CFRP Sandwich Structure Weight Reduction via Direct Resin Bonding

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Solution Overview

Problem

Existing sandwich structures used in small aircraft, such as air mobility vehicles, have a high weight due to the thickness of the fiber-reinforced plastic (FRP) layers, which hinders further weight reduction.

Innovation Solution

A sandwich structure comprising at least one first ply and one second ply of carbon fiber reinforced plastic (CFRP) with a honeycomb or foam core, where the CFRP plies have a thickness of 0.05 mm to 0.15 mm and the thermoset resin acts as an adhesive directly bonded to the core without interposing any other layer.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If the thickness of FRP layers is increased to maintain mechanical strength, then the strength is improved, but the weight increases

Engineering Contradiction:
Improvemechanical strengthVSAvoidweight of sandwich structure
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent applies parameter changes by optimizing the thickness of FRP layers to a specific range (0.05-0.15mm) and controlling the resin content (30-70 mass%) to achieve the optimal balance between mechanical strength and weight reduction. This quantitative parameter optimization allows the structure to maintain sufficient strength while minimizing weight.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent uses composite materials by combining carbon fiber reinforced plastic (CFRP) with a honeycomb core structure. The CFRP layers are bonded directly to the honeycomb core using thermoset resin, creating a composite sandwich structure that achieves high strength-to-weight ratio by leveraging the strength of both the fiber-reinforced plastic and the lightweight core.

Inventive Principle:
Principle #40Composite materials

2Reliability

If adhesive layers are added to bond FRP to core, then the bonding reliability is improved, but the weight increases

Engineering Contradiction:
Improvebonding reliabilityVSAvoidweight of sandwich structure
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent extracts and eliminates the separate adhesive layer from the bonding system. Instead of using a dedicated adhesive layer between the FRP and honeycomb core, the thermoset resin within the FRP itself is used for bonding, thereby removing the unnecessary intermediate layer and reducing weight while maintaining bonding reliability.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The thermoset resin in the FRP serves dual functions: as the matrix material providing structural integrity and as the adhesive bonding the FRP to the honeycomb core. This multi-functionality eliminates the need for separate adhesive layers, reducing weight while maintaining reliable bonding.

Inventive Principle:
Principle #6Universality (Multi-functionality)

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 configuration achieves a significant weight reduction of the sandwich structure while maintaining sufficient mechanical properties, making it suitable for use in small aircraft as a structural material.

Implementation Method 1

The first thermoset resin is directly bonded to the core without interposing any other layer between the first thermoset resin and the core. The second thermoset resin is directly bonded to the core without interposing any other layer between the second thermoset resin and the core.

Methodology Applied
Scientific EffectAdhesion: Adhesive

Implementation Method 2

heating and curing first uncured thermoset resin with the first uncured thermoset resin in direct contact with one side of the core so that the first cured thermoset resin is directly bonded to the one side of the core

Methodology Applied
Scientific EffectCuring: Heat Treatment

Data Source

PatentUS20250065595A1Sandwich structure, method of producing sandwich structure, and aircraft
Publication Date: 2025.02.27 SUBARU CORP
  • US20250065595A1 patent drawing
  • US20250065595A1 patent drawing
  • US20250065595A1 patent drawing

AI summary

A sandwich structure includes a first ply of CFRP, a second ply of CFRP and a honeycomb or foam core. The first ply of the CFRP includes first carbon fibers and thermoset resin which is matrix reinforced with the first carbon fibers. The second ply of the CFRP includes second carbon fibers and thermoset resin which is matrix reinforced with the second carbon fibers. The core is sandwiched between the first and second plies of the CFRP. Ply thicknesses of the first and second plies of the CFRP are each not less than 0.05 mm and not more than 0.15 mm. The first thermoset resin is directly bonded to the core without interposing any other layer between the first thermoset resin and the core. The second thermoset resin is directly bonded to the core without interposing any other layer between the second thermoset resin and the core.