Structural Gap Filler Injection for Debris-Free One-Up Assembly

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Solution Overview

Problem

The aircraft manufacturing process is hindered by loose debris between components, requiring time-consuming disassembly and cleaning, which increases labor and reduces efficiency.

Innovation Solution

A method involving drilling an injection hole and encapsulating drilling debris with a structural gap filler, followed by drilling a hole through the filler to maintain clamp-up and reduce burr production, thereby eliminating the need for disassembly and cleaning.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If components are disassembled to remove drilling debris from gaps, then cleaning effectiveness is improved, but manufacturing time and labor increase

Engineering Contradiction:
Improvecleaning effectivenessVSAvoidmanufacturing time
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The gap filler material is applied to the gap between components before drilling operations begin. This preliminary application creates a barrier that prevents drilling debris from accumulating in the gap, eliminating the need for subsequent disassembly and cleaning operations while maintaining manufacturing precision

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention converts the potentially harmful effect of drilling debris generation into a beneficial process by using the gap filler material to capture and contain the debris within the gap. The debris that would normally require cleaning is instead encapsulated by the curing filler, transforming a cleaning requirement into an automated containment solution

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

2Object-generated harmful factors

If components are disassembled to remove loose debris, then debris removal is improved, but labor and flow time increase

Engineering Contradiction:
Improveloose debris removalVSAvoidflow time
Core Design Contradiction:
Object-generated harmful factorsVSLoss of time

Solution Approach 1:

The gap filler is applied in advance before drilling operations, creating a protective barrier that prevents loose debris from generating in the first place. This preliminary protective measure eliminates the need for time-consuming disassembly and cleaning operations that would otherwise be required to remove harmful debris

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The gap filler material performs the debris removal function automatically through its curing process. As the filler cures, it encapsulates any debris within the gap, performing the cleaning function self-service without requiring external intervention, disassembly, or additional labor

Inventive Principle:
Principle #25Self-service

3Stability of the object's composition

If clamp-up is maintained during drilling operations, then assembly stability is improved, but burr production increases

Engineering Contradiction:
Improveassembly stabilityVSAvoidburr production
Core Design Contradiction:
Stability of the object's compositionVSObject-generated harmful factors

Solution Approach 1:

The gap filler material serves as an intermediary substance between the components during drilling operations. It fills the gap that would otherwise allow burrs to form and accumulate, while still permitting clamp-up to be maintained for assembly stability. The filler material absorbs and contains burrs within the gap, preventing them from becoming loose harmful factors

Inventive Principle:
Principle #24Intermediary (Mediator)

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 manufacturing time and costs by encapsulating debris within the structural gap filler, maintaining clamp-up during processing, and minimizing burr production during subsequent drilling operations.

Implementation Method 1

Drilling debris generated between the first component and the second component during drilling of the injection hole are encapsulated by injecting a structural gap filler through the injection hole and between the first component and the second component

Methodology Applied
Scientific EffectEncapsulation: Physical Containment

Implementation Method 2

Clamp-up of the first component and the second component is maintained between drilling the injection hole and drilling the hole

Methodology Applied
Scientific EffectCompression: Compression

Data Source

PatentUS11851213B1Methods and structural gap filler for one-up assembly
Publication Date: 2023.12.26 THE BOEING CO
  • US11851213B1 patent drawing
  • US11851213B1 patent drawing
  • US11851213B1 patent drawing

AI summary

Methods and structural gap filler for one up assembly of structures. Drilling debris generated between the first component and the second component during drilling of an injection hole are encapsulated by injecting a structural gap filler through the injection hole and between the first component and the second component.