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Waspaloy CNC Machining: Properties, Applications, Machining Challenges & Cost Control Guide

0   |   Published by VMT at Oct 28 2026   |   Reading Time:About 8 minutes

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In aerospace, defense, and energy applications, components must operate reliably under extreme temperature, pressure, and corrosive environments. Many stainless steels, and even common titanium alloys, lose structural strength rapidly at temperatures exceeding 600°C. To meet these harsh demands, Waspaloy CNC machining has become a critical manufacturing solution for high-reliability components.

 

As a premium nickel-based superalloy, Waspaloy delivers exceptional high-temperature mechanical performance. However, its high work-hardening rate and low thermal conductivity make it one of the most challenging materials to machine. This guide covers Waspaloy's material properties, target applications, machining difficulties, and cost-control strategies to help you successfully produce precision Waspaloy parts. At the end, we share a case study of how our machining factory resolve coaxiality and thermal distortion in an 800mm waspaloy aerospace turbine shaft to achieve ±0.005 mm precision and 98.7%.

 

 

What is Waspaloy CNC Machining ?

 

Waspaloy CNC machining refers to the precision manufacturing process of cutting, turning, milling, and grinding Waspaloy (UNS N07001), a precipitation-hardenable nickel-based superalloy, using high-rigidity CNC machine tools and 5-axis machining centers.

 

Waspaloy Materials Composition and Mechanical Properties

 

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As detailed in the chemical and mechanical property breakdown above, Waspaloy is engineered for extreme environments:

 

  • High-Temperature Strength:Maintains exceptional tensile (145–175 ksi) and yield strength (100–115 ksi) up to 1,500°F–1,600°F (815°C–870°C), with maximum service limits reaching 1,800°F (980°C).
  • Hardness & Creep Resistance:Typically supplied or utilized at 34–44 HRC, offering outstanding resistance to deformation under sustained high thermal and mechanical stress.

 

Waspaloy belongs to the elite tier of custom superalloys CNC machining. Because its mechanical properties far exceed standard metals, utilizing standard machining parameters or general-purpose tooling will instantly cause tool chipping or catastrophic part failure, making advanced machine rigidity and specialized tooling non-negotiable. Therefore, you need to pay attention to the machining services supplier possessing a range of advanced machining equipments.

 

 

 

Where Can You Use Waspaloy CNC Machined Parts?

 

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Thanks to its physical and chemical stability in high-temp and high-strength environments like aerospace, defense, and energy applications, Waspaloy CNC machined parts are widely used in critical industrial applications where safety is paramount and failure is never an option:

 

 

Compressor and Rotor Discs

 

  • Subjected to massive centrifugal forces from high-speed rotation and extreme temperatures generated by high-pressure gases.
  • Waspaloy provides exceptional yield strength and fatigue resistance, ensuring rotor discs maintain micrometer-level dimensional stability at tens of thousands of revolutions per minute, preventing deformation or bursting caused by centrifugal stress.

 

Turbine Shafts and Seals

 

  • Core torque-transmission components exposed to extreme thermal and axial tensile stresses.
  • Turbine shafts must transmit immense mechanical power. Waspaloy's high shear strength and outstanding thermal fatigue resistance make it the ideal choice for connecting high-pressure compressors to turbine sections, while Waspaloy seals maintain stable sealing clearances under severe high-temperature and high-pressure differentials.

 

High-Temperature Casings and Rings

 

  • Engine combustion chambers and external turbine containment structures directly exposed to high-temperature combustion gases.
  • It offers excellent thermal expansion control and high thermal stability, effectively enclosing internal high-speed rotating parts while resisting casing creep and deformation under high pressure differentials and severe thermal cycling.

 

Missile Systems and Airframe Hardware

 

  • Intense aerodynamic frictional heat generated during supersonic flight, as well as rocket engine thrust vector control zones.
  • Used to manufacture high-temperature fasteners, structural connection rings, high-temperature aerodynamic control fin shafts, and nozzle support structures, delivering reliable load-bearing capacity under transient extreme temperatures.

 

Gas Turbines and Chemical Processing

 

  • High-temperature gas turbines in land-based power plants and environments with corrosive chemical media.
  • Demonstrates unmatched resistance to high-temperature oxidation and sulfidation corrosion during long-term continuous operation spanning tens of thousands of hours, significantly extending equipment maintenance intervals.

