Fastener Interference Fit for Spark Containment

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Solution Overview

Problem

Aircraft manufacturing faces challenges in achieving fault-tolerant spark protection in flammable zones due to manufacturing faults like oversized holes, contamination, and inconsistencies, which can lead to sparking and particle ejection, requiring additional steps and time for cap seal application.

Innovation Solution

A fastener system comprising a sleeve, a washer, and a bolt, where the washer is positioned between the sleeve and the aircraft structure, forming an interference fit to seal the hole and prevent particle ejection, eliminating the need for cap seals and enhancing fault tolerance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a cap seal is applied over the fastener head to achieve fault tolerance, then spark protection reliability is improved, but installation time and process complexity increase

Engineering Contradiction:
Improvespark protection reliabilityVSAvoidinstallation time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The invention extracts the sealing function from the cap seal and relocates it to the fastener system itself through the interference fit between the sleeve and fastener, eliminating the need for separate cap seal application while maintaining fault tolerance

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The sealing function is merged with the fastening function by designing the sleeve-fastener interference fit to simultaneously provide both mechanical fastening and spark containment, consolidating multiple functions into a single integrated system

Inventive Principle:
Principle #5Merging (Combining)

2Reliability

If a cap seal is applied over the fastener head to achieve fault tolerance, then spark protection reliability is improved, but device complexity increases

Engineering Contradiction:
Improvespark protection reliabilityVSAvoidfastener system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The invention removes the cap seal component entirely and extracts its sealing function, reducing the number of parts and simplifying the overall fastener system while maintaining fault tolerance through the interference fit design

Inventive Principle:
Principle #2Taking out (Extraction)

3Reliability

If an interference fit is formed between the sleeve and aircraft structure to prevent sparking, then electrical connection is improved, but manufacturing precision requirements increase due to faults like oversized holes

Engineering Contradiction:
Improveelectrical connectionVSAvoidhole dimension precision
Core Design Contradiction:
ReliabilityVSManufacturing precision

Solution Approach 1:

The invention designs the interference fit with built-in tolerance compensation that cushions against manufacturing variations, allowing the system to maintain reliable electrical connection even when holes are oversized or have other manufacturing inconsistencies

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Solution Approach 2:

The interference fit parameters are specifically designed to accommodate a range of hole dimensions, transforming the rigid precision requirement into a more flexible parameter range that still ensures adequate electrical connection and spark containment

Inventive Principle:
Principle #35Parameter changes

4Reliability

If cap seals are applied to each fastener to ensure consistent coverage, then spark protection consistency is improved, but productivity decreases

Engineering Contradiction:
Improvespark protection consistencyVSAvoidfastener installation productivity
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The invention eliminates the cap seal application step entirely, removing the productivity bottleneck while maintaining consistent spark protection through the pre-designed interference fit that requires no additional operations

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The fastener system provides its own spark containment function through the interference fit between sleeve and fastener, making the system self-sufficient and eliminating the need for separate cap seal application operations

Inventive Principle:
Principle #25Self-service

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

The solution provides efficient and consistent spark containment in flammable zones, reducing installation time and costs by eliminating the need for cap seals and ensuring reliable particle containment even with manufacturing faults.

Implementation Method 1

the sleeve expands to form an interference fit with the washer

Methodology Applied
Scientific EffectInterference fit: Friction

Data Source

PatentUS10393161B2Method for fuel tank spark containment
Publication Date: 2019.08.27 THE BOEING CO
  • US10393161B2 patent drawing
  • US10393161B2 patent drawing
  • US10393161B2 patent drawing

AI summary

A method and apparatus for forming a seal over a hole in a structure. The apparatus comprises a washer, a sleeve, and a fastener. The washer has a first channel. The sleeve has a second channel and an expandable section. The sleeve is positioned inside the first channel in the washer. The fastener has an elongate portion positioned inside the second channel of the sleeve to cause at least a portion of the expandable section of the sleeve to form a first interference fit with the washer.