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4D / 5D Carbon-Carbon Composite Materials
Explore BZNCarbon’s advanced 4D and 5D carbon-carbon composites. Engineered for aerospace, energy, and thermal applications requiring superior strength, density, and temperature resistance.
Category: C-C Composites
Tag: 4D / 5D Carbon-Carbon Composite Materials
Description
BZNCarbon’s 4D and 5D carbon-carbon composites are next-generation materials tailored for the most demanding thermal and structural environments. Unlike traditional 3D carbon-carbon materials, our 4D/5D composites incorporate additional fiber orientations within the plane, offering optimized load distribution and durability.
Manufactured using pitch-based or resin-based matrices and advanced CVI/CVD processes, these composites exhibit outstanding mechanical integrity, density control, and heat resistance. With customizable properties and formats, BZNCarbon’s high-density 4D/5D C/C composites are ideal for mission-critical systems across aerospace, defense, energy, and industrial sectors.
What Are 4D and 5D Carbon-Carbon Composites?
While all C/C materials are inherently three-dimensional (with fiber alignment in the X, Y, and Z axes), 4D and 5D structures introduce one or more additional fiber bundles within the planar directions—such as hoop, radial, or circumferential reinforcements. This enhances in-plane mechanical strength and thermal conductivity without compromising weight.
BZNCarbon can also provide polar-woven or hoop-based 4D composites, where reinforcement follows circular or radial patterns, commonly used in rotating systems or cylindrical thermal barriers.
We produce materials with bulk densities ranging from 1.5 to 1.95 g/cm³, and we are capable of reaching ≥1.90 g/cm³ with specialized isostatic and HIP equipment.
Applications
Aerospace structural components
Rocket motor insulators and throat linings
Brake pads and friction discs for defense or racing
High-temperature molds and tooling
Furnace supports, carriers, and lining systems
Nuclear shielding and containment fixtures
Thermal protection systems for re-entry vehicles
General Specifications (XYZ-based 4D Composites)
Property | Direction | Requirement | Typical Result |
---|---|---|---|
Bulk Density | — | ≥ 1.85 g/cm³ | 1.868 g/cm³ |
Fiber Configuration | — | 4D | 4D |
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 (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 (RT–590°C) | X-Y / Z | Reported | 1.569×10³ / 1.620×10³ J/kg·K |
X-ray Inspection | — | No defects | Passed |
Polar / Hoop-Woven 4D Composite Specifications
Property | Value |
---|---|
Fiber Volume – Total | 40–45% |
Fiber Volume – Hoop Direction | 45% ± 5 |
Fiber Volume – Axial Direction | 36% ± 4 |
Fiber Volume – Radial Direction | 19% ± 4 |
Bulk Density | ≥ 1.90 g/cm³ |
Tensile Strength (Hoop) | ≥ 100 MPa |
Compressive Strength (Hoop) | ≥ 80 MPa |
Compressive Strength (Axial) | ≥ 71 MPa |
Thermal Conductivity (900°C) | ≥ 40 W/m·K (Hoop) / ≥ 22 (Axial) |
Thermal Expansion | < 3.1 ×10⁻⁶ /°C |
Open Porosity | < 5% |
Carbon Content | ≥ 99.9% |
Graphitization Temperature | ≥ 2500 °C |
Advantages
Ultra-high temperature capability (up to 3000°C+ in inert environments)
Highly customizable reinforcement patterns (3D/4D/5D/Hoop/Polar)
Superior resistance to thermal shock and chemical attack
Extended wear life in frictional and structural uses
Lightweight, rigid, and oxidation-resistant structure
Enhanced dimensional stability under dynamic loads