 

 

 

Waspaloy VS Nimonic 90: Which One Should You Choose for Aerospace Turbine Blades?

 

 

Waspaloy alloy delivers high strength (tensile strength of 965 to 1100 MPa) and high-temperature resistance (870 to 980 degrees Celsius) due to its molybdenum and cobalt content. Meanwhile, Nimonic 90 performs exceptionally well in high-temperature applications (up to 815 degrees Celsius), offering outstanding creep resistance and high strength (tensile strength of 965 to 1100 MPa). As you can see, Waspaloy used for CNC machined aerospace turbine blades provides slightly better heat resistance and high-strength performance while offering greater safety, whereas choosing Nimonic 90 can help slightly reduce overall costs.

 

Aerospace Turbine Blades CNC Machining Manufacturing

 

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Is Waspaloy Hard to Machine?

 

Yes. The machinability rating of Waspaloy is typically 12% to 14%, making it difficult to machine, roughly comparable to Inconel alloys (12% to 16%), while Hastelloy is slightly more forgiving (16% to 25%). The challenges of machining Waspaloy carry risks of dimensional distortion and poor surface quality, but more importantly, tooling costs account for a high proportion of the quotation (potentially reaching up to 30%). It is essential to evaluate your partner factory's low-speed, high-feed and tool selection strategies, coolant and machine rigidity configurations, and quality management systems to reduce defect rates and costs.

 

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Why is Waspaloy So Difficult to Machine?

 

 

Understanding Waspaloy’s unique machining challenges is essential for your teams looking to prevent part rejection, control high tooling expenses, and optimize production efficiency. Here are the reasons:

 

1.Work Hardening: Waspaloy rapidly hardens when subjected to stress and deformation during cutting, especially if CNC cutting forces are too high. Subsequent passes must cut through this newly hardened layer, making ongoing machining extremely difficult.

 

2.High Tensile Strength: Waspaloy boasts high tensile strength—typically reaching around 160,000 psi (1,103 MPa) in the fully aged condition. Compared to alloys with lower tensile strength, machining Waspaloy requires significantly greater cutting forces, which in turn easily triggers work hardening.

 

3.Abrasive Microstructure: The microstructural particles within the alloy act like fine sandpaper on cutting tools, making this already tough-to-machine material even more demanding on tooling life.

 

4.Chemical Reaction and Built-Up Edge (BUE): At elevated cutting temperatures, Waspaloy can chemically react with the material of the cutting tool. In fact, "sticking" or adhesion can occur, where workpiece material welds onto the cutting edge.

 

 

 

Common Manufacturing Errors for Waspaloy CNC Machining

 

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These factors are also the root causes behind several common manufacturing errors, including:

 

1. Geometric distortion and dimensional out-of-tolerance in Waspaloy parts: Slender shafts or structures with large hollow bores are particularly prone to bending due to residual stress relief.

 

2. Hard-to-detect thermal microcracks in Waspaloy components: These cracks lead to fatigue failure, posing critical risks in high-stakes aerospace applications.

 

3. Barreling effect during shaft machining: When machining Waspaloy shaft components, the center segment often ends up thicker than both ends, creating a "barrel-shaped" error.

 

4. Localized hardening caused by dwell or tool dulling: Tool hesitation (dwelling) or edge wear causes severe local work hardening, rendering subsequent passes unmachinable and scrapping the part.

 

5. Tool marks or inaccurate geometry at step-shaft fillet radii: Poor surface finish or incorrect profiles at the fillet radius create stress concentration points where cracks originate.

 

6. Poor chip evacuation during deep hole drilling: Inadequate chip removal leads to rapid temperature spikes, causing the drill bit to seize and burst inside the hole, resulting in a scrapped part.

 

 

 

How Do Machine Shops Resolve These 6 Manufacturing Errors?

 

 

To overcome the severe work-hardening rates and thermal sensitivity of Waspaloy, experienced CNC machining suppliers typically mitigate these errors through optimized process routing, upgraded tooling strategies, and strict in-process quality control:

 

 

1. Preventing Geometric Distortion and Dimensional Out-of-Tolerance

 

  • Control Strategy:Staged machining combined with stress relieving.
  • Implementation:Avoid finishing the part in a single pass. After rough machining with proper stock allowance, a dedicated stress-relieving heat treatment is introduced to release internal residual stresses before final precision machining. For slender shafts or thin-walled hollow components, symmetrical cutting and specialized follower rests are utilized to support the workpiece and prevent bending from cutting forces.

