Joint Turbine Rotor Bend Correction by Local Heating and Cooling
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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
Engineering 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
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.
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.
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
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.
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.
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
Implementation Method 2
heating the convex portion; and cooling the joined portion after the step of heating
Implementation Method 3
cooling the joined portion after the step of heating
Implementation Method 4
cooling the joined portion after the step of heating
Data Source
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.


