Airframe Micro-Pulsing Assembly With Indexing Features

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Solution Overview

Problem

Current airframe assembly processes face delays due to uneven completion times of components, require significant setup times, and rely on time-consuming and expensive automated inspection techniques.

Innovation Solution

A method and system for assembling airframes using micro pulsing and indexing features that allow simultaneous work at multiple stations, utilizing indexing features to convey instructions and perform work during pauses or pulses, maintaining structural loft without full scans.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If automated optical inspection techniques and probes are used to inspect position of parts, then measurement precision is improved, but loss of time and device complexity increase

Engineering Contradiction:
Improveposition inspection accuracyVSAvoidinspection time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

Indexing features are embedded in the structure during manufacturing, establishing a known reference framework before inspection occurs. This preliminary action eliminates the need for time-consuming scanning during assembly, as the reference data is already available from the indexing features.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

Physical indexing features (such as holes, pins, or geometric elements) create a digital or positional copy of the structure's configuration. This copying mechanism allows the system to know the structure's state without performing physical measurements, significantly reducing inspection time while maintaining precision.

Inventive Principle:
Principle #26Copying

2Ease of operation

If components are moved between cells for assembly work, then ease of operation is improved, but loss of time increases due to setup time at each cell

Engineering Contradiction:
Improveassembly flexibilityVSAvoidsetup time
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

The indexing features serve multiple functions: they guide the structure through the assembly line, provide reference for positioning at workstations, and enable rapid identification of the structure's configuration. This multi-functionality eliminates the need for separate setup procedures at each cell, reducing setup time while maintaining operational flexibility.

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

3Manufacturing precision

If the entire section remains at the cell until all work is completed, then manufacturing precision is maintained, but productivity decreases

Engineering Contradiction:
Improveassembly accuracyVSAvoidassembly throughput
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The assembly process is segmented into discrete workstations along the pulsing line, with each station performing specific tasks. The indexing features enable each station to work independently on its assigned portion of the structure without requiring the entire section to wait, thereby maintaining precision through controlled positioning while improving throughput through parallel processing.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The pulsing line enables continuous movement and processing of structures through multiple workstations. Indexing features ensure that each workstation can immediately begin work when the structure arrives, eliminating idle time and maintaining continuous productive action while preserving manufacturing precision through accurate positional reference.

Inventive Principle:
Principle #20Continuity of useful action

Data Source

PatentUS12509247B2Indexing for airframes undergoing pulsed-line assembly
Publication Date: 2025.12.30 THE BOEING CO
  • US12509247B2 patent drawing
  • US12509247B2 patent drawing
  • US12509247B2 patent drawing

AI summary

Systems and methods are provided for assembling a structure. The systems and method including micro pulsing a structure along a track in a process direction by less than a length of the structure. The structure is indexed to one or more work stations by mating indexing features in a manufacturing excess of the structure to complementary features at the work stations. The work stations would the perform work on the structure at the work stations while the structure is indexed to the work stations. Iteratively repeating the micro pulsing and indexing and working upon the structure until it is ready to advance to the next assembly process.