Index Pin Locking Apparatus for Automated Aircraft Wing Assembly

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Solution Overview

Problem

In robotic assembly of large structures like aircraft wings, human interaction is required to connect and release support hardware, increasing costs, time, and injury risks due to the need for manual operation at coupling locations.

Innovation Solution

An index pin locking apparatus with a movable pin lock that automatically engages and disengages an index pin, allowing for automated positioning and retention of structural components, reducing the need for human intervention.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If manual hardware connection and release is used to support structural components, then the component can be retained at desired location, but human interaction increases cost, time, and injury risk

Engineering Contradiction:
Improvecomponent retention reliabilityVSAvoidautomation level of hardware operation
Core Design Contradiction:
ReliabilityVSExtent of automation

Solution Approach 1:

The index pin locking apparatus enables automated self-servicing through robotic operation. The pin lock mechanism automatically engages and disengages the index pin without human intervention, allowing the robotic system to independently perform support hardware operations while maintaining component retention reliability

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Manual mechanical operations are replaced by an automated robotic system. The robotic apparatus uses a controlled pin lock mechanism to engage and disengage the index pin, substituting human-operated mechanical actions with automated robotic control, thereby eliminating the need for human interaction while maintaining operational reliability

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

2Manufacturing precision

If manual hardware connection and release is used, then component positioning can be achieved, but manufacturing time and cost increase

Engineering Contradiction:
Improvecomponent positioning precisionVSAvoidmanufacturing efficiency
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The automated pin lock mechanism performs positioning and retention operations independently through robotic control. The system automatically engages the index pin to precisely position components and maintains this positioning throughout the manufacturing process, eliminating manual intervention while preserving positioning precision and improving manufacturing efficiency

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The index pin is pre-positioned and the pin lock mechanism is designed to automatically engage with it. This preliminary setup allows the robotic system to quickly secure components at precise locations without manual adjustment, thereby maintaining manufacturing precision while significantly reducing the time and cost associated with manual positioning operations

Inventive Principle:
Principle #10Preliminary action

3Ease of operation

If hardware is moved away from coupling location for processing, then component processing can be performed, but the hardware must be reconnected after processing

Engineering Contradiction:
Improvecomponent processing accessibilityVSAvoidtime for hardware connection and disconnection
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

The automated robotic pin lock system replaces manual hardware operations. The robotic apparatus can quickly engage and disengage the index pin through automated control, providing component processing accessibility while minimizing the time required for hardware connection and disconnection cycles

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

Solution Approach 2:

The pin lock mechanism is designed with movable components that can rapidly transition between engaged and disengaged states. This dynamic design allows the hardware to be quickly moved away from the coupling location for processing and just as quickly reconnected, maintaining ease of operation while reducing the time loss associated with repeated connection and disconnection operations

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS10717547B2Method of supporting a structure using an index pin locking apparatus
Publication Date: 2020.07.21 THE BOEING CO
  • US10717547B2 patent drawing
  • US10717547B2 patent drawing
  • US10717547B2 patent drawing

AI summary

A method for supporting a structure includes coupling an index pin to the structure, moving an index head relative to the structure to receive the index pin within a bore extending through the index head, and actuating a pin lock of the index head to retain the index pin within the bore.