Plasma Torch Electrode Cooling Channels for Longer Service Life

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Solution Overview

Problem

Gas-cooled plasma torches have shorter service life and higher operational costs due to intense wear on thermally loaded components, requiring frequent replacement and interrupting the cutting process, compared to liquid-cooled systems.

Innovation Solution

The electrode design for plasma torches incorporates an elongate electrode body with a cavity and strategically positioned openings for enhanced gas flow, allowing for a more efficient cooling system that prolongs the service life of the electrode and reduces wear by distributing cooling gas effectively across the thermally loaded areas.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If gas-cooled plasma torches are used instead of liquid-cooled systems, then construction simplicity and ease of handling are improved, but service life of wearing parts decreases due to insufficient cooling

Engineering Contradiction:
Improveconstruction simplicityVSAvoidservice life of wearing parts
Core Design Contradiction:
Device complexityVSDuration of action of stationary object

Solution Approach 1:

The electrode is divided into multiple functional zones with separate cooling channels: a first cooling channel for the electrode body and a second cooling channel for the emission insert. This segmentation allows independent optimization of cooling for each component, improving overall service life while maintaining the simple gas-cooled design

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different cooling strategies are applied to different parts of the electrode based on their specific thermal loads. The electrode body receives cooling through one channel while the emission insert receives cooling through another channel, with potentially different flow rates and cooling intensities tailored to each component's requirements

Inventive Principle:
Principle #3Local quality

2Temperature

If large volume flows of gas are used for cooling, then cooling effectiveness is improved, but gas consumption increases operational costs

Engineering Contradiction:
Improvecooling effectivenessVSAvoidgas consumption
Core Design Contradiction:
TemperatureVSQuantity of substance

Solution Approach 1:

The total gas flow is segmented into separate streams for different cooling purposes. The first cooling channel and second cooling channel can receive different volumes of cooling gas, allowing optimization of gas distribution to match actual thermal loads of different components, reducing overall gas consumption while maintaining effective cooling

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The cooling system allows independent adjustment of gas flow parameters (volume, pressure, temperature) for each cooling channel. This enables optimization of cooling effectiveness while minimizing gas consumption by matching flow parameters to the actual thermal requirements of each component

Inventive Principle:
Principle #35Parameter changes

3Manufacturing precision

If frequent replacement of wearing parts is performed, then cutting quality is maintained, but productivity decreases due to process interruptions

Engineering Contradiction:
Improvecutting qualityVSAvoidprocess continuity
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The cooling system is designed to prevent excessive wear by maintaining optimal temperatures of the electrode and emission insert through effective cooling. This preliminary protective action extends the service life of wearing parts, allowing them to maintain cutting quality for longer periods without requiring replacement, thus improving process continuity

Inventive Principle:
Principle #10Preliminary action

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 improved cooling mechanism significantly extends the service life of the electrode and maintains cutting quality over a longer period, reducing operational costs and minimizing interruptions during the cutting process.

Implementation Method 1

a cavity (32) which extends in the electrode body (30) from the open end (34) in the direction of the closed end (33), and which is fluidically connected via at least one opening (32c) in the wall thereof to the radial outer side, in relation to the longitudinal axis L, of the electrode body (30)

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 2

The improved cooling mechanism significantly extends the service life of the electrode and maintains cutting quality over a longer period

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Implementation Method 3

an arc (pilot arc) is firstly ignited between a cathode (electrode) and an anode (nozzle) and is subsequently transferred directly to a workpiece in order to thereby make a cut

Methodology Applied
Scientific EffectArc heating: Electric Arc

Implementation Method 4

These gases are ionized and dissociated by the energy of the arc. The resulting plasma jet is used for cutting the workpiece

Methodology Applied
Scientific EffectIonization: Ionisation

Data Source

PatentUS12011789B2Electrodes for gas- and liquid-cooled plasma torches
Publication Date: 2024.06.18 KJELLBERG STIFTUNG
  • US12011789B2 patent drawing
  • US12011789B2 patent drawing
  • US12011789B2 patent drawing

AI summary

A gas conducting unit for a gas-cooled plasma cutting torch, wherein the gas-conducting unit is single-part or multi-part tubular or annular. The gas-conducting unit comprises a single-part or multi-part tubular or annular gas-conducting unit body with a longitudinal axis L1. In a wall of the gas-conducting unit body, there are situated at least one opening, which is inclined by an angle δ in a range of ±15° with respect to the longitudinal axis L1, and at least one second opening, which is inclined radially with respect to the longitudinal axis L1 or which, in a radial plane, is inclined at an angle γ in the range of ±30° from the radial to the longitudinal axis L1.