Partially Covered Sandwich Core for Weight-Efficient Structural Stability

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Solution Overview

Problem

Existing sandwich components, particularly those used in aircraft, face challenges in achieving a balance between mechanical stability and weight reduction, often requiring full-surface cover layers that compromise weight efficiency.

Innovation Solution

A partially covered core design with selective fiber reinforcement, where only specific regions are coated with a first cover layer, allowing the core to be accessible and visible in uncoated areas, while maintaining mechanical stability through unidirectional or crossed fibers.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If full-surface cover layers are used to ensure mechanical stability, then structural integrity is improved, but weight increases significantly

Engineering Contradiction:
Improvemechanical stabilityVSAvoidcomponent weight
Core Design Contradiction:
StrengthVSWeight of stationary object

Solution Approach 1:

The patent applies cover layers selectively only in specific regions where mechanical stability is required, rather than covering the entire surface. This localized application maintains structural integrity in critical areas while reducing overall material usage and weight.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The core is divided into different regions: covered regions where mechanical support is needed and uncovered regions where weight reduction is prioritized. This segmentation allows differential application of cover layers based on local structural requirements.

Inventive Principle:
Principle #1Segmentation

2Strength

If complete cover layers are applied to maintain structural integrity, then mechanical strength is improved, but material usage increases

Engineering Contradiction:
Improveload-bearing capabilityVSAvoidmaterial consumption
Core Design Contradiction:
StrengthVSQuantity of substance

Solution Approach 1:

Cover layers are applied locally only where load-bearing requirements demand additional structural support, rather than uniformly across the entire component surface. This reduces material consumption while maintaining necessary strength.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

Instead of applying complete cover layers across the entire surface, the patent uses partial coverage with fiber reinforcement only in regions where it provides necessary structural support, eliminating excessive material usage.

Inventive Principle:
Principle #16Partial or excessive action

3Weight of stationary object

If selective regional coating is used to reduce weight, then weight savings are achieved, but mechanical stability may be compromised

Engineering Contradiction:
Improvecomponent weightVSAvoidstructural integrity
Core Design Contradiction:
Weight of stationary objectVSStrength

Solution Approach 1:

The patent strategically places cover layers in specific regions where mechanical stability is most critical, using local quality enhancement to maintain overall structural integrity while achieving weight reduction in non-critical areas.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The selection of which regions to cover is determined in advance based on structural analysis, placing reinforcement exactly where needed before manufacturing, ensuring mechanical stability is maintained while minimizing material usage.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS20250242564A1Lightweight sandwich component with partially covered core and method for producing a sandwich component
Publication Date: 2025.07.31 DIEHL AVIATION LAUPHEIM GMBH
  • US20250242564A1 patent drawing
  • US20250242564A1 patent drawing
  • US20250242564A1 patent drawing

AI summary

A sandwich component includes a core having two opposite flat sides and at least one first cover layer connected to the core, mechanically stabilizing the sandwich component and containing at least one fiber component containing fibers. At least one of the flat sides is coated with the first cover layer such that only a coating region of this side is covered by the first cover layer, so that an uncoated free region of this flat side remains, and this flat side is not coated with any further layers so that the core is accessible from an environment in the free region on this flat side. A method for producing a sandwich component includes providing the core, and coating at least one of the flat sides with the first cover layer such that the core remains accessible from the environment in the free region on this flat side.