| Low-Carbon and Low-Alloy Steel | Construction steel, carburizing steel, machine components | Vacuum carburizing Quench and temper | 880–980°C | High vacuum for heating; hydrocarbon pulses for carburizing; high-purity nitrogen or helium for quenching | Gas quench followed by tempering at approximately 150–220°C | High surface hardness with a tough, low-carbon core | Useful for gears and shafts. Case depth depends on carburizing time, temperature, and carbon potential. Avoid excessive surface carbon, which can increase retained austenite and cracking risk. |
| Medium-Carbon and Alloy Steel | Quenched-and-tempered shafts, pins, dies, structural machine parts | Austenitizing Oil-free gas quench and temper | 800–900°C | Vacuum heating followed by nitrogen, helium, or argon backfill for inert cooling | Pressurized gas quench; temper commonly at 450–650°C | Balanced strength, hardness, and toughness with reduced oxidation | Section thickness and alloy hardenability determine the required gas-quench pressure. Large cross-sections may require slower cooling or a separate quench strategy. |
| Cold-Work Tool Steel | High-chromium tool steel, punch and die steel, wear-resistant tooling | Hardening Double or triple tempering | 1,000–1,080°C | High vacuum or partial-pressure inert gas; avoid decarburization and uncontrolled oxidation | High-pressure gas quench, followed by tempering at approximately 150–550°C | High wear resistance, dimensional stability, and compressive strength | Preheating steps reduce thermal shock. Multiple tempers are often used to transform fresh martensite and stabilize dimensions. |
| High-Speed Steel | Molybdenum or tungsten high-speed cutting-tool steel | High-temperature hardening Multiple tempering | 1,180–1,260°C | High vacuum with controlled partial pressure; protective gas during high-temperature holding and cooling | Rapid gas quench, commonly followed by two or three tempers around 540–570°C | Secondary hardness and hot-wear resistance | Temperature uniformity is critical because the austenitizing range is narrow. Excessive soaking can cause grain growth or distortion. |
| Hot-Work Tool Steel | Hot-work die steel, extrusion tooling, forging dies | Vacuum hardening Tempering and optional stress relief | 980–1,050°C | Vacuum or inert partial pressure with high-purity quench gas | High-pressure gas quench; temper commonly at 550–650°C | Hot strength, thermal-fatigue resistance, and toughness | Use controlled heating and staged preheating for complex dies. Uniform gas flow is important for minimizing distortion in large tooling. |
| Martensitic Stainless Steel | Hardenable stainless cutlery, valves, shafts, surgical instruments | Vacuum hardening Tempering | 980–1,070°C | High vacuum or inert partial pressure; prevent chromium-oxide scale and surface contamination | Gas quench followed by tempering, typically 150–650°C depending on grade and target properties | Corrosion resistance combined with high hardness and strength | Carbon and alloy content strongly affect the hardening temperature. Overheating may promote grain growth, retained austenite, or reduced corrosion performance. |
| Austenitic Stainless Steel | Corrosion-resistant process parts, medical and food-contact components | Solution annealing Stress relief when specified | 1,040–1,150°C | Vacuum or high-purity inert atmosphere; use clean, low-contamination fixtures | Rapid gas cooling to suppress carbide precipitation; water cooling may be required for some large sections | Restore corrosion resistance and dissolve unwanted precipitates | Cooling must be sufficiently rapid through the sensitization range. Vacuum processing does not replace the need for correct alloy-specific cooling rates. |
| Precipitation-Hardening Stainless Steel | High-strength corrosion-resistant components and aerospace hardware | Solution treatment Age hardening | 1,020–1,050°C solution treatment; 480–620°C aging | Vacuum or inert atmosphere with controlled cooling | Gas cooling, air cooling, or sub-zero treatment depending on grade; aging follows solution treatment | High strength with controlled corrosion resistance | Strength is highly dependent on aging temperature and time. Follow the material specification because different conditions can produce substantially different hardness and toughness. |
| Alpha Titanium Alloys | Commercially pure titanium and alpha titanium components | Stress relief Annealing | 540–760°C | High vacuum or ultra-high-purity argon; minimize oxygen, nitrogen, and hydrogen pickup | Furnace cooling or controlled inert-gas cooling | Reduce residual stress and improve dimensional stability | Titanium reacts readily with oxygen and nitrogen at elevated temperature. Clean surfaces, compatible fixtures, and tight atmosphere control are essential. |
