingFigure 1~3
  • EP2340142B1 patent drawingFigure 4~6

AI summary

The invention relates to a method for assembling titanium parts and steel parts by diffusion welding that comprises placing two thin spacers (14, 16) made of niobium or vanadium and of copper, respectively, between a titanium part (10) and a steel part (12), placing the part and spacer assembly under vacuum, and subjecting the same to hot isostatic compression at a temperature of between 900°C and 950°C and under a pressure of between 1000 and 1500 bars for about two hours. The invention also relates to the production of turbine shafts for turbine engines.