Automated Fuselage Assembly Using Movable Cradles

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Solution Overview

Problem

The assembly of large commercial aircraft fuselages is labor-intensive and production rates are subject to fluctuations due to heavy dependence on manual labor, leading to unstable production environments.

Innovation Solution

An automated facility with movable cradles and robots that can assemble fuselage panels in a single upright position, utilizing determinant assembly holes for precise panel alignment and fastening, and an automated guide vehicle system for efficient movement of cradles and robots across the assembly floor, reducing manual labor and increasing production stability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Extent of automation

If manual labor is used for assembling fuselage panels, then flexibility in assembly operations is maintained, but production rates fluctuate and production stability deteriorates

Engineering Contradiction:
Improveautomation of fuselage assemblyVSAvoidcomplexity of assembly facility
Core Design Contradiction:
Extent of automationVSDevice complexity

Solution Approach 1:

The assembly facility is divided into multiple independent cells, each capable of assembling fuselage panels. This segmentation allows the system to process multiple panels simultaneously while maintaining manageable complexity in each individual cell. The movable cradles are also segmented into discrete units that can be independently positioned and operated.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The movable cradles are designed as multi-functional units that can support various fuselage panel configurations and be repositioned to different locations. These cradles serve multiple purposes: positioning panels, supporting robotic operations, and enabling flexible cell reconfiguration. This universality reduces the need for specialized equipment for each assembly task.

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

2Adaptability or versatility

If fixed jigs and fixtures are secured to the floor for assembling panelized fuselages, then assembly precision is maintained, but facility flexibility and reconfigurability are reduced

Engineering Contradiction:
Improvereconfigurability of assembly facilityVSAvoidprecision of panel alignment
Core Design Contradiction:
Adaptability or versatilityVSManufacturing precision

Solution Approach 1:

The cradles are designed to be movable rather than fixed, allowing dynamic repositioning to different assembly locations. This mobility enables the facility to be reconfigured for different panel types and assembly sequences while maintaining precision through controlled positioning mechanisms and alignment systems during movement.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The movable cradles act as intermediary devices between the floor and the fuselage panels. Instead of directly securing fixtures to the floor, the cradles provide a mobile platform that interfaces with both the floor (for movement) and the panels (for precise positioning and support), thereby mediating between flexibility and precision requirements.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Productivity

If heavy dependence on manual labor is maintained, then ease of operation is preserved, but productivity and production stability deteriorate

Engineering Contradiction:
Improveproduction rate of fuselage assemblyVSAvoidoperational simplicity of assembly process
Core Design Contradiction:
ProductivityVSEase of operation

Solution Approach 1:

The robotic systems are equipped with autonomous capabilities to perform assembly operations with minimal human intervention. The movable cradles and robotic end effectors work together in an automated sequence, with the system serving itself by automatically positioning components, performing fastening operations, and transitioning between tasks without requiring constant manual oversight.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Manual mechanical operations are replaced with automated robotic systems that perform fastening, positioning, and assembly tasks. The robotic end effectors substitute for manual tools and operations, dramatically increasing productivity while the automated control systems manage the complexity, effectively replacing human operation with automated mechanical-intelligent systems.

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

Data Source

PatentEP2604523B1Automated assembly of panelized aircraft fuselages
Publication Date: 2017.04.05 THE BOEING CO
  • EP2604523B1 patent drawingFigure 1
  • EP2604523B1 patent drawingFigure 2A~2B
  • EP2604523B1 patent drawingFigure 2C~2D

AI summary

A facility for assembling aircraft fuselages comprises a plurality of movable cradles. Each cradle is configured to support a fuselage keel structure and assemble a panelized fuselage in a single upright build position (Fig.1).