Composite Structure Shaping with Sequential Automated Manipulators

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Solution Overview

Problem

Existing composite manufacturing techniques are labor-intensive and time-consuming, requiring special handling to prevent defects during the transfer and placement of composite materials, especially for structures with complex contours and geometries.

Innovation Solution

A method and system utilizing automated manipulators to hold and shape uncured composite members from an initial to a final contour by sequentially forming unformed portions while maintaining unformed portions in the initial contour, applying tension and heat as needed, and using a place tool to define the final shape.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If automated manipulators are used to shape composite members, then productivity and manufacturing precision are improved, but device complexity increases

Engineering Contradiction:
Improvemanufacturing efficiencyVSAvoidsystem complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The composite member is divided into multiple unformed portions that are sequentially shaped along its length. Multiple manipulators are positioned at different locations to independently shape different portions, enabling parallel processing and improving productivity while managing system complexity through modular architecture

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The place tool is pre-configured with the final contour geometry before the composite member is positioned. This preliminary setup allows the automated manipulators to directly form the final shape without requiring complex real-time calculations or adjustments during the shaping process

Inventive Principle:
Principle #10Preliminary action

2Manufacturing precision

If sequential shaping of unformed portions is performed while holding remaining portions, then manufacturing precision is improved, but duration of action increases

Engineering Contradiction:
Improvecontour accuracyVSAvoidshaping time
Core Design Contradiction:
Manufacturing precisionVSDuration of action of moving object

Solution Approach 1:

While one manipulator is shaping a portion of the composite member, other manipulators simultaneously shape different portions. The process maintains continuous useful action across the entire member by eliminating idle time between shaping operations through parallel processing of multiple unformed portions

Inventive Principle:
Principle #20Continuity of useful action

Solution Approach 2:

The system dynamically coordinates multiple manipulators to adapt their positioning and shaping sequences based on the specific geometry and length of the composite member. This dynamic adjustment allows optimization of the shaping process for different part configurations, balancing precision requirements with production time

Inventive Principle:
Principle #15Dynamics

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This approach reduces the likelihood of defects and enhances efficiency by automating the shaping process, allowing for precise formation of complex composite structures with reduced labor and time requirements.

Implementation Method 1

synchronizing motion of the automated manipulators to form a final contour along the length of the composite member

Methodology Applied
Scientific EffectTension: Tension

Implementation Method 2

The operations include applying heat to the composite member while forming the final contour along the length of the composite member

Methodology Applied
Scientific EffectHeating: Heating

Data Source

PatentEP4353466B1Systems and methods for shaping composite structures
Publication Date: 2025.08.27 THE BOEING CO
  • EP4353466B1 patent drawingFigure 1
  • EP4353466B1 patent drawingFigure 2~3
  • EP4353466B1 patent drawingFigure 4A~4B

AI summary

A method for shaping a composite structure includes steps of: (1) holding a composite member in an initial contour along a length of the composite member; and (2) forming a final contour along the length of the composite member by: (3) sequentially shaping formed portions of the composite member while holding unformed portions of the composite member in the initial contour to form portions of the final contour; and (4) sequentially shaping the unformed portions of the composite member to form other portions of the final contour.