Metal-Composite Joint Assembly Using Cold Spray Sealed Fastening

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Solution Overview

Problem

Existing methods for assembling metal parts with organic matrix composite materials face issues of material abrasion and defects at the interface due to escaped sprayed material during cold gas spray deposition, leading to weakened mechanical strength.

Innovation Solution

A method involving the formation of a protective layer and seal on the organic matrix composite material, followed by additive manufacturing using cold gas spray deposition to create a fastening element, ensuring the sprayed material does not escape and forming a defect-free joint.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If cold gas spray deposition is used to form the fastening element, then the fastening element can be formed at low temperature suitable for organic matrix composite material, but sprayed material escapes between the connecting portions causing interface defects and material abrasion

Engineering Contradiction:
Improvedeposition temperatureVSAvoidinterface quality
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

A protective layer is introduced as an intermediary between the sprayed material and the organic matrix composite material. This protective layer captures escaped sprayed material, preventing it from causing abrasion and defects on the composite material surface, thus maintaining interface quality while allowing cold gas spray deposition to proceed

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The protective layer is formed in advance before the cold gas spray deposition process. This preliminary action prepares the surface to receive sprayed material without damage, preventing the harmful effects of material escape before they can occur during the deposition process

Inventive Principle:
Principle #10Preliminary action

2Temperature

If cold gas spray deposition is used to form the fastening element, then the organic matrix composite material is not damaged by high temperature, but the sprayed material escapes causing material abrasion on the composite material

Engineering Contradiction:
Improvematerial temperatureVSAvoidmaterial abrasion
Core Design Contradiction:
TemperatureVSObject-affected harmful factors

Solution Approach 1:

The protective layer serves as a mediator that intercepts escaped sprayed material, preventing direct contact with and abrasion of the organic matrix composite material. This allows the cold gas spray deposition to proceed at low temperatures without the harmful abrasion effect

Inventive Principle:
Principle #24Intermediary (Mediator)

3Adaptability or versatility

If cold gas spray deposition is used to form the fastening element, then the process is suitable for organic matrix composite material, but defects occur at the interface between the fastening element and the first connecting portion

Engineering Contradiction:
Improveprocess compatibilityVSAvoidinterface defect rate
Core Design Contradiction:
Adaptability or versatilityVSManufacturing precision

Solution Approach 1:

The protective layer acts as an intermediary that prevents escaped sprayed material from creating defects at the interface between the fastening element and the first connecting portion. This maintains manufacturing precision while preserving the compatibility of cold gas spray deposition with organic matrix composite material

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 method enhances the mechanical strength of the assembly by preventing material escape and interface defects, resulting in a robust and reliable connection.

Implementation Method 1

forming, by additive manufacturing using cold gas spray deposition of metal powder, also known by the acronym CGS for 'Cold Gas Spraying', a fastening element

Methodology Applied
Scientific EffectCold gas spray deposition: Deposition (physical)

Implementation Method 2

a part of the sprayed material could escape between the first connecting portion and the second connecting portion. This leads both to abrasion of the second connecting portion

Methodology Applied
Scientific EffectAbrasion prevention: Abrasion

Data Source

PatentUS12496783B2Method for assembling a first metal part with a second part made of an organic matrix composite material
Publication Date: 2025.12.16 ARIANEGRP SAS
  • US12496783B2 patent drawing
  • US12496783B2 patent drawing
  • US12496783B2 patent drawing

AI summary

The invention relates to a method for assembling a first metal part with a second part made of an organic matrix composite material, the first part having a first connecting portion and the second part having a second connecting portion, the method comprising the steps of:causing the first connecting portion and the second connecting portion to overlap, a through-hole of the second connecting portion opening onto the first connecting portion,forming a protective layer on the side wall of the through-hole,forming a seal between the protective layer and the first connecting portion, andforming, by additive manufacturing using cold gas spray deposition of metal powder, a fastening element which extends into the through-hole, is fastened to the first connecting portion and encloses the second connecting portion.