Flexible Hexagonal Core Element for Sandwich Panel Delamination

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Solution Overview

Problem

The aerospace and rocketry industries face challenges with delamination in sandwich construction panels due to limited bonding areas and moisture retention in honeycomb cores, leading to costly failures and detection difficulties, and there is a need for a core material that is lightweight, formable, and ventable to prevent cryo-pumping in rocket fuel tanks.

Innovation Solution

A flexible core element made from a continuous sheet of material die-cut into a repeating geometrical design with hexagonal nodes and rectangular wall members, folded concertina-style to create a double-surfaced core with a large bonding area, allowing for venting and exhibiting good bending and shear strength, while being stackable and formable.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If honeycomb cores are used in sandwich construction, then the panel achieves stiffness and light weight, but the bonding area between skin and core is minimal leading to delamination

Engineering Contradiction:
Improvepanel stiffnessVSAvoidbonding area
Core Design Contradiction:
StrengthVSArea of stationary object

Solution Approach 1:

The core is divided into multiple discrete foam cells arranged in a grid pattern, where each cell provides an independent bonding interface. This segmentation increases the total bonding area between the skin and core compared to continuous honeycomb structures, while maintaining the lightweight and stiff characteristics through the cellular geometry.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The core structure transitions from a two-dimensional honeycomb pattern to a three-dimensional foam cell arrangement with vertical walls. This dimensional change creates multiple bonding surfaces (top, bottom, and side walls of each cell), significantly increasing the bonding area without compromising the panel's stiffness or increasing weight.

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

2Stability of the object's composition

If honeycomb cores are used, then the panel structure is established, but moisture is trapped in closed cells causing delamination at high altitudes

Engineering Contradiction:
Improvepanel structureVSAvoidmoisture retention
Core Design Contradiction:
Stability of the object's compositionVSObject-affected harmful factors

Solution Approach 1:

The core uses an open-cell foam structure rather than closed honeycomb cells. This porous configuration allows moisture and air to pass through the core material, preventing moisture accumulation that would otherwise cause delamination at high altitudes. The foam cells remain interconnected, maintaining structural integrity while providing venting capability.

Inventive Principle:
Principle #31Porous materials

3Adaptability or versatility

If a core material is made lightweight and formable, then it is suitable for various applications, but bending strength may be compromised

Engineering Contradiction:
ImproveformabilityVSAvoidbending strength
Core Design Contradiction:
Adaptability or versatilityVSStrength

Solution Approach 1:

The core combines foam material with a woven fabric reinforcement layer. The foam provides lightweight properties and formability, while the woven fabric reinforcement enhances bending strength and structural stability. This composite approach allows the core to be shaped into various configurations without sacrificing mechanical strength.

Inventive Principle:
Principle #40Composite materials

Data Source

PatentUS7541085B2Flexible construction element with large bonding surface area and method of manufacture
Publication Date: 2009.06.02 BURDON ROBERT L J
  • US7541085B2 patent drawing
  • US7541085B2 patent drawing
  • US7541085B2 patent drawing

AI summary

A flexible core element having a large bonding surface area suitable for sandwich type construction comprising a plurality of first hexagonal nodes defining a first surface, a plurality of second hexagonal nodes defining a second surface spaced apart from and parallel to the first surface, and a plurality of rectangular wall members which interconnect said first hexagonal nodes to said second hexagonal nodes and define the depth of the core element. Each hexagonal node corresponds to an open hexagonal cell on its obverse surface and serves as a bonding surface. The core element is fabricated from a continuous sheet of material that has been die-cut with a repeating geometrical design, creased and folded, concertina style, in upon itself to make a double-sided core material that is flexible, able to vent, exhibits good bend and shear strength, and has a large surface bonding area rendering it suitable in the construction of lightweight sandwich panels and offering a wide array of other applications.