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High-Temperature Alloy Casting Turbine Parts Treatment Factory

目录
Thermal Processing for High-Strength Equiaxed Turbine Alloys
Core Heat Treatment Capabilities for Equiaxed Castings
Superalloys Commonly Heat Treated
Case Study: Heat Treatment of Equiaxed Rene 77 Vane Ring Segments
Project Background
Typical Heat Treated Component Models and Applications
Heat Treatment Challenges for Equiaxed Superalloy Castings
Certified Heat Treatment Solutions
Results and Verification
Thermal Process Execution
Post-Treatment Finishing
Inspection and Testing
FAQs

Thermal Processing for High-Strength Equiaxed Turbine Alloys

Equiaxed crystal castings made from nickel-based superalloys are widely used in turbine blades, vanes, and combustion components across aerospace and energy sectors. To unlock their full mechanical and microstructural performance, these castings require precision-controlled heat treatment cycles for grain refinement, stress relief, and phase transformation stabilization.

Neway AeroTech is a certified heat treatment supplier for equiaxed crystal superalloy castings such as Inconel 713C, Rene 77, and Hastelloy X. Our thermal processing solutions ensure structural integrity, dimensional stability, and fatigue resistance in both OEM and repair-grade components.

high-temperature-alloy-casting-turbine-parts-treatment-factory

Core Heat Treatment Capabilities for Equiaxed Castings

Our thermal cycles are engineered to meet turbine OEM and aerospace standards for grain control, residual stress management, and mechanical property optimization.

  • Solution treatment for gamma prime phase uniformity

  • Aging treatment to increase yield strength and creep resistance

  • Stress-relief annealing post-casting or machining to eliminate internal residual stress

  • Controlled ramp rates and inert atmosphere for oxidation-sensitive parts

All heat treatments conform to AMS 2774, AMS 5662/3, and customer-specific turbine alloy protocols.

Superalloys Commonly Heat Treated

Alloy

Max Service Temp (°C)

Heat Treatment Purpose

Application

Inconel 713C

950

Stress relief + aging

Nozzle guide vanes

Rene 77

1040

Solution + aging

Turbine blades, vane rings

Hastelloy X

1175

Grain stabilization

Combustor hardware

Nimonic 90

920

Aging hardening

Vane segments, valve guides

These alloys benefit from phase strengthening and microstructure densification via tightly controlled temperature-time profiles.

Case Study: Heat Treatment of Equiaxed Rene 77 Vane Ring Segments

Project Background

An aerospace customer submitted a batch of equiaxed Rene 77 cast vane segments requiring full-cycle thermal processing. The cycle included solution treatment at 1160°C, aging at 845°C for 24 hours, and final stress relief at 870°C. All parts met OEM microstructure and hardness requirements.

Typical Heat Treated Component Models and Applications

Component

Alloy

Process

Industry

Nozzle Segment

Inconel 713C

Aging + stress relief

Power Generation

Vane Ring

Rene 77

Solution + aging

Aerospace

Combustor Liner

Hastelloy X

Annealing + stress relief

Energy

Turbine Shroud

Nimonic 90

Aging hardening

Industrial Gas Turbines

All components are validated for grain size, phase structure, and hardness consistency post-treatment.

Heat Treatment Challenges for Equiaxed Superalloy Castings

  1. Uniform temperature distribution is critical to prevent grain boundary liquation and deformation

  2. Controlled ramp rates ≤ 10°C/min reduce thermal shock and structural distortion

  3. Atmospheric control (vacuum or argon) needed to suppress oxidation on critical surfaces

  4. Repeatability of microstructure across thick and thin cast cross-sections

  5. Residual stress relief required before CNC finishing or coating application

Certified Heat Treatment Solutions

  • Multi-zone furnaces with ±2°C thermal uniformity across load volume

  • Vacuum or argon purged chambers for reactive alloys like Rene and Hastelloy

  • Cycle programming with real-time data logging for full traceability

  • **Integrated post-treatment cleaning and passivation

  • HIP available as a combined service to eliminate porosity

Results and Verification

Thermal Process Execution

All cycles followed material-specific solution and aging protocols with soak times validated by thermocouple mapping. Castings were fixtured to minimize deformation during high-temperature exposure.

Post-Treatment Finishing

After treatment, parts underwent CNC machining or EDM. Surfaces were cleaned and passivated per AMS2700 for oxidation protection.

Inspection and Testing

SEM analysis confirmed phase formation and grain refinement. Hardness testing validated mechanical targets. X-ray inspection confirmed structural soundness post-treatment.

FAQs

  1. What heat treatment cycles are used for equiaxed turbine components?

  2. Can Inconel and Rene alloys be treated together in one furnace batch?

  3. How is oxidation prevented during high-temperature solution treatment?

  4. What inspection methods verify phase transformation and hardness?

  5. Do you offer HIP and CNC machining after heat treatment?