Hybrid Composites

Combine carbon, glass, or aramid fibers, used in tailored applications like tail assemblies.

Hybrid composites are materials that combine two or more types of reinforcing fibers within a polymer matrix to take advantage of the different properties of each fiber. The goal is to combine the best features of multiple materials to create a composite with tailored performance characteristics. Hybrid composites are becoming increasingly important in aerospace applications due to their versatility, durability, and ability to optimize various mechanical properties.


What Are Hybrid Composites?

Hybrid composites use multiple fiber types (e.g., carbon fiber, glass fiber, aramid fiber, natural fibers) within a single matrix material (often epoxy, polyester, or thermoplastics). The fibers are carefully arranged in a manner that exploits the specific advantages of each material for particular sections of a component. For example, glass fiber may provide better impact resistance, while carbon fiber offers higher stiffness and strength.


How Hybrid Composites Are Used in Commercial Aviation

Hybrid composites are applied in areas where multi-functional performance is required, including:

  • Wing Structures: Hybrid composites can provide a balance between lightweight and impact resistance, making them useful in both primary and secondary wing components.
  • Fuselage Components: Used for parts that need to withstand both tensile strength and impact resistance, like floor panels and sidewalls.
  • Control Surfaces: Hybrid materials can be used in rudders, elevators, and ailerons to provide stiffness and resilience against impacts.
  • Nacelle Components: Hybrid composites are ideal for areas of the engine nacelles that require both lightweight and toughness.
  • Interior Components: Hybrid composites may be used for parts like seating structures, overhead bins, and partition panels, where strength-to-weight ratio and impact resistance are key.
  • Landing Gear Fairings: Hybrid composites offer both strength and the ability to dissipate impact energy when subjected to debris strikes.

Advantages of Hybrid Composites in Aviation

  • Optimized Properties: Hybrid composites offer a combination of strength, toughness, impact resistance, stiffness, and light weight—all tailored to specific needs.
  • Reduced Cost: By combining high-performance fibers (like carbon fiber) with lower-cost fibers (like glass fiber), manufacturers can reduce costs while maintaining performance.
  • Improved Impact Resistance: Glass and aramid fibers (like Kevlar) are often added to hybrid composites to improve toughness and resilience under impact or crash conditions.
  • Weight Reduction: Hybrid composites allow for the use of less-expensive fibers where high strength is less critical, reducing overall weight compared to using only high-performance fibers.
  • Manufacturing Flexibility: Hybrid composites can be customized for specific applications based on fiber orientation and stacking sequences.

Disadvantages of Hybrid Composites in Aviation

  • Complex Manufacturing: Manufacturing hybrid composites requires a more complex process due to the need to manage different fiber types and their behaviors.
  • Increased Repair Complexity: Repairing hybrid composite materials can be challenging because different fibers may require different repair methods.
  • Cost Considerations: While hybrid composites are cheaper than using pure high-performance fibers, they are still more expensive than traditional materials like aluminum or steel.
  • Fatigue Resistance: The fatigue resistance of hybrid composites can sometimes be lower than that of pure high-performance composites like CFRP, especially if the fiber mismatch leads to stress concentrations.

Fiber Combinations in Hybrid Composites

Different fiber combinations in hybrid composites allow for performance optimization depending on the specific design needs. Some common combinations include:

  • Carbon Fiber + Glass Fiber: Often used when lightweight and strength are both necessary but at a lower cost than pure CFRP.
  • Carbon Fiber + Aramid Fiber (Kevlar): Used for high impact resistance and toughness, especially in areas exposed to potential bird strikes or ground impacts.
  • Glass Fiber + Aramid Fiber: Typically used for parts that need impact resistance but do not need the stiffness of carbon fiber.
  • Natural Fibers + Carbon or Glass Fiber: In some eco-friendly designs, natural fibers like hemp, flax, or sisal may be combined with carbon or glass fibers to create a lightweight, strong, and sustainable hybrid composite.

Applications of Hybrid Composites in Aircraft

  • Boeing 787 Dreamliner: Some secondary structures, like wing fairings, use hybrid composite materials to balance lightness and resilience.
  • Airbus A350: Hybrid composites can be found in the interior components (e.g., seats, walls) as well as in some nacelle parts.
  • Bombardier Global 7500: In corporate jets, hybrid composites are used to create a balance of lightweight and stiffness, especially in interior furnishings and access panels.

Key Properties and Performance Characteristics of Hybrid Composites


Challenges in Hybrid Composite Use

  1. Design Complexity: Tailoring fiber orientations and ply stacking to optimize strength in one direction while maintaining flexibility in another requires advanced computational methods.
  2. Cost Management: Balancing performance and cost is key, especially in commercial aviation where operating cost savings are critical.
  3. Repairability: Different fibers within a hybrid composite may require different repair techniques, complicating field repairs and in-service maintenance.
  4. Quality Control: Consistent quality across different fiber types and layered laminates can be challenging.

Future Trends in Hybrid Composites

  • Bio-Composites: Hybrid composites incorporating natural fibers combined with carbon or glass fibers could lower environmental impact and provide sustainable alternatives.
  • Smart Hybrid Composites: Incorporating sensor systems or self-healing fibers to enhance monitoring and maintenance.
  • Improved Recycling Methods: The development of recyclable hybrid composite systems could contribute to reducing the environmental footprint.
  • Autonomous Manufacturing: Advances in automated fiber placement and robotic layups will simplify the manufacturing of hybrid composites, improving their cost-effectiveness.

Summary

Hybrid composites combine the best qualities of different fibers, creating materials that are strong, tough, lightweight, and cost-effective for various applications in aviation. They are primarily used in non-critical structures, interior components, and parts that need to balance multiple performance criteria like impact resistance, strength, and flexibility.

As technologies improve, hybrid composites are poised to play a larger role in lightweight aircraft structures, eco-friendly materials, and next-generation aviation innovations.

PropertyHybrid Composites
Tensile StrengthModerate to high, depending on fiber choice
Stiffness (Elastic Modulus)High (for CFRP) or moderate (for GFRP/aramid combinations)
Impact ResistanceHigh (especially with aramid fibers)
Fatigue ResistanceModerate to high
Density1.5 – 2.0 g/cm³ (depending on fiber mixture)
Manufacturing ComplexityHigh (due to mixed fibers)
CostModerate, less than pure CFRP but more than metals
Environmental ImpactPotential for bio-based fibers in hybrid combinations

Parts that are made of or use Hybrid Composites

Part Number Name Alt Part Number ATA Chapter Cage Code NSN Rotable Repair Stations Suppliers

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