Joint Turbine Rotor Bend Correction by Local Heating and Cooling

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Conventional methods for correcting bends in joint type-turbine rotors, such as journal correction and balance weight addition, are insufficient and have limited effectiveness, especially as the rotor ages and materials deviate in alloying elements.

Innovation Solution

A method involving measuring displacement at the joined portion, local heating of the convex portion to exceed the transformation point, and controlled cooling to induce plastic deformation and reduce the bend, while minimizing material hardening and cracking risks.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If journal correction process or balance weight addition is used to correct bend, then the bend of turbine rotor is corrected, but the correction effectiveness is limited and cannot cover all bending problems

Engineering Contradiction:
Improvebend correction effectivenessVSAvoidapplicability to different bending cases
Core Design Contradiction:
Manufacturing precisionVSAdaptability or versatility

Solution Approach 1:

The invention changes the physical state of the metal material by controlling temperature parameters during local heating. By heating the convex portion to specific temperature ranges (including transformation points for steels), the material undergoes phase changes that enable plastic deformation and bend correction, providing a more versatile solution compared to conventional mechanical methods.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The invention utilizes phase transitions of metal materials during heating and cooling processes. When the convex portion is heated to transformation temperatures and then cooled, the material undergoes phase changes (such as austenite to martensite transformation in steels) that create plastic deformation to correct the bend, expanding the适用范围 beyond what conventional methods can achieve.

Inventive Principle:
Principle #36Phase transitions

2Manufacturing precision

If local heating is applied to correct bend, then the displacement is reversed and the rotor approaches straight-axis state, but material hardening and cracking risks increase

Engineering Contradiction:
Improvestraight-axis state achievementVSAvoidmaterial resistance to hardening and cracking
Core Design Contradiction:
Manufacturing precisionVSStrength

Solution Approach 1:

The invention applies local heating only to the convex portion of the bent rotor rather than heating the entire rotor. This localized approach concentrates thermal energy where needed to induce plastic deformation for bend correction, while minimizing the overall thermal impact on the rotor structure and reducing the risk of widespread material hardening and cracking.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The heating and cooling process is performed in controlled cycles with specific temperature ranges and holding times. By using periodic thermal action with controlled parameters including transformation points, the invention achieves gradual plastic deformation that corrects the bend while allowing the material to undergo controlled phase transitions that reduce residual stresses and minimize hardening effects.

Inventive Principle:
Principle #19Periodic action

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

Effectively corrects the bend by reversing the displacement, allowing the turbine rotor to approach a straight-axis state with reduced vibration impact, suitable for various materials including those prone to cracking like 3.5 Ni—Cr—Mo—V steel.

Implementation Method 1

heating the convex portion

Methodology Applied
Scientific EffectThermal heating: Heating

Implementation Method 2

heating the convex portion; and cooling the joined portion after the step of heating

Methodology Applied
Scientific EffectPhase transformation: Phase Change

Implementation Method 3

cooling the joined portion after the step of heating

Methodology Applied
Scientific EffectThermal cooling: Cooling

Implementation Method 4

cooling the joined portion after the step of heating

Methodology Applied
Scientific EffectThermal contraction: Thermal Contraction

Data Source

PatentUS11679430B2Method of correcting bend of joint type-turbine rotor
Publication Date: 2023.06.20 KK TOSHIBA
  • US11679430B2 patent drawing
  • US11679430B2 patent drawing
  • US11679430B2 patent drawing

AI summary

According to an embodiment, a method of correcting a bend of a joint type-turbine rotor comprises: measuring displacement of a convex portion of the bend at a joined portion of the joint type-turbine rotor or displacement of a surface opposite to the convex portion in a circumferential direction of the joint type-turbine rotor; heating the convex portion; and cooling the joined portion after the step of heating. The steps of heating and cooling are performed during the step of measuring.