Composite Preform Figuring with Overlapping Fibers

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Solution Overview

Problem

Existing methods face challenges in shaping composite materials with large curved surfaces due to difficulties in bending flat planar fibrous preparations without forming gaps, which can reduce the strength and dimensional accuracy of the final composite material.

Innovation Solution

A preform figuring method involving a figuring die with curved surfaces, where sheet-shape fibrous preparations are stacked and bent with overlapping layers to prevent gap formation, ensuring continuous fiber reinforcement and uniform thickness, and the use of thermosetting resin impregnation and heat-curing to shape the composite material.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Shape

If flat planar fibrous preparations are bent to form large curved surfaces, then the composite material can achieve curved shapes, but gaps form between layers reducing strength and dimensional accuracy

Engineering Contradiction:
Improvecurved surface shapeVSAvoiddimensional accuracy
Core Design Contradiction:
ShapeVSManufacturing precision

Solution Approach 1:

The fibrous preparation is divided into multiple sheet layers, with each layer being bent and positioned separately on the figuring die. This segmentation allows precise control of each layer's position and curvature, preventing gap formation while achieving the desired large curved surface shape.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention transitions from bending a single flat sheet to stacking and bending multiple sheets in three-dimensional space. By utilizing the stacking dimension, the method achieves complex curved surfaces while maintaining layer continuity and preventing gaps through overlapping edges.

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

2Shape

If sheet-shape fibrous preparations are stacked and bent onto curved surfaces, then curved composite materials can be formed, but fiber tension increases reducing material strength

Engineering Contradiction:
Improvecurved surface shapeVSAvoidfiber strength
Core Design Contradiction:
ShapeVSStrength

Solution Approach 1:

Dividing the fibrous preparation into multiple sheets allows each individual sheet to be bent with smaller curvature radius, reducing the fiber tension experienced by each layer. The segmented approach distributes the bending stress across multiple layers rather than concentrating it in a single thick layer.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The figuring die provides a curved surface that guides the bending of each sheet layer. By using the die's curved geometry, the fibers are bent along a controlled path that minimizes excessive tension while achieving the desired curved shape.

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Manufacturing precision

If multiple sheet-shape fibrous preparations are stacked with overlapping layers, then gap formation is prevented, but the manufacturing process complexity increases

Engineering Contradiction:
Improvegap preventionVSAvoidstacking process complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The fibrous preparation is segmented into multiple sheets that are stacked sequentially on the figuring die. Each sheet is positioned and bent individually, allowing precise control over layer alignment and overlap, which prevents gaps while maintaining a manageable manufacturing process.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The sheets are pre-cut and pre-positioned on the figuring die before bending. This preliminary arrangement of sheets with planned overlapping edges simplifies the subsequent bending process and ensures gap prevention without requiring complex real-time adjustments during manufacturing.

Inventive Principle:
Principle #10Preliminary action

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

This method enables the creation of composite materials with large curved surfaces without excessive fiber tension or gap formation, enhancing the strength and dimensional accuracy of the final product, particularly suitable for aircraft structural parts.

Implementation Method 1

shaping the composite material by impregnating the dry preform with the thermosetting resin and then heat-curing the thermosetting resin

Methodology Applied
Scientific EffectHeat-curing: Phase Change

Data Source

PatentUS11453181B2Preform figuring method, composite material shaping method, composite material, and aircraft structural part
Publication Date: 2022.09.27 SUBARU CORP
  • US11453181B2 patent drawing
  • US11453181B2 patent drawing
  • US11453181B2 patent drawing

AI summary

A preform figuring method includes mounting and stacking sheet-shape fibrous preparations that have been or are yet to be impregnated with a thermosetting resin on a figuring die that has first and second figuring surfaces at least either one of which is a curved surface and making a preform for a composite material which has a curved surface that corresponds to the curved surface of the figuring die as a stack of the fibrous preparations which has layers by bending the fibrous preparations mounted on the first figuring surface onto the second figuring surface. At least a fraction of the layers that constitute the stack are formed by mounting sheet-shape fibrous preparations on the first figuring surface or the fibrous preparation adjacent in a stacking direction so that the fibrous preparations partly overlap and bending portions of the fibrous preparations mounted so as to overlap onto the second figuring surface.