 

2. Romoving Hard-to-Detect Thermal Microcracks and Fatigue Risks

 

  • Control Strategy:Low-heat cutting parameters paired with 100% Fluorescent Penetrant Inspection (FPI).
  • Implementation:Worn or dull tools are strictly prohibited. Cutting speeds are reduced, and high-pressure coolant (HPC) is delivered directly into the cutting zone to minimize heat accumulation at the source. After machining, 100% FPI is performed to inspect for surface and subsurface microcracks, ensuring zero-defect delivery for critical aerospace components.

 

3. Correcting the "Barreling Effect" on Shaft Components

 

  • Control Strategy:Dynamic compensation, path micro-adjustments, and segmented turning.
  • Implementation:The center section of a long shaft tends to deflect due to lower rigidity. Machinists apply taper dynamic compensation or segmented turning strategies in CNC programming, paired with high-rigidity tailstocks and steady rests to counteract cutting forces and ensure consistent diameter and coaxiality across the entire length.

 

4. Avoiding Localized Over-Hardening Caused by Dwell

 

  • Control Strategy:Optimized G-code programming and strict tool life management.
  • Implementation:Tool dwelling (hesitation) on the cutting surface is strictly forbidden during G-code programming, ensuring continuous feed movement. Additionally, a strict tool life management protocol is enforced to replace inserts before reaching critical wear limits, preventing dull edges from causing severe work hardening.

 

5. Romoving Tool Marks and Crack Risks at Step-Shaft Fillet Radii

 

  • Control Strategy:Custom full-radius tooling and CMM/optical profile inspection.
  • Implementation:Precision full-radius carbide or ceramic-coated tools are selected for finish passes, combined with corner smoothing toolpaths. After machining, the fillet radius profile is strictly verified using a Coordinate Measuring Machine (CMM) or optical contour racer to eliminate potential stress concentration points.

 

6. Preventing Deep Hole Drilling Seizure and Tool Bursting

 

  • Control Strategy:High-pressure internal coolant gun drilling/deep hole drilling with peck cycles.
  • Implementation:Specialized deep hole drills equipped with high-pressure through-spindle coolant (70–100 bar) are used to inject coolant directly to the hole bottom, flushing out chips and rapidly lowering temperatures. Optimized chipbreakers and peck drilling cycles are implemented to prevent chip clogging and bit breakage inside the hole.

 

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Do Waspaloy CNC Machined Parts Rust Easily?

 

Don't worry, Waspaloy features exceptional resistance to rust and oxidation, making it highly corrosion-resistant in chemical and aerospace applications involving contact with high-temperature air and fuel. However, for an extra layer of security and to further extend the service life of Waspaloy CNC machined parts, applying protective coatings is recommended, such as MCrAlY coatings, diffusion aluminides, and Hastelloy C-series (Ni-Cr-Mo alloy) based coatings.

 

 

What Coatings is Neccassary to Use for Custom Waspaloy Parts?

 

 

When deciding whether to apply a coating and which type to choose, it is recommended to evaluate based on the following dimensions:

 

  • Operating Temperature and Environment:If exposed long-term to oxygen-rich combustion gases above 900°C or corrosive atmospheres containing sulfur and vanadium, prioritize anti-oxidation/hot-corrosion coatings.
  • Structural Complexity:Parts with internal cooling holes or complex internal cavities (such as turbine blades) are better suited for diffusion coatings, while external surfaces are ideal for overlay coatings.
  • Budget Balance:Considering the part's criticality within the overall system and replacement costs, select the most cost-effective process—avoid blindly pursuing the most expensive option.

