- Graphites
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- C-C Composites
- 2D
- 2D Carbon-Carbon Composite Sheets and Plates
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3D Carbon-Carbon Composite Materials
BZNCarbon offers high-density 3D carbon-carbon composites with exceptional strength and thermal stability. Ideal for aircraft brakes and structural parts exposed to extreme heat.
Category: C-C Composites
Tag: 3D Carbon-Carbon Composite Materials
Description
BZNCarbon’s 3D carbon-carbon composite (C/C) materials are advanced carbon fiber-reinforced carbon structures built to meet the needs of industries where strength, heat resistance, and longevity are essential. Unlike 2D composites that rely solely on fibers in two planar directions, 3D C/C composites incorporate reinforcement in all three axes (X, Y, Z), enabling them to withstand complex thermal and mechanical stresses.
Available in standard and custom geometries—including disks, plates, and blocks—our 3D C/C composites can also be tailored using various weave architectures such as XYZ woven, axial-radial-hoop (also known as hoop 3D), or as per your proprietary design.
BZNCarbon is one of the few producers capable of achieving a minimum bulk density of 1.90 g/cm³, thanks to specialized HIP equipment, significantly enhancing the strength-to-weight performance.
What Is 3D Carbon-Carbon Composite?
3D C/C composite is a high-strength, high-temperature resistant material composed of carbon fibers embedded in a carbon matrix. The fiber orientation covers all three spatial axes, delivering isotropic mechanical reinforcement and increasing fracture toughness, dimensional stability, and thermal fatigue resistance.
This structural configuration allows for longer service life, improved heat distribution, and better resistance to internal cracking under thermal cycling or impact loads—particularly in aerospace braking systems and industrial high-heat environments.
Applications
Aircraft Braking Systems (civil and defense-grade)
Rocket Propulsion and Nozzle Components
High-Temperature Furnace Fixtures
Aerospace Insulation and Structural Linings
Heat Shields for Industrial or Space Systems
Thermal Protection Panels and Support Blocks
Aviation and Motorsport Disc Brakes
Key Technical Specifications
Property | Direction | Requirement | Typical Result |
---|---|---|---|
Bulk Density | — | ≥ 1.85 g/cm³ | 1.868 g/cm³ |
Fiber Configuration | — | 3D (X, Y, Z) | 3D (X, Y, Z) |
Tensile Strength | X-Y / Z | ≥130 MPa / ≥70 MPa | 161 MPa / 76 MPa |
Tensile Modulus | X-Y / Z | ≥50 GPa / ≥30 GPa | 59.1 GPa / 38 GPa |
Flexural Strength | X-Y | ≥120 MPa | 142 MPa |
Compressive Strength | X-Y / Z | ≥160 MPa / ≥220 MPa | 162 MPa / 274 MPa |
Thermal Conductivity (900°C) | X-Y / Z | ≥40 / ≥20 W/m·K | 50 / 22 W/m·K |
Thermal Expansion (at 1000°C) | X-Y / Z | 0.5–1 / 1–1.5 ×10⁻⁶/K | 0.55 / 1.16 ×10⁻⁶/K |
Porosity | — | 3–5% | 4.3% |
Specific Heat Capacity (RT–590°C) | X-Y / Z | Reported Value | 1.569×10³ / 1.620×10³ J/(kg·K) |
X-Ray Inspection | — | No structural defects | Passed |
Custom test reports, X-ray validation, and shape adaptations available upon request.
Advantages
True 3D structure for multi-directional load-bearing capacity
High thermal conductivity and resistance to thermal shock
Ultra-low thermal expansion ensures shape integrity
Lightweight yet mechanically superior to traditional metals
Extremely low porosity and high purity
Stable under vacuum, inert gas, and oxidative conditions
Engineered for extended service life in critical systems