Spring-Biased Bonding Tabs for Composite Propeller Lightning Paths

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Solution Overview

Problem

Existing lightning strike protection systems for composite propeller blades are inadequate, particularly for designs where a conductive strip or band is affixed to the leading edge, as they do not effectively direct the strike to the propeller hub, leading to potential damage.

Innovation Solution

A bonding tab assembly with a mounting bracket and a spring-biased metal strip is used to electrically bond a protective metal band on the propeller blade to the hub, providing a direct path for lightning strikes to be directed to the hub, with adjustable spring force for reliable contact.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a conductive strip or band is affixed to the leading edge of the composite propeller blade, then lightning strike protection is provided to the blade, but the strike is not effectively directed to the propeller hub, leading to potential damage

Engineering Contradiction:
Improvelightning strike protection effectivenessVSAvoidelectrical conductivity path to hub
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

A bonding tab assembly serves as an intermediary component between the protective metal band and the propeller hub. The assembly includes a bonding tab with contact surfaces that electrically connect the metal band to the hub, ensuring effective lightning strike diversion. The bonding tab assembly acts as a mediator to establish reliable electrical continuity from the leading edge protection to the hub grounding point.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The bonding tab assembly utilizes spring biasing to maintain optimal contact pressure between the bonding tab and both the metal band and the hub. By adjusting the spring force parameter, the system ensures continuous electrical conductivity under varying operational conditions such as vibration and thermal expansion, maintaining reliable lightning protection without mechanical damage.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If spring-biased contact is used to ensure continuous electrical conductivity, then reliable bonding is achieved, but the device complexity increases

Engineering Contradiction:
Improvecontinuous electrical conductivityVSAvoidbonding tab assembly structure
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The bonding tab assembly is segmented into distinct functional components: a bonding tab with contact surfaces, a spring biasing mechanism, and mounting features. This segmentation allows each component to perform its specific function optimally while simplifying the overall design and assembly process. The modular structure makes the complex function of maintaining reliable electrical contact more manageable and manufacturable.

Inventive Principle:
Principle #1Segmentation

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 assembly effectively channels lightning strikes from the blade to the hub, enhancing protection by ensuring continuous electrical conductivity and reducing potential damage to the propeller.

Implementation Method 1

A bonding tab is attached to the upright mounting plate of the mounting bracket and adapted to being brought into spring-biased contact with a portion of the protective metal band affixed to the leading edge of the composite propeller blade

Methodology Applied
Scientific EffectSpring force: Spring

Data Source

PatentUS12441485B2Bonding tab assemblies providing lightning strike protection for composite aircraft propellers
Publication Date: 2025.10.14 TEXTRON INNOVATIONS INC
  • US12441485B2 patent drawing
  • US12441485B2 patent drawing
  • US12441485B2 patent drawing

AI summary

Lightning strike protection for composite propellers is provided by a bonding tab assembly which is electrically bonded to an electrically conductive protective band fixed to a leading edge of the composite propeller blade. The bonding tab establishes an electrically conductive path for a lightning strike on the protective band to be directed to the propeller hub thereby providing lightning strike protection to the propeller. The bonding tab assembly may include a mounting bracket having a lower mounting flange and an upright mounting plate, the lower mounting adapted to being attached to a counterweight clamp attached to a metallic blade collar surrounding the propeller blade shank. A bonding tab is attached to the upright mounting plate of the mounting bracket and adapted to being brought into spring-biased contact with a portion of the protective metal band affixed to the leading edge of the composite propeller blade.