 

 

Table: Coating Options and Comparison for Custom Waspaloy Parts

 

 

Coating Type Key Composition and Process Main Features Application Scenarios Cost Comparison
MCrAlY Overlay Coatings • Ni, Co, Cr, Al, Y alloys

• Thermal spray (HVOF), PVD
Dense protective oxide film; resists high-temp spallation; acts as TBC bond coat External turbine blades, combustion chamber liners High

Strict equipment and vacuum requirements; top-tier high-temp protection
Diffusion Aluminides • Al diffusion into base metal

• CVD, aluminizing process
Strong metallurgical bond; nickel-aluminum compound; does not peel off easily Complex shapes, turbine parts with internal cooling channels High Cost-Performance

High batch efficiency and mature technology for high-volume or cavity parts
Hastelloy C-Series Based Coatings • Ni-Cr-Mo alloy base

• Weld overlay, thermal spray
Rich in Mo & Cr; superior pitting and crevice corrosion resistance Chemical machinery, components exposed to corrosive fuels/exhaust Moderate

Cost depends on method/thickness; targets specific chemical corrosion

 

 

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How to Control the Comprehensive Production Cost of Custom Waspaloy Parts?

 

 

Waspaloy’s expensive raw material price and extremely high machining difficulty (machinability rating of only 12%–14%) dictate that the production cost of its custom parts is much higher than that of ordinary metals. However, high cost does not mean paying blindly. Through refined management across design, machining, quality, and post-processing, significant cost reduction and efficiency gains can be achieved without sacrificing component performance and safety.

 

 

1. Drawing and Design Stage: Optimizing Manufacturability from the Design

 

Up to 70% of manufacturing costs are determined during the design phase. When drawing blueprints or submitting procurement requirements, optimizing design can significantly reduce machining difficulty:

 

  • Reasonable Tolerances and Surface Roughness:Avoid overly tight tolerance requirements (such as micron-level tolerances or roughness below Ra 0.4 μm) on non-critical mating surfaces. For Waspaloy, excessive precision demands mean extra precision grinding or polishing processes, multiplying machining hours.
  • Optimized Geometric Shapes:Avoid excessively deep, narrow slots, tiny internal fillet radii, or ultra-thin-walled structures. Deep slots and small radii require small-diameter tools and lower cutting speeds, easily causing tool wear or chatter and drastically lengthening the machining cycle.
  • Reserving Reasonable Machining Stock:For parts requiring heat treatment (like stress-relieving annealing), reserving moderate stock prevents direct scrapping due to thermal stress deformation. However, excessive stock increases cutting time and tool wear, making a balanced process approach essential.

 

2. Machining and Manufacturing Stage: Choosing a Factory That Understands "Time and Tool Management"

 

In Waspaloy quotations, machining hour fees and tool wear costs (which can account for 20% to 30% of the quote) are two core components. When evaluating a factory's cost-reduction capability, focus on its process level:

 

  • Tool Consumption Optimization:Professional factories use custom carbide or ceramic-coated tools and enforce strict tool life management strategies. Through low-speed high-feed cutting parameters and high-pressure coolant (HPC), they increase material removal rates (MRR) while protecting tool life, lowering per-part tool costs.
  • Machining Time Control:Factories equipped with high-rigidity 5-axis machining centers or mill-turn centers can achieve "one-chuck multi-face machining," drastically cutting setup and adjustment time while avoiding cumulative positioning errors from multiple setups.

 

3. Quality Control Stage: Reducing Scrap Rates is the Best Cost Saving

 

In Waspaloy machining, zero defects and low scrap rates equal maximum cost savings. Due to the material's extremely high value and numerous processing steps, scrapping a nearly finished part loses not just the raw material, but all preceding labor hours and tool costs.

 

  • Reviewing the Supplier's Process Router:Ensure the factory arranges a standard stress-relieving annealing process between roughing and finishing to prevent parts from distorting and being scrapped due to stress relief after final machining.
  • Full-Process Quality Monitoring:Prioritize suppliers equipped with in-process inspection and fluorescent penetrant inspection (FPI) capabilities to promptly screen out defective items and avoid continuing to invest subsequent process costs into unqualified parts.

 

4. Surface Coating Selection: Adhering to "On-Demand Selection" Over Blind Upscaling

 

Coatings are crucial for extending Waspaloy component life, but costs vary dramatically among coating processes (e.g., PVD/HVOF overlays vs. traditional aluminizing):

 

Precise Assessment of Operating Environment: If the part operates only around 800°C without strong corrosive media, Waspaloy's native oxidation layer is sufficient, eliminating the need to stack expensive multilayer thermal barrier coatings (TBCs).

 

Tiered Coating Solutions: For components with complex internal cavities or film cooling holes, prioritize diffusion aluminides, which offer high batch processing efficiency and excellent cost-performance; reserve high-cost MCrAlY overlays exclusively for absolute extreme ultra-high-temperature combustion sections.

