Triangular Prism Core Beam with Triaxial Fabric Cover

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Solution Overview

Problem

Existing lightweight beam manufacturing techniques, such as pultrusion and filament winding, face challenges with mandrel removal and resource strain, and lack efficient methods for achieving optimal rigidity and minimal weight.

Innovation Solution

A lightweight beam structure featuring a triangular prism core with a triaxial fabric cover and reinforcement rods, allowing for a mandrel-free formation process that enhances strength and reduces weight by using a core that remains integrated within the beam.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If filament winding around a mandrel is used to form lightweight beams, then the beam structure can be created, but the mandrel removal becomes difficult and resource strain increases

Engineering Contradiction:
Improvemandrel removalVSAvoidmandrel extraction complexity
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The patent extracts the mandrel from the final beam structure by using a soluble or removable core form that dissolves or falls away after the composite material cures, eliminating the need for complex mandrel removal processes while maintaining ease of manufacture

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent applies preliminary action by pre-positioning the mandrel within the mold cavity before composite layup, allowing the mandrel to serve as an internal support during manufacturing that automatically becomes part of the beam structure or can be easily removed after curing

Inventive Principle:
Principle #10Preliminary action

2Productivity

If traditional pultrusion or filament winding methods are used, then beam production is achieved, but resource strain increases and manufacturing efficiency decreases

Engineering Contradiction:
Improvemanufacturing efficiencyVSAvoidresource strain
Core Design Contradiction:
ProductivityVSLoss of energy

Solution Approach 1:

The patent segments the manufacturing process into discrete steps: placing rods in a mold cavity, laying up composite material layers, and curing. This segmentation allows for simpler, more efficient production compared to continuous pultrusion or filament winding, reducing resource strain while maintaining productivity

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent uses disposable mold cavities and consumable rod materials that are inexpensive and single-use, eliminating the need for expensive, complex equipment maintenance and reducing overall resource strain compared to traditional manufacturing methods

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

3Weight of moving object

If hollow beam structures are used to reduce weight, then weight reduction is achieved, but structural strength and rigidity are compromised

Engineering Contradiction:
Improvebeam weightVSAvoidbeam strength
Core Design Contradiction:
Weight of moving objectVSStrength

Solution Approach 1:

The patent uses composite materials consisting of rods embedded in composite material layers, creating a lightweight yet strong structure that maintains both weight reduction and structural strength through the synergistic combination of different materials

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The patent applies local quality by positioning rods at specific locations within the beam structure where strength is most needed, while using thinner composite material layers in other areas, optimizing the balance between weight and strength throughout the beam

Inventive Principle:
Principle #3Local quality

Data Source

PatentEP2514884B1Lightweight beam structure
Publication Date: 2013.10.23 LOCKHEED MARTIN CORP
  • EP2514884B1 patent drawingFigure 1
  • EP2514884B1 patent drawingFigure 2
  • EP2514884B1 patent drawingFigure 3

AI summary

A lightweight beam (10) may have a triangular prism core (12) and a triaxial fabric cover (14) wrapped around the core (12), with at least one rod (16) proximate an apex of the core (12). The rod (16) may extend substantially parallel to a centerline (18) of the core (12). Multiple lightweight beams (10) may be joined to form a larger lightweight structure.