Key to Metals AG (Datenlieferant)
Titanium Ti-6Al-4V (SAE)
Weitere Informationen finden Sie hier.
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Einsatzbeispiele
- For parts of intricate design requiring a combination of good strength-to-weight rate and corrosion resistance, but usage is not limited to such applications.
- For parts to be rough machined prior to solution and precipitation heat treatment and for parts, such as pressure vessels and other aerospace structures, requiring high strength-to-weight ratios at or near room temperature, but usage is not limited to such applications
- For structurally cast components requiring a combination of good strength-to-weight ratio and corrosion resistance, but usage is not limited to such applications
- Primarily for highly-stressed parts, such as rotating parts in gas turbine engines, requiring high strength in the annealed condition.
- The high-strength titanium alloy castings covered by this specification are intended for use in airframe, missile and other applications where sound lightweight castings are required.
- These castings have been used typically for parts of intricate design requiring a combination of good strength-to-weight ratio and corrosion resistance up to 550°F (288°C), but usage is not limited to such applications.
- These castings have been used typically for parts of intricate design requiring a combination of good strength-to-weight ratio, creep and fatigue properties, and corrosion resistance up to 750°F (399°C), but usage is not limited to such applications
- These compacts have been used typically for light weight nuts ("B-nuts") used for connecting fluid lines to fittings and to equipment, and for other small high-quantity miscellaneous hardware, but usage is not limited to such applications.
- These forgings have been used typically for parts that do not require heat treatment but require high mechanical properties in the annealed condition and for which processing above the beta transus is permissible, but usage is not limited to such applications. This alloy exhibits high strength-to-weight ratios up to 399°C (750°F)
- These products have been used typically for complex-shaped powdered metal products made to near net shape dimensions with properties similar to wrought products, but usage is not limited to such applications.
- These products have been used typically for parts requiring moderate strength with a maximum service temperature in the 399 to 510°C range depending on time at temperature where the product is to be used in the annealed condition, but usage is not limited to such applications.
- These products have been used typically for parts requiring strength up to 399°C (750°F), but usage is not limited to such applications.
- These products have been used typically for parts requiring strength up to 750°F (400°C), but usage is not limited to such applications.
- These products have been used typically for parts that do not require heat treatment but require high mechanical properties in the annealed condition and for which processing above the beta transus is permissible, but usage is not limited to such applications. This alloy exhibits high strength-to-weight ratios up to 750°F (399°C).
- These products have been used typically for parts that require high mechanical properties and are machined from product in the heat treated condition, but usage is not limited to such applications. This alloy exhibits high strength-to-weight ratios up to 750°F (399°C).
- These products have been used typically for parts which are machined after being solution heat treated and aged, and are suitable for parts requiring high strength-to-weight ratios at or near room temperature, but usage is not limited to such applications.
- These products have been used typically for parts which are machined after solution heat treatment and aging and are suitable for parts requiring high strength-to-weight ratios up to moderately elevated temperatures, but usage is not limited to such application
- These products have been used typically for parts which are machined after solution heat treatment and aging; and are suitable for parts requiring high strength-to-weight ratios up to moderately elevated temperatures, but usage is not limited to such applications.
- This material has been used typically for driver sheet used as a consumable manufacturing aid in superplastic forming of titanium alloy sheet or plate components at 871-927°C (1600-1700°F), but usage is not limited to such applications.
- This material has been used typically for parts to be formed or machined in the solution heat treated condition and subsequently precipitation heat treated requiring high strength-to-weight ratio and stability up to 288°C (550°F) in the precipitation heat treated condition, but usage is not limited to such applications.
- This material has been used typically requiring high strength-to-weight ratio and stability up to 288°C (550°F) in the precipitation heat treated condition in material thicknesses 50.80 mm and under, but usage is not limited to such applications.
- This plate has been used typically for parts in damage-tolerant, stress-corrosion-resistant applications requiring strength up to 399°C, but usage is not limited to such applications.
- This powder has been used typically for compaction into net or near net shapes and into forging stock in the form of billets or preforms, but usage is not limited to such applications.
- This product has been used typically for machining and forging preforms in applications that require static mechanical properties similar to wrought mill and recrystallized annealed products, but usage is not limited to such applications.
- This wire has been used typically as filler metal for gas-metal-arc and gas-tungsten-arc welding of titanium with chemistry matched to weld standard grade Ti 6Al-4V alloy, but usage is not limited to such applications.
- Used typically for parts to be rough machined prior to solution and precipitation heat treatment and for parts requiring high strength-to-weight ratios at or near room temperature, but usage is not limited to such applications.
Abdeckungen; Antriebe; Bauwesen; Chemieindustrie; Fördertechnik; Formteile; Mechanik; Öl und Gas; Raumfahrt; Textilindustrie
Physikalische Eigenschaften
| Name | Wert | Messverfahren und -bedingungen |
|---|---|---|
| Dichte | > 4.346 kg/dm³ | |
| Mechanische Eigenschaften | ||
| 0,2-%-Streckgrenze bei Zugbeanspruchung | 722.6 – 1180.7 MPa | |
| Schlagenergie | > 19 J | |
| Schubmodul | 42 – 51 GPa | |
| Zug-Elastizitätsmodul | 110 – 133 GPa | |
| Zugdehnung beim Bruch | > 3 % | |
| Zugfestigkeit | > 827 MPa | |
| Elektrische und magnetische Eigenschaften | ||
| spezifischer elektrischer Widerstand | 0.016 – 1.76 Ω∙mm²/m | |
| Thermische Eigenschaften | ||
| spezifische Wärmekapazität | 557.57 – 565.218 J/(kg∙°C) | |
| Wärmeleitfähigkeit | 6.577 – 7.52 W/(m∙°C) | |
Daten bereitgestellt von
Key to Metals AG
IBDT Ingenieurbüro Daniel Trost
+49 176 703 22 119
Anfrage per E-Mail
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