Equiaxed crystal cast Rene alloy parts are widely used in gas turbine engines, power plant hardware, and aerospace hot section components. While equiaxed casting provides robust isotropic properties and cost-effective production, welding these nickel-based superalloys requires tight control over heat input, filler compatibility, and post-weld microstructure restoration to avoid hot cracking and HAZ embrittlement.
Neway AeroTech delivers welding services for equiaxed Rene alloy castings including turbine blades, vanes, and combustion liners. Our AS9100D and NADCAP-compliant processes include TIG and laser welding, supported by post-weld heat treatment, HIP, and detailed non-destructive inspection.
Neway AeroTech applies controlled welding methods to repair or join Rene alloy castings with high resistance to thermal fatigue and creep.
TIG welding using Rene-compatible filler metals for blade and vane tip restoration
Laser welding for precision joining in thin-walled turbine parts
Vacuum and inert gas welding chambers to suppress oxidation
Post-weld heat treatment to recover mechanical strength and grain uniformity
We routinely weld Rene 41, Rene 77, and Rene 80 components.
Rene Grade | Max Temp (°C) | Yield Strength (MPa) | Application |
|---|---|---|---|
980 | 950 | Turbine casings, flame holders | |
1040 | 960 | Vane rings, HPT nozzles | |
1050 | 880 | Combustor liners, transition ducts |
These alloys are engineered for weldability, thermal fatigue resistance, and oxidation durability under sustained high-temperature exposure.
A turbine maintenance customer submitted Rene 77 equiaxed cast nozzle segments exhibiting tip erosion and microcracking at trailing edges. TIG welding using Rene-matched filler metal was performed, followed by heat treatment and HIP processing. X-ray and SEM inspection confirmed crack elimination and grain continuity.
Component | Weld Type | Alloy | Industry |
|---|---|---|---|
Nozzle Segment | TIG multi-pass | Rene 77 | |
Flame Tube | Laser weld, low-distortion | Rene 80 | |
Blade Tip | TIG buildup + contouring | Rene 41 | |
Inner Liner Flange | Vacuum weld seam | Rene 41 |
Each weld zone is engineered to sustain creep, oxidation, and thermal cycling over extended service intervals.
Crack susceptibility due to gamma prime segregation at grain boundaries
HAZ hardening and distortion under uncontrolled arc conditions
Porosity control in multi-pass TIG welding
Low weld ductility post-solidification without tailored PWHT
Dimensional restoration of complex vane and blade profiles
Preheating to 400–650°C to reduce thermal gradients and minimize cracking
Low interpass temperature TIG welding with matched Rene filler wires
Post-weld heat treatment and HIP for microstructure recovery
CMM and final machining to restore profile geometry
Optional TBC coating after weld for hot section reusability
Welds were applied in controlled layers with gas shielding and matched wire composition. Penetration was validated via cross-section macrographs. Blended weld profiles ensured aerodynamic continuity in vane and blade surfaces.
Components underwent HIP at 1030°C and full-cycle stress-relief heat treatment. Machining restored fit interfaces and sealing surfaces. Optional coating applied on leading edges and outer shrouds.
X-ray testing confirmed weld fusion and porosity-free zones. CMM validated dimensional targets. SEM ensured no microcracks or grain coarsening in HAZ.
What Rene alloys are best suited for TIG vs. laser welding?
How do you mitigate cracking in Rene alloy weld zones?
Can equiaxed Rene parts be welded and recoated with TBC?
What is the typical post-weld heat treatment for Rene 77?
Do you offer weld repair for OEM turbine blade and vane hardware?