About |
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Technology: Selective Laser Sintering Windform® XT 2.0 is the evolution of the ground breaking high performance Windform® XT, the carbon fiber reinforced composite material, known for its mechanical properties, which made it particularly suitable in demanding applications such as motorsport sector, aerospace and UAV’s. Windform® XT 2.0 is an innovative material, and will replace the Windform® XT, as the “Top Level” of the current Windform® range. Windform® XT 2.0 improves mechanical properties compared to “traditional” Windform® XT, while maintaining the same workability for Laser Sintering machines in order to better fulfill the needs of Additive Manufacturing required to produce end use parts and prototypes. Windform® XT 2.0 retains the matte black colour of the previous version and features improvements in mechanical properties: +8% in tensile strength, +22% in tensile modulus and +46% increase in elongation at break. Windform XT® 2.0 allows for the creation of accurate, reliable and durable prototypes and is perfect for functional applications. Applications: Windform® XT 2.0 is the high-tech material for Additive Manufacturing chosen by those working in the Motorsport, Automotive (suitable for example for components under the hood, such as intake manifolds and functional cooling ducts), Air (for components UAV, Unmanned Aerial Vehicle) Aerospace (useful also to create prototype satellite, such as the CubeSat) and Design, as it allows applications that are fully functional, as well as bench testing, or testing and racing on the track. Surface Finish: After SLS Process 6.0 Ra µm After finishing 1.8 Ra µm&& |
Product Description | |
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Generic | PA Not specified |
Material Status | Commercial: Active |
Features | Good Rigidity,Durability |
Availabilitys | North America,Asia Pacific,Europe |
Process Methods | 3D Printing, Laser Sintering/Melting |
Technical Data | |||
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PHYSICAL | Nominal value | Unit | Test method |
Density | |||
20℃ | 1.10 | g/cm³ |
MECHANICAL | Nominal value | Unit | Test method |
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Tensile modulus | 8930 | MPa | ISO 527-2 |
per density unit | 8140 | MPa | |
tensile strength | 83.8 | MPa | ISO 527-2 |
Tensile strain | |||
fracture | 3.8 | % | ISO 527-2 |
Bending modulus | 7340 | MPa | ISO 178 |
per density unit | 6690 | MPa | |
bending strength | 133 | MPa | ISO 178 |
per density unit | 121 | MPa | |
Ultimate Tensile Strength(per density unit) | 76.4 | MPa/g/cm³ |
IMPACT | Nominal value | Unit | Test method |
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Charpy Notched Impact Strength | |||
23℃ | 4.7 | kJ/m² | ISO 179 |
Charpy Unnotch Impact strength | |||
23℃ | 22 | kJ/m² | ISO 179 |
Impact strength of cantilever beam notch | |||
23℃ | 5.3 | kJ/m² | ISO 180 |
Notched impact strength of cantilever beam | |||
23℃ | 19 | kJ/m² | ISO 180 |
THERMAL | Nominal value | Unit | Test method |
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Hot deformation temperature | |||
1.8 MPa, unannealed | 173 | ℃ | ISO 75-2/A |
Vicat Softening Temp | |||
A50 | 176 | ℃ | ISO 306/A50 |
Melting temperature | 179 | ℃ | ISO 11357 |
Electrical performance | Nominal value | Unit | Test method |
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Surface resistivity | < 1.0E+8 | ohms | ASTM D257 |
Volume resistivity | < 1.0E+8 | ohms·cm | ASTM D257 |
Notes |
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1. Typical properties: these are not to be construed as specifications. |
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