Integrally Woven 3D Preform with Off-Axis Stiffeners

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Solution Overview

Problem

Existing reinforced composite materials face limitations in creating strong, lightweight structures that can withstand high out-of-plane loads and require complex geometric shapes, with prior methods either relying on weak adhesive joints or mechanical coupling that adds weight and introduces thermal expansion issues.

Innovation Solution

An integrally woven preform with stiffeners in multiple directions, such as 0°, ±60°, and ±45°, is developed using a conventional loom, where fibers exchange positions to create a hexagonal or diamond pattern, enhancing structural integrity and allowing for the formation of complex shapes without the need for adhesives or mechanical fasteners.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If adhesive joints or mechanical fasteners are used to join reinforcement preforms, then the structural integrity and strength are improved, but the weight increases and thermal expansion issues are introduced

Engineering Contradiction:
Improvestructural integrityVSAvoidcomponent weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent merges multiple reinforcement preforms into a single integrated woven structure with interlaced fibers. The fibers from different preforms are interwoven together at the joints, creating a unified composite structure that eliminates the need for separate adhesive joints or mechanical fasteners, thereby reducing weight while maintaining structural integrity

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The patent uses composite fiber structures where reinforcement fibers from multiple preforms are interlaced and combined with matrix material. This composite approach allows the joint regions to have enhanced properties through the intermingling of fibers from different directions, providing both strength and weight efficiency

Inventive Principle:
Principle #40Composite materials

2Strength

If adhesive joints are used to join reinforcement preforms, then the structural integrity is improved, but thermal expansion mismatches and reliability issues occur

Engineering Contradiction:
Improvejoint strengthVSAvoidthermal stability
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The patent merges multiple reinforcement preforms into a single integrated woven structure with interlaced fibers. The fibers from different preforms are interwoven together at the joints, creating a unified composite structure that eliminates the need for separate adhesive joints or mechanical fasteners, thereby reducing weight while maintaining structural integrity

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The patent achieves homogeneity by interlacing fibers from multiple preforms together, creating a uniform distribution of reinforcement materials at the joint regions. This homogeneous fiber arrangement ensures consistent thermal and mechanical properties throughout the structure, eliminating thermal expansion mismatches that would occur with heterogeneous adhesive joints

Inventive Principle:
Principle #33Homogeneity

3Adaptability or versatility

If complex geometric shapes are created using multiple joined preforms, then the shape adaptability is improved, but the manufacturing complexity and number of joints increase

Engineering Contradiction:
Improveshape complexityVSAvoidmanufacturing complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent applies segmentation by creating a modular woven structure where different sections of the composite can be independently designed and manufactured. The interlaced fiber architecture allows the structure to be divided into functional segments while maintaining continuity through the interwoven fiber paths, enabling complex shapes without requiring multiple separate joints

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent uses another dimension by implementing fiber interlacing in the through-thickness direction. This three-dimensional fiber arrangement allows the structure to achieve complex geometric shapes and structural features without requiring additional joints in the planar directions, thereby reducing manufacturing complexity while maintaining shape adaptability

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

4Ease of manufacture

If conventional loom weaving is used to create multi-directional stiffeners, then the manufacturing ease is improved, but achieving off-axis reinforcement patterns is difficult

Engineering Contradiction:
Improveweaving simplicityVSAvoidstiffener orientation
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The patent applies dynamics by implementing a flexible fiber routing system where fibers can change direction and orientation dynamically throughout the weaving process. This allows the conventional loom to produce off-axis reinforcement patterns by dynamically adjusting fiber paths during weaving, maintaining manufacturing simplicity while achieving versatile stiffener orientations

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent uses parameter changes by varying the weaving pattern parameters to achieve different stiffener orientations. By changing the interlacing sequence, fiber angles, and weave density parameters during the weaving process, the conventional loom can produce off-axis reinforcement patterns without requiring complex mechanical modifications to the loom itself

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentEP2382082B1Woven preform with integral off axis stiffeners
Publication Date: 2021.06.16 ALBANY ENGINEERED COMPOSITES INC
  • EP2382082B1 patent drawingFigure 1~2
  • EP2382082B1 patent drawingFigure 3
  • EP2382082B1 patent drawingFigure 4

AI summary

An integrally woven three-dimensional preform with stiffeners in two or more directions constructed from a woven fabric having a first, second and optional third woven fabric layer. A plurality of yarns are interwoven over a region between the first and second fabric layers such that the first fabric layer is foldable relative to the second fabric layer. An additional plurality of yarns are interwoven over a region between the second and third fabric layers such that the third fabric layer is foldable relative to the second fabric layer. Upon folding of the woven fabric layers, the integrally woven three-dimensional preform with stiffeners in two or more directions is formed.