Flat Composite Panel With Integrated Tear Straps

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Solution Overview

Problem

Flat composite panels used in aircraft pressure decks face challenges in impact damage resistance and repair due to their thinness and requirement for external stiffeners, which complicate both the manufacturing and repair processes.

Innovation Solution

A flat composite panel with integrated tear arrestment features, comprising a base panel made of fiber-reinforced polymer with interspersed first and second tear straps oriented in orthogonal directions, which enhances the panel's stiffness and resistance to impact damage without the need for external stiffeners.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If external stiffeners are added to increase panel stiffness, then the panel stiffness is improved, but the device complexity and manufacturing difficulty increase

Engineering Contradiction:
Improvepanel stiffnessVSAvoidstructure complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The patent merges the stiffener function directly into the panel structure by integrating longitudinal and transverse tear straps within the laminate layers. This eliminates the need for separate external stiffeners while maintaining the required stiffness through the integrated tear arrestment features that prevent damage propagation.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The patent uses composite materials by combining fiber-reinforced polymer plies with tear straps in a multi-layer laminate structure. The composite construction integrates the stiffening function throughout the panel thickness, achieving enhanced stiffness without additional external components.

Inventive Principle:
Principle #40Composite materials

2Manufacturing precision

If specialized tooling is used for co-curing stiffeners with panel, then the manufacturing precision is improved, but the manufacturing cost and complexity increase

Engineering Contradiction:
Improvestiffener attachment precisionVSAvoidmanufacturing complexity
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

The patent extracts the stiffener function from separate components and integrates it directly into the panel laminate structure. This eliminates the need for specialized co-curing tooling while maintaining manufacturing precision through the integrated tear strap design that is formed as part of the panel itself.

Inventive Principle:
Principle #2Taking out (Extraction)

3Reliability

If impact damage occurs to the panel, then the structural integrity is compromised, but the repair process becomes time-consuming and complex

Engineering Contradiction:
Improvestructural integrityVSAvoidrepair complexity
Core Design Contradiction:
ReliabilityVSEase of repair

Solution Approach 1:

The patent applies preliminary anti-action by incorporating tear straps that prevent damage propagation before full structural failure occurs. The integrated tear arrestment features stop crack propagation paths, maintaining structural integrity and simplifying repair by limiting the extent of damage that needs to be addressed.

Inventive Principle:
Principle #9Preliminary anti-action

4Weight of moving object

If the panel is made thinner to reduce weight, then the weight is reduced, but the impact damage resistance decreases

Engineering Contradiction:
Improvepanel weightVSAvoidimpact damage resistance
Core Design Contradiction:
Weight of moving objectVSObject-affected harmful factors

Solution Approach 1:

The patent uses composite materials with fiber-reinforced polymer plies and integrated tear straps to achieve high impact resistance in thin-panel configurations. The multi-layer composite structure provides damage tolerance without requiring increased thickness, maintaining weight efficiency while improving impact resistance.

Inventive Principle:
Principle #40Composite materials

Data Source

PatentUS12311615B2Flat composite panel with tear arrestment and method of making the same
Publication Date: 2025.05.27 THE BOEING CO
  • US12311615B2 patent drawing
  • US12311615B2 patent drawing
  • US12311615B2 patent drawing

AI summary

A pressure deck for an aircraft comprises a flat composite laminate base panel having integrated tear straps to enhance damage arrestment. The tear straps include a plurality of multi-ply, spaced apart longitudinal and lateral tear straps interspersed with the plies of the base panel.