Flexible Component Shaping With Closed-Loop Fit Alignment

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Solution Overview

Problem

Current processes for assembling large, flexible aerospace components are time-consuming and labor-intensive, and there is a need for efficient control of shape and fit between components to minimize deformation and ensure precise alignment.

Innovation Solution

A manufacturing system utilizing a holding structure, actuators, and a closed feedback loop to iteratively adjust the shape of components to a target shape using a controller that determines deviations and applies displacements until a tolerance is met, incorporating metrology systems for precise measurement and control.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If traditional manual processes are used for assembling large flexible components, then labor flexibility is maintained, but manufacturing time increases and labor costs increase

Engineering Contradiction:
Improvemanufacturing efficiencyVSAvoidassembly time
Core Design Contradiction:
ProductivityVSLoss of time

Solution Approach 1:

The system enables self-service through automated actuators that automatically adjust component shapes based on real-time metrology measurements and controller directives, eliminating the need for manual labor while maintaining precise control over the assembly process

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Manual mechanical adjustment processes are replaced with an automated control system comprising actuators, metrology systems, and controllers that use feedback loops to automatically shape and position components, substituting human labor with automated mechanical and computational systems

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Manufacturing precision

If traditional assembly processes are used for large flexible components, then process simplicity is maintained, but shape control precision deteriorates

Engineering Contradiction:
Improveshape control precisionVSAvoidsystem complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The system employs closed-loop feedback control where metrology systems continuously measure component shapes, the controller compares measurements against target specifications, and actuators automatically adjust shapes based on the feedback, ensuring precise shape control throughout the assembly process

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The control system integrates multiple functions into a unified platform: metrology systems perform both measurement and quality verification, actuators provide both shaping and positioning capabilities, and the controller coordinates all operations, reducing overall system complexity despite enhanced precision requirements

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Manufacturing precision

If iterative shape adjustment is implemented, then shape accuracy improves, but process time increases

Engineering Contradiction:
Improveshape accuracyVSAvoidassembly speed
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The iterative adjustment process operates continuously without interruption: metrology systems continuously monitor component shapes, the controller continuously processes measurements and generates adjustment directives, and actuators continuously apply corrections, maintaining uninterrupted productive action throughout the shaping process

Inventive Principle:
Principle #20Continuity of useful action

Solution Approach 2:

The system performs preliminary shaping actions using actuators before final assembly operations, pre-positioning components to within acceptable tolerances in advance, which reduces the need for time-consuming adjustments during the actual assembly process

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS20250322119A1Manufacturing systems and methods for shaping and assembling flexible structures
Publication Date: 2025.10.16 THE BOEING CO
  • US20250322119A1 patent drawing
  • US20250322119A1 patent drawing
  • US20250322119A1 patent drawing

AI summary

A manufacturing system and method for determining and optimizing shaping locations and shaping inputs and shaping a component using the shaping locations and shaping inputs includes steps of: determining shaping locations on the component for application of shaping inputs that change an as-built shape of the component toward a target shape of the component and determining the shaping inputs to be applied to the component at the shaping locations to change the as-built shape of the component toward the target shape of the component; applying the shaping inputs to the component at the shaping locations on the component; and changing the as-built shape of the component to within a predetermined tolerance of the target shape.