Composite Blade Assembly via Chemical Bonding

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Solution Overview

Problem

Current turbomachine compressor rectifiers face challenges with composite material interfaces, particularly in terms of mass, cost, and differential expansion issues due to the use of metallic fixing means, which complicates assembly and maintenance.

Innovation Solution

The use of organic matrix composite parts with a thermoplastic or thermosetting matrix for the blades and housing, allowing for chemical or physico-chemical bonding and minimizing metallic fasteners, along with processes like compression molding, injection, and thermoforming for manufacturing, enables a lightweight, cost-effective, and easily assembled stator design.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If metallic fixing means are used to assemble composite parts, then mechanical strength is improved, but mass increases and differential expansion issues occur

Engineering Contradiction:
Improvemechanical strengthVSAvoidmass
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent replaces metallic mechanical fastening systems with a chemical bonding system using polymeric adhesive. The composite part is bonded to the support structure through surface treatment (sandblasting, plasma treatment, or chemical etching) followed by adhesive application, eliminating the need for metallic fasteners and their associated weight and differential expansion problems.

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

Solution Approach 2:

The patent uses composite materials (fiber-reinforced polymers) for both the part to be fixed and the support structure, creating a homogeneous material system that bonds effectively through polymeric adhesive. This composite-to-composite bonding approach ensures compatible thermal expansion characteristics and eliminates the metal-composite interface problems.

Inventive Principle:
Principle #40Composite materials

2Strength

If metallic fixing means are used to assemble composite parts, then mechanical strength is improved, but device complexity increases due to numerous assembly issues

Engineering Contradiction:
Improvemechanical strengthVSAvoidassembly complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The patent replaces complex mechanical fastening systems (requiring alignment, torque control, and multiple fasteners) with a simplified adhesive bonding process. The surface treatment and adhesive application steps eliminate the need for precise mechanical alignment and complex fastener installation, significantly reducing assembly complexity.

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

3Weight of moving object

If composite materials are used for blades and housing, then mass is reduced, but manufacturing precision requirements increase for chemical bonding

Engineering Contradiction:
ImprovemassVSAvoidbonding precision
Core Design Contradiction:
Weight of moving objectVSManufacturing precision

Solution Approach 1:

The patent modifies surface parameters through treatment processes (sandblasting to create roughness, plasma treatment to increase surface energy, or chemical etching to create micropores) that enhance adhesive bonding without requiring extremely tight dimensional tolerances. These surface parameter changes enable reliable bonding while maintaining manufacturing feasibility.

Inventive Principle:
Principle #35Parameter changes

4Strength

If hybrid metallic/composite assemblies are used, then structural performance is improved, but cost increases due to multiple material interfaces

Engineering Contradiction:
Improvestructural performanceVSAvoidmanufacturing cost
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The patent adopts a homogeneous composite-material architecture where both the blade/part and support structure are made from composite materials. This eliminates the hybrid metallic/composite interface, simplifying the manufacturing process and reducing costs associated with multi-material joining, while maintaining structural performance through optimized composite design.

Inventive Principle:
Principle #33Homogeneity

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

This approach results in a low-mass, low-cost bladed stator with improved mechanical strength, simplified assembly and maintenance, reduced time for assembly, and reduced differential expansion issues, while maintaining structural rigidity and aerodynamic optimization.

Implementation Method 1

sealing means the operation of fixing a part in a support using a polymeric element charged or not by mechanical blocking and/or by physico-chemical interaction with the support and/or or the part to be fixed

Methodology Applied
Scientific EffectChemical bonding: Chemical Bonding

Implementation Method 2

sealing means the operation of fixing a part in a support using a polymeric element charged or not by mechanical blocking and/or by physico-chemical interaction with the support and/or or the part to be fixed

Methodology Applied
Scientific EffectPhysico-chemical interaction: Adhesive

Implementation Method 3

the housing with a thermosetting or thermoplastic CMO wall is manufactured by a process selected from the group consisting of compression molding, injection of a thermoplastic or thermosetting matrix, thermoforming and co-consolidation

Methodology Applied
Scientific EffectThermosetting polymerization: Photopolymerisation

Data Source

PatentEP2431571B1Assembly of a blade and a composite support by secure fixing
Publication Date: 2013.06.05 TECHSPACE AERO
  • EP2431571B1 patent drawingFigure 1~2

AI summary

The present invention relates to a mechanical assembly (1) comprising: - a part to be fixed (3) by one of its ends; - a housing with an organic matrix composite wall or CMO (2) intended to receive the part to be fixed (3); - an injected sealing composite (4) comprising a thermoplastic or thermosetting material filled between 0 and 70% by mass, creating a mechanical and/or physico-chemical bond between the part to be fixed (3) and the housing with an organic matrix composite wall (2).