Dispersion-Hardened Piston Ring via Gas-Phase Carbide Nanoparticles

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Solution Overview

Problem

Current methods for producing dispersion-hardened piston rings with carbide nanoparticles are limited by the inability to effectively transport and deposit discrete nanoparticles, resulting in agglomerated coatings rather than finely dispersed ones, which compromises wear resistance and adhesion due to differences in thermal expansion and mechanical properties.

Innovation Solution

A method involving the use of a thermal spraying process where carbide nanoparticle precursors react in a gas flow to form nanoparticles, which then coagulate with microcrystalline particles, utilizing a carrier gas like nitrogen and a transition metal halide precursor, such as WCl6, to produce a dispersion-hardened object like a piston ring with enhanced wear resistance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If discrete carbide nanoparticles are used for dispersion hardening, then wear resistance and material strength increase, but particle transport and deposition become impossible under normal pressure conditions

Engineering Contradiction:
Improvewear resistanceVSAvoidparticle transport
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The patent changes the pressure parameter from normal to reduced pressure conditions, enabling the transport of discrete carbide nanoparticles through the spray gun. This parameter modification allows nanoparticles (1-200 nm) to be conveyed without forming agglomerates, achieving dispersion hardening with fine particles that provide superior wear resistance.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent introduces a carrier gas as an intermediary medium to transport the carbide nanoparticles. The carrier gas flows through the spray gun, carrying the fine particles through the reduced pressure zone and depositing them on the substrate, thereby solving the transport problem without requiring direct mechanical handling of the nanoparticles.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of manufacture

If agglomerated nanoparticles are used instead, then particle transport becomes possible, but the coating contains microparticles and agglomerates rather than discrete nanoparticles

Engineering Contradiction:
Improveparticle transportVSAvoidparticle dispersion
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

The patent applies reduced pressure conditions throughout the spray process, creating a controlled environment where discrete nanoparticles remain separated during transport. This pressure parameter change prevents the formation of agglomerates that would otherwise occur at normal pressure, maintaining manufacturing precision while enabling particle transport.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent replaces mechanical particle handling and transport systems with a gas-phase transport mechanism under reduced pressure. This substitution allows discrete nanoparticles to be conveyed through the spray gun using gas flow dynamics rather than mechanical means, preventing agglomeration and maintaining particle dispersion.

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

3Reliability

If metal carbides are introduced into a metallic matrix, then adhesion is limited to surface wetting without metallurgical bonding

Engineering Contradiction:
ImproveadhesionVSAvoidbond strength
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The patent utilizes phase transitions during the thermal spray process, where the metallic matrix material melts and forms a molten layer on the substrate. The carbide particles are embedded in this molten matrix, and upon cooling, metallurgical bonding occurs between the matrix and substrate, creating strong adhesion rather than mere surface wetting.

Inventive Principle:
Principle #36Phase transitions

Solution Approach 2:

The patent creates a composite material structure where carbide particles are embedded in a metallurgically bonded metallic matrix. The matrix material (such as nickel-based alloys) provides strong adhesion to the substrate through metallurgical bonding, while the carbide particles provide wear resistance, creating a synergistic composite structure.

Inventive Principle:
Principle #40Composite materials

4Ease of manufacture

If plasma spraying is used for molybdenum-based materials, then deposition is achieved, but wear resistance is insufficient for heavily loaded engines

Engineering Contradiction:
ImprovedepositionVSAvoidwear resistance
Core Design Contradiction:
Ease of manufactureVSStrength

Solution Approach 1:

The patent changes the particle material from molybdenum-based materials to fine carbide particles (WC, Cr3C2, TiC, VC) with sizes of 1-200 nm. This material and size parameter change provides significantly higher wear resistance for heavily loaded engine conditions while using thermal spray deposition to achieve coating formation.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent creates a composite coating structure with a metallic matrix and embedded carbide particles. This composite material provides both the deposition capability of thermal spray and the superior wear resistance of carbide particles, overcoming the limitations of molybdenum-based plasma spray coatings.

Inventive Principle:
Principle #40Composite materials

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 enables the production of a piston ring with discrete carbide nanoparticles, improving wear resistance and adhesion by ensuring the nanoparticles are transported and deposited as discrete entities, enhancing the material's strength and reducing wear-related issues in internal combustion engines.

Implementation Method 1

the gas flow behind the combustion chamber being supplied with the aid of a carrier gas at least one carbide nanoparticle precursor which reacts in the gas flow to form a carbide

Methodology Applied
Scientific EffectGas flow transport: Convection

Implementation Method 2

at least one carbide nanoparticle precursor which reacts in the gas flow to form a carbide

Methodology Applied
Scientific EffectChemical reaction: Chemical Bonding

Implementation Method 3

the nanoparticles being produced only in the gas phase and then coagulating with microcrystalline particles of a wettable powder

Methodology Applied
Scientific EffectCoagulation: Coagulation

Implementation Method 4

High Velocity Oxygen Spray (HVOF) technology offers the ability to deposit particles with low thermal impact and high kinetic energy on a substrate to form dense layers with high bond strength

Methodology Applied
Scientific EffectKinetic energy impact: Impact Force

Implementation Method 5

the gas flow behind the combustion chamber being supplied with the aid of a carrier gas

Methodology Applied
Scientific EffectCombustion: Combustion

Data Source

PatentEP2252562B1Method and device for producing a dispersion-hardened object that contains carbide nanoparticles
Publication Date: 2016.09.14 FEDERAL MOGUL BURSCHEID GMBH
  • EP2252562B1 patent drawingFigure 1

AI summary

The invention relates to a method for producing a dispersion-hardened object that contains carbide nanoparticles, said method comprising the production of an object by means of a thermal spraying method. According to the invention, at least one precursor is fed to the gas stream behind the combustion chamber by means of a carrier gas, said precursor reacting in the gas stream to produce a carbide, or carbide nanoparticles are fed via an external thermally stressed nanoparticle generator. A dispersion-hardened object is thus produced, for example a component for an internal combustion enginem such as a piston ring. The method is carried out by means of a thermal spraying device which, in addition to at least one line for feeding a thermal spay powder, also comprises behind the combustion chamber at least one line for feeding a precursor by means of a carrier gas.