Prototypes, one-off or series parts for the aviation, aerospace and medical industries, for example functional components with an integrated cooling structure, bionically optimized functional components, bone foam with bioanalog structure as bone replacement material, individual biocompatible implants or prostheses with a microcellular structure.
Materials
Titanium Commercially Pure
Range of application
Technical data after recommended heat treatment
|
1 Tensile test according to DIN EN ISO 50125. 2 By using a special heat treatment a higher elongation can be achieved. 3 Preliminary values subject to change or update. |
|
| Yield strength Re1 | 530 - 570 N/mm2 |
| Tensile Strength Rm 1 | 600 - 620 N/mm2 |
| Elongation A 1,2 | 15,5 - 20 % |
| Young's modulus 1 | 110 kN/mm2 |
| Thermal conductivity λ3 | 21 Wm/k |
| Coefficient of thermal expansion 3 | 8,9 · 10-6 K-1 |
Heat treatment
Carry out heat treatment in argon atmosphere. Heat to 1000 °C in 4 hours. Maintain temperature for 1 hour. Let components cool to 70 °C in oven.
Chemical composition
COMPONENT INDICATIVE VALUE (%)
Ti Balance
Fe 0 – 0,30
O 0 – 0,25
C 0 – 0,08
N 0 – 0,03
H 0 – 0,015
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