Electroplated Composite Fan Blade Sheath Without Adhesive Bonding

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Solution Overview

Problem

Thermoplastic or thermoset composite fan blades face issues with through-thickness impact capability, leading to delamination and damage due to adhesive-bonded titanium sheaths, which are costly and unreliable in dynamic impacts.

Innovation Solution

An electroplated sheath is applied to the composite fan blade, extending from the platform portion to the tip, with a nickel alloy plating material, and optionally including a bond coat, to enhance structural integrity and impact resistance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If adhesively bonded titanium sheath is used, then structural integrity is maintained, but manufacturing cost increases and reliability decreases in dynamic impact

Engineering Contradiction:
Improveadhesive bond reliabilityVSAvoidmanufacturing cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent replaces the chemical adhesive bonding system with an electroplated metallic sheath system. The electroplated sheath provides mechanical and metallurgical bonding through direct metal-to-composite attachment, eliminating reliance on adhesive bonds that fail in dynamic impact. This substitution resolves the contradiction by providing both low manufacturing cost (electroplating is simpler than titanium machining) and high reliability (metallic bond withstands dynamic loads).

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent changes the bonding mechanism parameter from chemical adhesion to electrochemical deposition and metallurgical bonding. By controlling electroplating parameters (current density, plating time, solution composition), the sheath achieves optimal thickness and adhesion strength. This parameter change enables reliable attachment without expensive adhesive bonding processes.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If adhesively bonded titanium sheath is used, then structural integrity is maintained, but device complexity increases

Engineering Contradiction:
Improvestructural integrityVSAvoidattachment scheme complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent extracts and removes the adhesive bonding layer from the attachment system. By eliminating the adhesive intermediary, the design simplifies from a multi-layer adhesive-bonded structure to a direct electroplated metallic attachment. This extraction reduces device complexity while maintaining structural integrity through the robust electroplated sheath.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The electroplated sheath serves multiple functions simultaneously: it provides structural reinforcement, corrosion protection, and direct metallurgical bonding to the composite substrate. This multi-functionality eliminates the need for separate adhesive layers and complex attachment schemes, reducing overall device complexity while maintaining structural integrity.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Strength

If adhesively bonded titanium tip caps are used, then tip protection is provided, but manufacturing cost increases

Engineering Contradiction:
Improvetip protection capabilityVSAvoidmanufacturing cost
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The patent replaces expensive precision-machined titanium tip caps with electroplated metallic tips. The electroplating process directly deposits metal onto the composite tip area, eliminating costly titanium machining operations while providing equivalent or superior tip protection. This substitution resolves the contradiction by maintaining strength at lower manufacturing cost.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

4Manufacturing precision

If complex machining of titanium details is performed, then precise geometry is achieved, but manufacturing cost increases

Engineering Contradiction:
Improvetitanium detail geometryVSAvoidmanufacturing cost
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

The patent replaces mechanical machining processes with electroplating deposition. The electroplating process naturally conforms to the substrate geometry and can be controlled to achieve precise dimensions and surface finishes without complex machining operations. This substitution maintains manufacturing precision while dramatically reducing manufacturing cost by eliminating expensive titanium machining.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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 electroplated sheath provides improved impact resistance, reduced manufacturing costs, and eliminates the need for adhesive bonding, ensuring structural integrity and preventing delamination.

Implementation Method 1

a sheath electroplated to a surface of the composite fan blade proximate at least one of the leading edge, the trailing edge and the tip

Methodology Applied
Scientific EffectElectroplating: Electroplating

Data Source

PatentUS20250376987A1In-situ electroplated sheath for composite fan blade
Publication Date: 2025.12.11 RTX CORP
  • US20250376987A1 patent drawing
  • US20250376987A1 patent drawing
  • US20250376987A1 patent drawing

AI summary

An electroplated sheath for a composite fan blade including a root portion adjacent a platform portion and an airfoil portion adjacent the platform portion and a tip adjacent the airfoil portion opposite the root portion; the airfoil portion defines a blade chord between a leading edge and a trailing edge; the airfoil portion defines a concave pressure side and a convex suction side defined between the leading edge and the trailing edge; and a sheath electroplated to a surface of the composite fan blade proximate at least one of the leading edge, the trailing edge and the tip.