• it
  • en

Materials

Titanium Commercially Pure

Range of application

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.

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