| AISI H13 / 1.2344 | Hot-work tool steel | Vacuum hardening and tempering | 1,010–1,030°C | Approximately 20–30 minutes after equalization | 10−2–10−4 mbar | High-pressure gas quench; commonly nitrogen | Use staged preheating to reduce thermal gradients. Double tempering is commonly applied, often around 540–650°C depending on hardness and toughness targets. |
| AISI D2 / 1.2379 | Cold-work tool steel | Vacuum hardening and double tempering | 1,020–1,050°C | Approximately 20–30 minutes after equalization | 10−2–10−4 mbar | High-pressure gas quench; oil quench may be specified for heavy sections | High carbon and chromium content can promote retained austenite. Cryogenic treatment may be used in selected specifications, followed by tempering. |
| AISI M2 / 1.3343 | High-speed steel | Vacuum hardening with multiple tempering | 1,180–1,230°C | Approximately 60–90 seconds per 25 mm after equalization | 10−3–10−5 mbar | Rapid high-pressure gas quench; interrupted cooling can be used for distortion control | The high austenitizing temperature requires accurate control and effective load shielding. Triple tempering is commonly used for dimensional stability. |
| AISI M42 / 1.3247 | Cobalt high-speed steel | Vacuum hardening and multiple tempering | 1,160–1,210°C | Approximately 60–90 seconds per 25 mm after equalization | 10−3–10−5 mbar | High-pressure gas quench with controlled cooling through the transformation range | Maintain a clean vacuum and avoid excessive surface reaction. Tempering is normally performed more than once to reduce retained austenite and stabilize hardness. |
| AISI S7 / 1.2709-type shock-resistant grades | Shock-resistant tool steel | Vacuum hardening and tempering | 1,000–1,030°C | Approximately 20–30 minutes after equalization | 10−2–10−4 mbar | Gas quench sized for section thickness and distortion limits | A lower end of the austenitizing range generally supports toughness, while the higher end may increase hardness. Temper promptly after quenching. |
| AISI T1 / 1.3355 | Tungsten high-speed steel | Vacuum hardening and multiple tempering | 1,190–1,230°C | Approximately 60–90 seconds per 25 mm after equalization | 10−3–10−5 mbar | Rapid high-pressure gas quench | Use precise temperature measurement near the load. Excessive soak can increase grain growth and undesirable carbide dissolution. |
| Commercially Pure Titanium, Grades 1–2 | Titanium | Vacuum stress relief or annealing | 550–760°C | Approximately 30–120 minutes, depending on section size | 10−3–10−5 mbar | Furnace cooling or controlled gas cooling | Titanium readily reacts with oxygen, nitrogen, and hydrogen at elevated temperature. Use clean, dry vacuum conditions and limit exposure at high temperature. |
| Ti-6Al-4V, Grade 5 | Alpha-beta titanium alloy | Stress relief or sub-transus annealing | 700–800°C | Approximately 60–120 minutes | 10−3–10−5 mbar | Air cooling, controlled gas cooling, or furnace cooling according to specification | For conventional annealing, avoid exceeding the beta-transus region unless a specialized solution treatment is intended. Surface color and oxygen pickup should be monitored. |
| Ti-6Al-4V ELI, Grade 23 | Medical-grade titanium | Stress relief or annealing | 650–800°C | Approximately 60–120 minutes | 10−4–10−5 mbar | Controlled gas cooling or furnace cooling | Use stricter contamination control than for general-purpose work. Surface chemistry and alpha-case formation can be critical for fatigue-sensitive components. |
| Ti-6246 | High-strength alpha-beta titanium alloy | Stress relief or duplex annealing | 700–900°C | Approximately 60–120 minutes | 10−4–10−5 mbar | Controlled gas cooling; follow the alloy-specific specification | The selected cycle influences strength, ductility, and transformed beta morphology. Avoid uncontrolled oxygen or nitrogen ingress during heating and cooling. |
| Ti-5Al-2.5Sn | Near-alpha titanium alloy | Stress relief or annealing | 700–850°C | Approximately 60–120 minutes | 10−4–10−5 mbar | Furnace cooling or controlled gas cooling | Temperature uniformity is important for dimensional stability. Confirm allowable surface oxygen content when the component is used in fatigue-critical service. |
| Ti-3Al-2.5V | Alpha-beta titanium alloy | Stress relief or annealing | 650–800°C | Approximately 30–90 minutes | 10−3–10−5 mbar | Air cooling or controlled gas cooling | Commonly processed below the beta-transus temperature. Minimize handling contamination and use clean fixtures compatible with titanium. |