| Alpha-Beta Titanium Alloys | Common aerospace-grade titanium components and high-strength fasteners | Stress relief Annealing or sub-transus treatment | 650–900°C | High vacuum or high-purity argon; avoid long exposure at temperatures that promote excessive alpha-case formation | Air, inert-gas, or furnace cooling according to the required microstructure | Control residual stress, strength, ductility, and fatigue performance | Processing below or above the beta transus produces different microstructures. Temperature uniformity and cooling rate should be validated for each section size. |
| Beta Titanium Alloys | Metastable beta titanium used for high-strength lightweight parts | Solution treatment Age hardening | 760–900°C solution treatment; 480–650°C aging | High vacuum or high-purity argon with very low residual oxygen and moisture | Rapid cooling after solution treatment, followed by controlled aging | High specific strength and adjustable mechanical properties | Small changes in solution and aging conditions can change the balance of beta, alpha, and metastable phases. Atmosphere contamination can reduce ductility and fatigue performance. |
| Nickel-Based Superalloys | Hot-section components, high-temperature fasteners, turbine and furnace parts | Solution treatment Age hardening | 1,050–1,300°C | High vacuum or high-purity inert gas; partial-pressure operation may limit evaporation of volatile elements | Controlled gas cooling, air cooling, or staged cooling depending on alloy and desired precipitate structure | High-temperature strength, creep resistance, and oxidation resistance | Temperature uniformity is especially important near the solidus temperature. Excessive heat can cause incipient melting, while insufficient cooling can alter precipitation behavior. |
| Cobalt-Based Heat-Resistant Alloys | Wear-resistant and high-temperature components | Solution annealing Stabilizing or aging treatment | 1,050–1,250°C | Vacuum or high-purity inert atmosphere; use clean, non-reactive fixtures | Gas cooling or controlled furnace cooling based on the specification | Improve high-temperature stability, wear resistance, and service life | Control of carbon, carbide distribution, and grain size is important. The furnace should provide stable temperature control across the full load. |
| Aluminum Alloys | Heat-treatable structural aluminum components | Solution heat treatment Quenching and artificial aging | 450–550°C solution treatment; 120–200°C aging | Air or inert atmosphere is commonly preferred; vacuum is mainly selected for special contamination-sensitive applications | Rapid gas or liquid quench according to the alloy and section thickness | Increase strength through precipitation hardening | Aluminum has a narrow solution-treatment window. Excessive temperature can cause incipient melting, while slow quenching can reduce achievable strength. |
| Copper and Copper Alloys | Electrical contacts, tooling, heat exchangers, and conductive components | Annealing Stress relief or solution treatment | 300–900°C | Vacuum or inert gas where oxidation and surface discoloration must be minimized | Furnace cooling, air cooling, or controlled inert-gas cooling | Restore ductility, reduce residual stress, and maintain surface cleanliness | Some copper alloys contain volatile or oxidation-sensitive elements. Select the atmosphere and cooling rate based on alloy composition and electrical requirements. |
| Cemented Carbide and Hardmetal Assemblies | Cutting inserts, wear components, and composite tooling | Vacuum brazing Stress-relief heating | 600–1,100°C, depending on filler metal | High vacuum or inert atmosphere suitable for the selected brazing filler | Controlled furnace cooling to limit thermal shock and residual stress | Join carbide to steel or other substrates without oxidation or flux residue | Match thermal expansion between joined materials. Joint clearance, filler-metal melting range, and heating rate strongly affect joint quality. |
| Powder-Metal and Additively Manufactured Steels | Tooling inserts, lattice structures, and near-net-shape steel parts | Vacuum stress relief Hardening and tempering | 300–1,100°C, depending on alloy and process route | Vacuum or inert atmosphere; low residual oxygen and moisture are important for porous or finely featured parts | Controlled gas cooling, furnace cooling, or staged cooling | Reduce residual stress, control porosity-related distortion, and achieve target hardness | Part geometry, density gradients, and build orientation can affect distortion. Use representative test coupons to validate the complete thermal cycle. |