Aircraft Fuselage Attachment Plate for Lightning and Heat Isolation

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Solution Overview

Problem

Aircraft fastening systems require expensive materials to prevent the transmission of electrical currents and heat from external elements to the fuselage, necessitating a cost-effective solution for electrical and thermal insulation while attaching fittings to the outside of the fuselage.

Innovation Solution

An attachment system featuring a plate with a first face attached to the element and a second face oriented towards the fuselage, using a metal fitting with a shoe and fastening bolts that sandwich the plate, incorporating an electrically or thermally insulating material to prevent current or heat flow, with an optional intermediate plate for enhanced insulation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If expensive insulating materials are used to prevent current and heat transmission to the fuselage, then protection against electrical and thermal disturbances is improved, but manufacturing cost increases

Engineering Contradiction:
Improveprotection against electrical and thermal disturbancesVSAvoidmanufacturing cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent introduces a buffer plate as an intermediary element between the metal fitting and the fuselage. This plate serves as a mediator that provides electrical and thermal insulation without requiring the entire fastening system to be made of expensive insulating materials. The buffer plate is positioned at the critical interface where insulation is most needed, effectively blocking current and heat transmission to the fuselage while using cost-effective materials.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The attachment system employs a composite structure combining metal fitting (for mechanical strength and fastening function) with a buffer plate made of insulating material (for electrical and thermal protection). This composite approach allows each component to perform its optimal function - the metal fitting provides secure attachment while the buffer plate provides insulation - without requiring the entire assembly to be made of expensive specialized materials.

Inventive Principle:
Principle #40Composite materials

2Strength

If metal fittings are used to fasten elements to the fuselage, then mechanical strength and ease of installation are improved, but electrical current and heat transmission to the fuselage increases

Engineering Contradiction:
Improvemechanical fastening strengthVSAvoidelectrical current and heat transmission
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

The fastening system is segmented into distinct functional components: a metal fitting for mechanical attachment and a separate buffer plate for insulation. This segmentation allows the metal fitting to provide full mechanical strength without compromising, while the buffer plate independently handles the insulation function. The separation of functions enables optimal performance in both strength and protection without requiring a compromise in material selection for either component.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The buffer plate acts as an intermediary barrier between the metal fitting and the fuselage. It is positioned in the load path and thermal/electrical conduction path, providing mechanical support for the fitting while simultaneously blocking the transmission of harmful currents and heat to the fuselage structure.

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

The solution effectively limits the passage of electrical currents and heat to the fuselage, reducing costs by using a buffer plate that acts as an electrical or thermal insulator, protecting the aircraft from disturbances and maintaining structural integrity during crashes or heat generation from skids.

Implementation Method 1

the plate is constituted of an electrically insulating material arranged to prevent the passage of current

Methodology Applied
Scientific EffectElectrical insulation: Electrical Resistance

Implementation Method 2

the plate is constituted of a thermally insulating material arranged to limit the passage of heat

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Data Source

PatentUS20250002134A1Aircraft having a system for attaching an element to a fuselage and having a lightning protection screen
Publication Date: 2025.01.02 AIRBUS OPERATIONS (SAS)
  • US20250002134A1 patent drawing
  • US20250002134A1 patent drawing
  • US20250002134A1 patent drawing

AI summary

An attachment system for fastening an element to an aircraft fuselage, wherein the attachment system has a plate having a first face and a second face oriented towards the fuselage, and wherein the plate is fastened to the fuselage, a fitting fastened to the element and having a contact face in contact with the first face, and at least one fastening bolt having a screw and a nut, wherein the head of the screw is housed in the plate on the side of the second face, and wherein the nut is screwed to the screw, sandwiching the plate and the fitting. Also an aircraft with such an attachment system.