Plasma Torch Nozzle Throat Design for Jet Stability

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Solution Overview

Problem

Conventional plasma arc torch nozzles suffer from inefficient energy transfer due to rapid jet expansion and arc instability, leading to reduced performance and quality in cutting and welding operations.

Innovation Solution

A nozzle configuration with distinct throat regions, including a throat inlet, acceleration, and expansion regions, designed to stabilize and focus the plasma jet, minimizing expansion and arc contact with nozzle walls, thereby optimizing plasma arc performance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If a conventional nozzle is used, then the structure is simple, but the plasma jet expands rapidly causing energy loss and reduced performance

Engineering Contradiction:
Improvecutting performanceVSAvoidjet energy loss
Core Design Contradiction:
ProductivityVSLoss of energy

Solution Approach 1:

The nozzle throat is divided into three distinct segmented regions: a compression region with a converging wall angle of 15-30 degrees to compress and focus the plasma jet, a constant diameter region with a length of 0.5-2 times the throat diameter to maintain focused flow, and an expansion region with a diverging wall angle of 5-15 degrees for controlled expansion. This segmentation allows each region to perform its specific function optimally, preventing rapid uncontrolled expansion and reducing energy loss.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention changes the geometric parameters of the nozzle throat, specifically using a converging wall angle of 15-30 degrees in the compression region and a diverging wall angle of 5-15 degrees in the expansion region. These parameter changes optimize the plasma flow characteristics, maintaining jet focus and reducing energy loss while improving cutting performance.

Inventive Principle:
Principle #35Parameter changes

2Ease of manufacture

If the nozzle throat shape is conventional, then manufacturing is easy, but arc instability occurs reducing performance

Engineering Contradiction:
Improvenozzle manufacturingVSAvoidarc stability
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

Different regions of the nozzle throat are given different local geometric qualities: the compression region has a steeper converging angle (15-30 degrees) to focus the arc, the constant diameter region maintains a uniform diameter to stabilize flow, and the expansion region has a gentler diverging angle (5-15 degrees) for controlled expansion. These localized quality variations ensure arc stability while remaining manufacturable using standard machining processes.

Inventive Principle:
Principle #3Local quality

3Device complexity

If the plasma jet is allowed to expand freely, then the nozzle structure is simple, but jet thrust and focus are lost

Engineering Contradiction:
Improvenozzle structureVSAvoidjet thrust
Core Design Contradiction:
Device complexityVSForce

Solution Approach 1:

The nozzle is segmented into three functional regions that work together to maintain jet thrust: the compression region concentrates the plasma to increase velocity and thrust, the constant diameter region maintains this focused high-velocity flow over a sufficient length (0.5-2 times throat diameter), and the expansion region provides controlled expansion that preserves momentum. This segmentation achieves high jet thrust with a relatively simple monolithic nozzle structure.

Inventive Principle:
Principle #1Segmentation

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 optimized nozzle configuration results in a more focused and controlled plasma jet, enhancing cutting precision and process efficiency by reducing energy loss and arc instability.

Implementation Method 1

an acceleration region that is disposed downstream of the throat inlet region and fluidly connected to the throat inlet region to compress the gas and accelerate the flow of the gas

Methodology Applied
Scientific EffectPressure gradient: Pressure Gradient

Implementation Method 2

as they leave the nozzle, the jets are highly under-expanded and very focused. However, as the jet leaves the nozzle it begins to expand rapidly.

Methodology Applied
Scientific EffectRapid expansion: Pressure Gradient

Data Source

PatentUS9560733B2Nozzle throat for thermal processing and torch equipment
Publication Date: 2017.01.31 LINCOLN GLOBAL INC
  • US9560733B2 patent drawing
  • US9560733B2 patent drawing
  • US9560733B2 patent drawing

AI summary

A nozzle assembly includes an upper portion defining an opening for receiving a gas and a longitudinally extending cylindrical body portion adjacent to the upper portion and defining a passageway for the gas. The nozzle assembly also includes a tip portion adjacent to the body portion, with the tip portion defining a throat channel. The throat channel includes a throat inlet region that focuses a flow of the gas. The throat inlet region is fluidly connected to the passageway via a throat inlet opening. The throat channel also includes an acceleration region that is disposed downstream of the throat inlet region and fluidly connected to the throat inlet region to compress the gas and accelerate the flow of the gas. The throat channel further includes an expansion region disposed downstream of the acceleration region and fluidly connected to the acceleration region to allow the gas to expand.