Rotor Blade Erosion Shield Segments with Deformable Joints

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Solution Overview

Problem

Conventional rotor blade abrasion strips are susceptible to fatigue damage and detachment due to strain experienced during high cycle fatigue and GAG cycles, leading to increased erosion vulnerability.

Innovation Solution

A rotor blade assembly with an erosion shield system featuring segments with deformable joints that isolate strain, using strain-tolerant materials and adhesive layers to maintain structural integrity and prevent fatigue cracking.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If conventional rigid abrasion strips are bonded to the leading edge of rotor blades, then erosion protection is provided, but fatigue damage and detachment occur due to strain during operational cycles

Engineering Contradiction:
Improveerosion protectionVSAvoidfatigue resistance
Core Design Contradiction:
Object-affected harmful factorsVSReliability

Solution Approach 1:

The erosion shield is divided into multiple discrete segments positioned along the leading edge of the rotor blade, with joints between segments that allow relative movement. This segmentation enables each segment to independently accommodate strain during operational cycles while maintaining continuous erosion protection, preventing the fatigue damage and detachment that occurs with rigid continuous strips

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The erosion shield segments are made from materials with specific mechanical properties including yield strengths of at least 15 ksi and elongations of at least 5%, creating a strain-tolerant material system. This parameter change in material properties allows the shield to undergo plastic deformation and absorb strain energy during high cycle fatigue and Ground-Air-Ground cycles without failing, resolving the contradiction between providing rigid erosion protection and resisting fatigue damage

Inventive Principle:
Principle #35Parameter changes

2Area of stationary object

If a continuous rigid erosion shield is used, then complete coverage is achieved, but strain isolation is impossible leading to fatigue cracking

Engineering Contradiction:
Improveshield coverage areaVSAvoidstructural integrity under strain
Core Design Contradiction:
Area of stationary objectVSStrength

Solution Approach 1:

The continuous erosion shield is segmented into multiple discrete sections with joints between them. These joints create discontinuities that allow strain isolation while the segments collectively maintain complete leading edge coverage. The segmentation enables the shield to cover the entire leading edge area while accommodating operational strains through relative movement at the joints

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The joints between erosion shield segments act as intermediary elements that decouple the segments from each other and from the underlying rotor blade structure. These joints accommodate relative movement and strain without transferring full strain loads through the entire shield system, maintaining structural integrity while allowing complete coverage

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 erosion shield system effectively reduces strain on the rotor blade, preventing fatigue cracking and detachment of the abrasion strips, thereby enhancing erosion protection and maintaining structural integrity.

Implementation Method 1

the joints deform responsive to strain experienced by the rotor blade, thereby isolating the erosion shield segments from at least a portion of the strain experienced by the rotor blade

Methodology Applied
Scientific EffectDeformation: Deformation

Implementation Method 2

an adhesive layer may be disposed between at least one of the erosion shield segments and the rotor blade

Methodology Applied
Scientific EffectAdhesion: Adhesive

Data Source

PatentUS10538317B2Rotor blade erosion protection systems
Publication Date: 2020.01.21 TEXTRON INNOVATIONS INC
  • US10538317B2 patent drawing
  • US10538317B2 patent drawing
  • US10538317B2 patent drawing

AI summary

In some embodiments, a rotorcraft includes an engine, a rotor hub assembly mechanically coupled to the engine and a plurality of rotor blade assemblies rotatably mounted to the rotor hub assembly. Each of the rotor blade assemblies includes a rotor blade having a leading edge and an erosion shield system extending spanwise along the leading edge of the rotor blade. The erosion shield system includes a plurality of erosion shield segments positioned adjacent to one another forming joints therebetween wherein, the joints deform responsive to strain experienced by the rotor blade, thereby isolating the erosion shield segments from at least a portion of the strain experienced by the rotor blade.