 

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Final Thoughts

 

Looking back across this entire guide, custom manufacturing Waspaloy parts requires a solid understanding of full-lifecycle process management, from initial drawing design to final surface protection:

 

  • Material Understanding and Application:Grasping Waspaloy’s unique properties to determine whether its application conditions align with your project requirements.
  • Material Comparison:Comparing Waspaloy against other similar high-temperature alloys to evaluate whether alternative materials might be a better fit.
  • Design and Cost Control:Leveraging Design for Manufacturability (DFM) optimization, setting realistic tolerances, and verifying that your supplier maintains a scientific process router to minimize Waspaloy’s high manufacturing costs and scrap risks.
  • Machining and Quality Control:Auditing whether a supplier can safeguard quality through low-speed/high-feed strategies, high-pressure coolant (HPC), specialized tooling, and 100% Fluorescent Penetrant Inspection (FPI).
  • Surface Protection Selection:Precisely matching protective coatings—such as MCrAlY overlays, diffusion aluminides, or Hastelloy C-series coatings—based on actual operating conditions (e.g., combustion gases above 900°C or harsh chemical environments) to balance performance and budget.

 

Facing challenges with Waspaloy part out-of-tolerance errors, high costs from rapid tool wear, or persistent scrap rates?

 

Submit your 3D CAD drawings today for a free DFM manufacturability evaluation and a customized stress-relieving process proposal, helping you achieve aerospace-grade precision while lowering your comprehensive production costs. [ We support 2D Drawings (PDF files), 3D Drawings (IGS/STP/STEP files)].

 

 

 

VMT CNC Machining Factory Case Study

 

Resolving Coaxiality and Thermal Distortion in an 800mm Waspaloy Aerospace Turbine Shaft to Achieve Sub-Micron Precision

 

In a procurement project for critical aero-engine components, a client required a custom 800 mm long Waspaloy aerospace-grade center-hollow turbine shaft featuring multi-step diameters ranging from 50 mm to 120 mm, imposing rigorous geometric and positional tolerance requirements across its entire length. However, the batches delivered by the previous supplier suffered from coaxiality out-of-tolerance at both ends of the shaft, with radial runout exceeding the aerospace-grade requirement of 0.01 mm (10 μm), leading to total batch rejection and project delay risks.

 

Upon taking over the project, our engineering team conducted a comprehensive review of the original process and identified two primary process bottlenecks that had not been properly managed:

 

  • Absence of Intermediate Stress-Relieving Processes:The previous supplier adopted a straightforward "one-pass machining to final dimensions" strategy. Due to Waspaloy's extreme cutting forces, high residual stresses accumulated during machining, which instantly released the moment the part was unlatched from the machine fixture, causing irreversible micro-bending of the shaft body.
  • Improper Workholding and Support Strategy:For the 800 mm slender shaft structure, excessive and concentrated clamping forces induced elastic deformation during machining, which rebounded after unclamping and triggered coaxiality deviations.

 

To address these root causes, we redesigned a scientific and standardized combination CNC machining and heat treatment process for the client:

 

  • Staged Machining and Intermediate Stress-Relieving Annealing:A stock allowance of 2.0–2.5 mm was left during roughing to release the majority of cutting heat and thermal stress. Subsequently, a dedicated vacuum stress-relieving annealing process was introduced to ensure thorough internal stress relief before proceeding to semi-finishing and finishing.
  • Dynamic Auxiliary Support and Flexible Workholding:High-precision NC hydraulic follower rests were configured on the mill-turn center to provide real-time tracking support matching the cutting position, effectively counteracting shaft bending caused by cutting forces. Additionally, hydraulic tension tailstocks were utilized to strictly control clamping forces below the deformation threshold.
  • High-Pressure Coolant and Toolpath Optimization:Through-hole drilling utilized an 80-bar spindle coolant gun drill to powerfully evacuate chips and control thermal accumulation inside the deep hole. For step-shaft transition zones, custom full-radius coated tools combined with corner smoothing toolpaths were deployed to eliminate stress concentrations from the ground up.

