Composite Honeycomb Part Structure With Braided Sock Reinforcement
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Existing manufacturing methods for composite material parts with honeycomb structures, particularly in turbomachines, face challenges in achieving optimal thermomechanical performance, aerodynamic efficiency, and cost-effectiveness, especially with issues related to bonding lines, draping complexity, and mechanical weaknesses at cell wall junctions.
Innovation Solution
A manufacturing process involving a combination of a braided continuous fibrous reinforcement sock and discontinuous long fibers, where the sock is draped around removable cores to form a honeycomb structure, followed by thermocompression to densify the assembly, ensuring fiber continuity and improved mechanical performance.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Productivity
If thermoplastic injection molding is used for honeycomb structures, then production speed and volume are improved, but mechanical performance is limited and bonding line management becomes complex
Solution Approach 1:
The patent uses a hybrid composite structure combining continuous braided fibers for the sock and discontinuous long fibers for the strip. This composite approach allows the material to exhibit both the drapability needed for complex honeycomb geometries and the mechanical strength required for high-performance applications, resolving the contradiction between production feasibility and mechanical performance.
Solution Approach 2:
The patent applies different fiber configurations to different locations: continuous braided fibers in the sock provide structural integrity and fiber continuity at junctions, while discontinuous long fibers in the strip provide drapability for complex shapes. This local differentiation allows each region to contribute its optimal properties to the final part performance.
2Strength
If thermocompression molding with pre-laminated continuous fibers is used, then mechanical performance is improved, but manufacturing complexity and cost increase due to individual cell draping
Solution Approach 1:
The patent segments the fibrous reinforcement into two functional components: the braided sock that forms the honeycomb cell walls and the strip that reinforces specific areas. This segmentation allows the sock to be formed as a single continuous piece using simple braiding, avoiding the need to drape each cell individually while still achieving high mechanical performance through the combination with the strip.
Solution Approach 2:
The braided sock acts as an intermediary structure that simplifies the manufacturing process. Instead of directly draping complex pre-laminated sheets over each cell, the sock provides a pre-formed, flexible substrate that can be easily manipulated and positioned, reducing the overall manufacturing complexity while maintaining structural integrity.
3Ease of manufacture
If thermocompression molding with discontinuous long fibers is used, then manufacturing cost is reduced and complex shapes are achieved, but material property variability increases and pull-out problems occur
Solution Approach 1:
The patent merges two fiber types into a single hybrid structure: continuous braided fibers in the sock provide consistent structural properties and fiber continuity at junctions, while discontinuous long fibers in the strip contribute to cost reduction and shape complexity. This merging allows the continuous fibers to compensate for the variability inherent in discontinuous fibers, maintaining reliability while achieving cost benefits.
Solution Approach 2:
The hybrid composite structure combines the advantages of both continuous and discontinuous fibers. The continuous braided sock ensures consistent mechanical properties and prevents pull-out at junctions, while the discontinuous strip reduces manufacturing cost and enables complex shapes. Together, they create a material system that is both reliable and cost-effective.
4Shape
If thin cell walls are used for aerodynamic performance, then aerodynamic efficiency is improved, but mechanical strength decreases
Solution Approach 1:
The hybrid composite structure enables thin cell walls to achieve both aerodynamic efficiency and mechanical strength. The continuous braided sock provides a consistent structural framework that maintains integrity at thin sections, while the discontinuous long fibers in the strip reinforce critical areas, allowing the cell walls to be made thin for aerodynamic performance without sacrificing mechanical strength.
Solution Approach 2:
The patent applies reinforcement locally where needed: the strip of discontinuous long fibers is positioned to reinforce specific areas of the honeycomb structure, while the continuous braided sock provides uniform structural support throughout. This local quality approach allows thin cell walls in non-critical areas for aerodynamic efficiency while maintaining strength in critical regions through targeted reinforcement.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
The process results in parts with enhanced mechanical strength, reduced vibrations, and improved aerodynamic performance while being cost-effective and simpler to produce, avoiding issues related to handling and draping complexity.
Implementation Method 1
a step of thermocompression of the assembly installed in the mold
Data Source
Figure 1~3
Figure 4~5
Figure 6~8
AI summary
The invention relates to a method for manufacturing a composite material part comprising a cellular structure which comprises at least one cell (21) delimited by walls, the method comprising: supplying at least a first core (40, 40a, 40b), providing a web of a first fibrous reinforcement comprising a plurality of long discontinuous fibres randomly distributed in a plane, producing at least one strip (50a) of the first fibrous reinforcement, producing a second fibrous reinforcement in the shape of a sock, inserting the first core into the sock, draping the strip (50a) around the sock containing the first core, placing the sock containing the first core and the wrapped strip in a mould (60), and thermocompression.