Automated Tape Placement for Contoured Composite Structures

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Solution Overview

Problem

Existing methods for fabricating highly contoured, multi-leg composite structures are labor-intensive and inefficient for high-volume production, particularly when using automatic fiber placement machines, which struggle with complex structural features and tight radii, limiting their ability to produce structures like Z or J-cross sections.

Innovation Solution

A method utilizing unidirectional pre-impregnated composite tape and automated tape placement equipment to fabricate continuous composite structures with nearly unlimited ply orientation, maintaining polar fiber orientation and constant width tape segments, allowing for accurate feature placement and efficient production of structures like frames, spars, and ribs.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If hand layup techniques are used to fabricate highly contoured composite structures, then manufacturing flexibility and adaptability are maintained, but labor intensity increases and productivity decreases

Engineering Contradiction:
Improvemanufacturing flexibilityVSAvoidproduction volume
Core Design Contradiction:
Adaptability or versatilityVSProductivity

Solution Approach 1:

The composite structure is divided into multiple plies or layers that can be independently fabricated and then assembled. This segmentation allows automated equipment to produce individual layers efficiently while maintaining the flexibility to create complex contoured shapes through the assembly of these standardized segments.

Inventive Principle:
Principle #1Segmentation

2Productivity

If automatic fiber placement machines are used to fabricate composite structures, then productivity and automation are improved, but the ability to produce highly contoured structures with tight radii and complex features deteriorates

Engineering Contradiction:
Improvefabrication speedVSAvoidability to produce complex geometries
Core Design Contradiction:
ProductivityVSAdaptability or versatility

Solution Approach 1:

The invention transitions from attempting to fabricate complex 3D contoured structures directly in one step to a two-dimensional approach where flat or simply curved plies are fabricated using automated equipment, then assembled into the final complex 3D shape. This dimensional transformation allows automated machinery to maintain its productivity advantage while achieving complex geometries through assembly rather than direct fabrication.

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

3Manufacturing precision

If AFP machines frequently start, stop, and change directions to accommodate complex structural features, then manufacturing precision may be maintained, but productivity and fabrication efficiency deteriorate

Engineering Contradiction:
Improvefeature placement accuracyVSAvoidfabrication efficiency
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The complex structural features are pre-fabricated as separate plies or components using automated equipment under optimized conditions, then positioned and assembled into the final structure. This preliminary fabrication of individual elements allows each component to be manufactured with high precision without the need for frequent machine stopping and direction changes during the overall fabrication process, thereby maintaining both precision and productivity.

Inventive Principle:
Principle #10Preliminary action

4Ease of manufacture

If AFP machines are used to fabricate structures with Z or J-cross sections, then some contoured shapes can be produced, but the ability to load material at inside corners deteriorates

Engineering Contradiction:
Improvecapability to produce certain cross sectionsVSAvoidability to fabricate all contoured structures
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

Structures with challenging geometries like Z or J-cross sections are divided into multiple plies that can be independently fabricated and assembled. This segmentation allows material to be loaded and processed in manageable sections rather than attempting to continuously form complex corner regions, enabling the production of structures that would be difficult or impossible to fabricate with continuous AFP processes alone.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS8932423B2Method for producing contoured composite structures and structures produced thereby
Publication Date: 2015.01.13 THE BOEING CO
  • US8932423B2 patent drawing
  • US8932423B2 patent drawing
  • US8932423B2 patent drawing

AI summary

A contoured composite structure is fabricated by laying up a composite charge that includes at least one ply formed by uni-directional fiber pre-preg ply segments having substantially constant widths. The ply segments are placed in side-by-side, overlapping relationship with their longitudinal centerlines aligned in a polar orientation related to the contour of the structure. The charge is formed into the shape of the structure and cured.