Welding Torch Nozzle Structure to Suppress Shield Gas Vortices

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Solution Overview

Problem

The existing welding torch designs suffer from a shortened laminar flow length of the shield gas stream, leading to vortex generation and compromised welding quality due to the configuration of the gas path within the nozzle.

Innovation Solution

A welding torch design featuring a cylindrical tip body, an orifice member with a first ring-like space, and a nozzle with a second ring-like space, where the second space is sealed by a large radius part and a tapered flow straightening wall, guiding the shield gas to extend its laminar flow length and reduce vortex generation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Length of stationary object

If the space inside the nozzle extends toward the torch base side, then the gas path is lengthened, but a drift including vortex is generated in the gas stream, shortening the laminar flow length

Engineering Contradiction:
Improvenozzle space lengthVSAvoidlaminar flow length
Core Design Contradiction:
Length of stationary objectVSReliability

Solution Approach 1:

The nozzle space is segmented into two distinct ring-like spaces: a first ring-like space between the tip body and orifice member, and a second ring-like space between the orifice member and nozzle. This segmentation allows the gas to flow through separate zones with different flow characteristics, preventing vortex formation while maintaining adequate path length.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The orifice member acts as an intermediary component between the tip body and nozzle, creating the first ring-like space that mediates the gas flow. This intermediate space with its emission holes serves as a transition zone that prevents direct vortex formation in the main nozzle space.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Productivity

If the second ring-like space is opened, then the gas path is extended, but vortex generation occurs reducing welding quality

Engineering Contradiction:
Improvegas flow path extensionVSAvoidwelding quality
Core Design Contradiction:
ProductivityVSManufacturing precision

Solution Approach 1:

The sealing part is positioned to substantially close the second ring-like space on the torch base side, creating a preliminary barrier that prevents gas from flowing backward and forming vortices. This anti-action is built into the structure to counteract the natural tendency toward vortex formation.

Inventive Principle:
Principle #9Preliminary anti-action

Solution Approach 2:

The sealing part is formed by a large radius part on the orifice member edge, using curved geometry to smoothly guide the gas flow and prevent sharp edges that would trigger vortex formation. The tapered surface with increasing radius provides smooth flow transition.

Inventive Principle:
Principle #14Spheroidality (Curvature)

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 extended laminar flow length of the shield gas stream ensures a wider shield width at the welding target point, enhancing the welding quality by minimizing vortex-induced drift and improving gas efficiency.

Implementation Method 1

a drift including a vortex may be generated in a gas stream that is emitted from the second emission hole and moving toward the torch edge side in the space inside the nozzle

Methodology Applied
Scientific EffectVortex: Vortex Ring

Implementation Method 2

the extended laminar flow length of the shield gas stream ensures a wider shield width at the welding target point

Methodology Applied
Scientific EffectLaminar flow: Laminar Flow

Data Source

PatentEP4186629A1Welding torch
Publication Date: 2023.05.31 DAIHEN CORP
  • EP4186629A1 patent drawingFigure 1
  • EP4186629A1 patent drawingFigure 2~3
  • EP4186629A1 patent drawingFigure 4

AI summary

A welding torch (A1) includes: a cylindrical tip body (2) extending in an axis line (Ox) direction; an orifice member (3) arranged on a radially outer side of the tip body, between which and the tip body a first ring-like space (21) is formed; a cylindrical nozzle (4) arranged on a radially outer side of the orifice member with an interposition of a second ring-like space (411) and having an edge on one side in the axis line direction. The tip body has a first emission hole (22) via which an inner space of the tip body communicates with the first ring-like space, and the orifice member has a second emission hole (34) via which the first ring-like space communicates with the second ring-like space. The second ring-like space is substantially closed by a sealing part on another side in the axis line direction, and an outlet opening (341) of the second emission hole is arranged close the sealing part (36).