Carbon Fiber Plate - Twill Weave - Standard Modulus - Matte - 24" x 24" x 13/64"
Carbon Fiber Plate - Twill Weave - Standard Modulus - Matte - 24" x 24" x 13/64"
1
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19
$458.99
20
+
$436.79
Estimated lead time for quantities greater than what is Available Now is expected to be between 2 and 4 weeks.
If there is an Available Now quantity listed above, it indicates our quantity in stock. Orders placed today for this quantity or less are expected to ship the next business day.
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This plate is fabricated via resin infusion and deploys a T700 (or equivalent) carbon fiber. In addition to being stiffer than aluminum carbon fiber plate this thicker version can be machined quite easily and shaped to yield a very interesting aesthetic often seen in knife handles or other products. Other manufacturers have dubbed this plate or ones similar "Artisan". Both sides have a peel ply finish which is matte / textured by default and with a quick cleaning can be bond ready.
Additional Information
| Application | Tooling Plates / Support Structures |
|---|---|
| Materials | Standard Modulus Carbon |
| Pattern | 3k 2X2 Twill Weave |
| Color | Black |
| Finish | Matte / Matte |
| Panel Thickness | 0.210000 |
| Plate / Panel Size | 24" x 24" / 609.6mm x 609.6mm |
| Width | 24.0 |
| Thickness | 0.21 |
| Length | 24 |
| Length (max continuous) | 24.0 |
| Areal Density | 1.663 |
| Volumetric Density | 0.055 |
| Weight | 6.653 |
| Primary Fiber | Toray T700S |
| Primary Resin / Hardener | Rhino 1411/4111 |
Engineering Properties
All laminate properties and mechanical calculations are based on Classical Lamination Theory and should be used as a reference only. Rock West Composites does not guarantee these properties or calculations.
| Avg EX Young's Modulus | 9300000.0 |
|---|---|
| Avg EY Young's Modulus | 9300000.0 |
| GXY Shear Modulus | 600000.0 |
| X Tensile Yield Strength | 103000.0 |
| X Compressive Yield Strength | 89000.0 |
| Y Tensile Yield Strength | 103000.0 |
| Y Compressive Yield Strength | 89000.0 |
| XY Shear Strength | 10627.0 |
| CTEX | 2.00E-06 |
| CTEY | 2.00E-06 |
| Poisson's Ratio vXY | 0.035 |
| Poisson's Ratio vYX | 0.035 |
Note:
- "X" is along the length of a tube, rod, plate, or panel.
- "Y" is around the perimeter of a tube, perpendicular to the length of pultruded parts, or along the width of a plate or panel.
Layup Orientation
408-22 Rev A
| Ply # | Orientation (degrees) | Location |
|---|---|---|
| 1 | All 0/90 | Inside |
- 0° fibers maximize bending stiffness and run along the length of the part. Consider bending a tube over your knee.
- 45° fibers maximize torsional stiffness and are typically plied together in an opposing manner, i.e. ±45°. Consider twisting a tube like a vehicle's driveshaft.
- 90° (or "hoop") fibers maximize crushing stiffness and generally assist in overall durability. Consider laying a tube on the ground and stepping on it.