Method for manufacturing a part out of a metal matrix composite material, and related device

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Solution Overview

Problem

Current manufacturing methods for composite materials with metal matrix reinforcement face challenges in achieving a balance between mechanical, thermal, and electrical properties, cost, and scalability, particularly in the aeronautics industry, where materials like aluminum and polymer-based composites fall short in severe environments and complex, energy-intensive processes.

Innovation Solution

A method for manufacturing composite parts using a fiber reinforcement densified by a metal matrix, involving a device with a support and molding portion that allows for pre-heating, sealing, and applying force to impregnate the metal matrix into the fiber reinforcement under vacuum, enabling efficient production of parts with improved thermal and electrical performance at a reasonable cost.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If aluminum is used for avionics housings to achieve low density and good thermal conductivity, then thermal management is improved, but the housing cannot remove all heat generated by power electronics, requiring supplementary cooling systems that increase mass

Engineering Contradiction:
Improveheat removal capabilityVSAvoidhousing mass
Core Design Contradiction:
TemperatureVSWeight of moving object

Solution Approach 1:

The patent applies composite materials by combining carbon fiber reinforcement with metal matrix (aluminum or magnesium) to create a material that simultaneously achieves low density, excellent thermal conductivity, and high mechanical strength. This composite structure eliminates the need for supplementary cooling systems while maintaining effective heat removal, thereby reducing overall housing mass compared to monolithic aluminum with added cooling components

Inventive Principle:
Principle #40Composite materials

2Weight of moving object

If polymer-based composite materials are used to achieve light weight and mechanical strength, then mass is reduced, but the material cannot conduct heat and electricity effectively and cannot resist severe temperature environments

Engineering Contradiction:
Improvepart massVSAvoidthermal and electrical conductivity
Core Design Contradiction:
Weight of moving objectVSTemperature

Solution Approach 1:

The patent resolves this contradiction by creating a hybrid composite material that combines the low density and mechanical strength of polymer-based fiber reinforcement (carbon, glass, or aramid fibers) with the thermal and electrical conductivity of a metal matrix. The metal matrix infiltrates the fiber reinforcement to form a composite that maintains the lightweight advantage while adding the necessary conductive properties and temperature resistance for severe environments

Inventive Principle:
Principle #40Composite materials

3Strength

If the Hyperclave enclosure method is used to manufacture metal matrix composite materials, then dimensional stability and mechanical properties are improved, but the process becomes extremely complex and consumes excessive energy and manufacturing time

Engineering Contradiction:
Improvemechanical propertiesVSAvoidmanufacturing process complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The patent applies segmentation by dividing the manufacturing process into distinct stages: first placing the fiber reinforcement in a mold, then separately introducing the molten metal matrix through a pouring channel. This segmented approach replaces the complex Hyperclave enclosure system with simpler, sequential operations that reduce device complexity while maintaining the infiltration of metal into fiber reinforcement to achieve desired mechanical properties

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent applies preliminary action by pre-placing the fiber reinforcement into the mold and preparing the mold cavity before introducing the molten metal matrix. The reinforcement is positioned and secured in advance, and the mold is prepared with heating elements and pouring channels ready, which streamlines the subsequent infiltration process and reduces overall manufacturing time and energy consumption compared to the Hyperclave method

Inventive Principle:
Principle #10Preliminary action

4Manufacturing precision

If high pressure is applied during metal matrix infiltration to achieve complete impregnation, then composite material quality is improved, but manufacturing cost and energy consumption increase

Engineering Contradiction:
Improveimpregnation qualityVSAvoidmanufacturing energy consumption
Core Design Contradiction:
Manufacturing precisionVSUse of energy by stationary object

Solution Approach 1:

The patent applies mechanics substitution by replacing the high-pressure infiltration system with a gravity-driven or low-pressure pouring system. The molten metal matrix is introduced through a pouring channel and allowed to infiltrate the fiber reinforcement naturally or with minimal pressure assistance, achieving complete impregnation without the energy-intensive high-pressure equipment used in conventional methods

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 method produces composite materials with enhanced mechanical, thermal, and electrical properties, offering better density and cost-effectiveness than monolithic aluminum or magnesium, while allowing for easy finishing operations, thus addressing the limitations of existing technologies.

Implementation Method 1

melting the metal matrix, introducing the metal matrix into the device so as to fill the space between the fiber reinforcement and the portions of the device

Methodology Applied
Scientific EffectMelting: Melting

Implementation Method 2

applying a force to the molding portion and/or to the support portion so as to bring the molding portion and the support portion together and to reduce the space between the fiber reinforcement and the portions of the device, to impregnate the fiber reinforcement with the metal matrix

Methodology Applied
Scientific EffectCompression: Compression

Implementation Method 3

under vacuum, enabling efficient production of parts with improved thermal and electrical performance

Methodology Applied
Scientific EffectVacuum: Vacuum

Data Source

PatentUS10843257B2Method for manufacturing a part out of a metal matrix composite material, and related device
Publication Date: 2020.11.24 SAFRAN ELECTRONICS & DEFENSE (FR)
  • US10843257B2 patent drawing
  • US10843257B2 patent drawing

AI summary

A method (S) for manufacturing a part (1) out of a metal matrix composite material, including the following steps: opening (S1) a device (10) that includes a supporting portion (14) and a molding portion (14); placing (S2) a fibrous reinforcement into the device (10); sealably closing (S3) the device (10) by providing a space between the fibrous reinforcement (2) and the device portions; feeding (S4) the molten metal matrix (3) into the device (10) such as to fill the space between the fibrous reinforcement (2) and the device portions (13, 14); and applying (S5) a force onto the equipment (10) such as to impregnate the fibrous reinforcement (2) with the metal matrix (3).