WINDFORM® XT 2.0

Category: Nylon, Unspecified , Polyamide
Manufacturer: CRP Technology s.r.l.
Trademark: WINDFORM®
Fillers: -
Ports: Qinzhou, Shekou, Shanghai, Ningbo
Delivery Terms FOB, CIF, DAP, DAT, DDP
PDF: gMukYQ_WINDFORM-XT-2-0.pdf
PRICE: ​Order Products​ email   sales@su-jiao.com
Wechat: WECHAT
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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
General Information
Filler / Reinforcement
  • Carbon Fiber
Features
  • Durable
  • Good Strength
Uses
  • Aerospace Applications
  • Automotive Applications
  • Prototyping
Agency Ratings
  • EC 1907/2006 (REACH)
Appearance
  • Black
Forms
  • Powder
Processing Method
  • 3D Printing, Laser Sintering/Melting
PhysicalNominal ValueUnit
Density (20°C)1.10g/cm³
MechanicalNominal ValueUnitTest Method
Tensile Modulus 8930MPaISO 527-2
Tensile Stress 83.8MPaISO 527-2
Tensile Strain (Break)3.8%ISO 527-2
Flexural Modulus 7340MPaISO 178
Flexural Stress 133MPaISO 178
Flexural Modulus - per density unit 6690MPa/g/cm³
Flexural Strength - per density unit 121MPa/g/cm³
Tensile Modulus - per density unit 8140MPa/g/cm³
Ultimate Tensile Strength - per density unit 76.4MPa/g/cm³
ImpactNominal ValueUnitTest Method
Charpy Notched Impact Strength (23°C)4.7kJ/m²ISO 179
Charpy Unnotched Impact Strength (23°C)22kJ/m²ISO 179
Notched Izod Impact Strength (23°C)5.3kJ/m²ISO 180
Unnotched Izod Impact Strength (23°C)19kJ/m²ISO 180
ThermalNominal ValueUnitTest Method
Heat Deflection Temperature (1.8 MPa, Unannealed)173°CISO 75-2/A
Vicat Softening Temperature 176°CISO 306/A50
Melting Temperature 179°CISO 11357
ElectricalNominal ValueUnitTest Method
Surface Resistivity < 1.0E+8ohmsASTM D257
Volume Resistivity < 1.0E+8ohms·cmASTM D257
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