 

Through optimized full-process control, we successfully helped the client resolve the precision bottleneck and achieved quantifiable performance improvements:

 

  • Full Precision Compliance:The overall coaxiality of the shaft was stably controlled within 0.005 mm (5 μm), and radial runout was reduced to 0.006 mm, outperforming the 0.01 mm aerospace acceptance standard.
  • Significant Improvement in Yield Rate:The scrap rate during mass production dropped from the previous supplier's over 25% to below 1.3% (achieving a yield rate of 98.7%).
  • 23% Reduction in Comprehensive Costs:Driven by zero scrap rates and enhanced material removal rates (MRR), the overall delivery schedule was shortened by 13 days, and the client's single-unit comprehensive procurement cost decreased by 23%.

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FAQs

 

 

What is the relationship between Waspaloy and Superalloys?

 

Waspaloy is a specific type of superalloy. Superalloys are high-performance materials widely used in CNC machining for the aerospace and energy sectors due to their exceptional high-temperature resistance. Other prominent superalloys include Inconel alloys, Hastelloy, Stellite 31 / X-40, and René N5. You can evaluate the specific properties of these materials to determine if they match your part's operating environment.

 

 

Waspaloy vs. Hastelloy: Do they share the same machining challenges?

 

Yes, both alloys share core machining hurdles such as rapid work-hardening, low thermal conductivity, and high abrasive wear on cutting tools. However, while Waspaloy demands higher cutting forces due to its extreme yield strength from precipitation hardening, Hastelloy generally poses a higher risk of chemical adhesion and Built-Up Edge (BUE) formation during machining.

 

 

Is it necessary to inspect Waspaloy surfaces for thermal microcracks caused by machining overhead?

 

Absolutely. Performing Fluorescent Penetrant Inspection (FPI) after finish machining Waspaloy precision parts is an essential step in the CNC machining workflow. Even though it contributes to the overall cost, it is vital to ensure long-term operational safety and part integrity.

 

 

What is the role of stress-relieving aging treatment in the process?

 

This is a critical manufacturing stage for custom precision Waspaloy parts. Incorporating a complete stress-relieving aging treatment between roughing and finishing significantly reduces residual stress and prevents part scrapping caused by subsequent work-hardening. When reviewing a potential supplier's process router, always scrutinize their experience in stress-relieving heat treatments.

 

 

Since Waspaloy is so difficult to machine, what surface roughness can be achieved?

 

Achieving Ra 0.8–1.6 μm after finish machining is a standard baseline for surface rouhness. If your application requires a smoother surface, secondary processing is necessary, such as precision grinding (achieving Ra 0.2–0.4 μm) or lapping/polishing (reaching mirror-like finishes of Ra 0.02–0.05 μm). Keep in mind that these additional steps will increase lead times and costs, so it is best to consult your supplier with your engineering drawings.

 

 

What does "leaving stock allowance for grinding" mean in practice?

 

This is a common machining strategy used by factories for Waspaloy component surfaces. For the most critical features on a part, such as turbine shaft bearing journals, they will reserve a single-sided stock allowance of 0.1–0.3 mm during CNC turning. The part is then transferred to a high-precision cylindrical grinder using diamond or CBN (Cubic Boron Nitride) wheels to achieve a refined surface roughness of Ra 0.2–0.4 μm, which belongs to the precision grinding.

 

 

What is the difference between Waspaloy AMS 5707, 5706, and 5708 in CNC machining?

 

These AMS specifications define the raw material form and heat-treatment state:

  • AMS 5707 (Bars and Forgings):As the most commonly used CNC raw material stock, it is delivered double-aged (34–44 HRC) for high-stress aerospace parts like turbine discs, rotor hubs, and heavy fasteners.
  • AMS 5706 (Bars and Rings):Supplied in a standard heat-treated condition, making it the preferred stock for turning long structural turbine shafts, seals, and high-pressure casings.
  • AMS 5708 (Sheets and Plates):Provided in a solution-treated state with lower initial hardness, ideal for milling and forming thin-walled combustion chamber liners and ring structures before final aging.

 

 

Disclaimer

 

The technical information and manufacturing advice shared on the VMT website are for general guidance only. While we strive for accuracy, VMT does not guarantee that the processes, tolerances, or material properties mentioned are applicable to every specific project. Any reliance you place on such information is strictly at your own risk. It is the buyer's responsibility to provide definitive engineering specifications for any production orders. Final specifications and service terms shall be subject to the formal contract or quotation confirmed by both parties.

 

 

 

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