Prechamber Spark Plug Hole Pattern for Lean-Burn Flame Jets

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Solution Overview

Problem

Conventional prechamber spark plugs in lean burn engines face issues such as inadequate fuel concentration at the spark gap, chaotic flow fields leading to ignition delay or flame quenching, insufficient mixing with residual gases, and slow burn rates, resulting in poor combustion performance.

Innovation Solution

A prechamber design with a specific geometry and hole pattern that creates a spiral flow pattern with higher velocity at the periphery and center, featuring a rotational offset and penetration angle for the holes to induce both radial and axial flow patterns, ensuring uniform velocity fields and fuel stratification to enhance flame kernel development and ignition.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If conventional prechamber spark plugs are used with simple combustion chamber design, then device complexity is reduced, but combustion performance deteriorates due to inadequate fuel concentration and chaotic flow fields

Engineering Contradiction:
Improveprechamber geometry complexityVSAvoidcombustion performance
Core Design Contradiction:
Device complexityVSProductivity

Solution Approach 1:

The prechamber is divided into distinct functional zones: a fuel concentration zone near the spark gap with specific geometry (smaller volume, controlled aspect ratio) to concentrate fuel-air mixture, and a combustion zone with larger volume for flame development. Multiple precisely positioned holes (typically 3-5 holes of specific diameter and orientation) create segmented flow patterns that organize the chaotic flow into structured spiral and radial flows, improving fuel distribution without excessive overall complexity

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different regions of the prechamber are given different geometric properties to optimize local functions. The fuel concentration region has specific dimensions and hole patterns designed to create high-velocity jets that concentrate fuel near the spark gap. The combustion region has different geometry to support flame kernel development and growth. This local differentiation of geometric quality enables improved combustion performance while maintaining reasonable overall device complexity

Inventive Principle:
Principle #3Local quality

2Productivity

If prechamber geometry is optimized for fuel concentration and flow control, then combustion performance improves, but manufacturing precision requirements increase

Engineering Contradiction:
Improvecombustion performanceVSAvoidhole pattern precision
Core Design Contradiction:
ProductivityVSManufacturing precision

Solution Approach 1:

The design specifies optimized parameter ranges rather than exact values, providing manufacturing tolerance. Hole diameters are specified within ranges (e.g., 0.5-1.5mm) rather than single values, and the number of holes is given as a range (3-5 holes) rather than a fixed number. Aspect ratios and volume ratios are defined as ranges that maintain the essential flow patterns and fuel concentration effects. This parameter-based approach with specified tolerances enables achieving improved combustion performance while accommodating normal manufacturing variations

Inventive Principle:
Principle #35Parameter changes

3Use of energy by moving object

If lean fuel mixtures are used to improve efficiency, then energy efficiency improves, but combustion stability deteriorates with conventional spark plugs due to poor flame kernel development

Engineering Contradiction:
Improveenergy efficiencyVSAvoidcombustion stability
Core Design Contradiction:
Use of energy by moving objectVSReliability

Solution Approach 1:

The prechamber geometry is designed to preliminarily organize the fuel-air mixture into concentrated streams and structured flow patterns (spiral and radial flows) before ignition occurs. The hole patterns create pre-conditioned flow fields that guide the flame kernel development in predictable directions. This preliminary organization of the combustible mixture and flow structure ensures stable flame propagation even with lean mixtures, maintaining combustion reliability while enabling efficient lean burn operation

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

This design achieves higher momentum flame jets and faster combustion rates by concentrating fuel at the periphery and reducing ignition delay, while preventing autoignition and flame quenching, leading to improved combustion performance in lean fuel mixtures.

Implementation Method 1

one or more holes including a hole axis that defines a rotational offset for creating a spiral flow pattern of the fuel-air mixture in the prechamber volume

Methodology Applied
Scientific EffectSpiral flow pattern: Vortex Ring

Implementation Method 2

provide a radial flow and an axial flow

Methodology Applied
Scientific EffectRadial flow: Convection

Implementation Method 3

which can exhibit both radial and axial air-fuel ratio stratification

Methodology Applied
Scientific EffectAxial flow: Convection

Implementation Method 4

concentrate fuel at the spark gap region of the spark plug

Methodology Applied
Scientific EffectFuel concentration:

Implementation Method 5

the flow field forces within the spark gap region may be chaotic resulting in zones with either very low flow fields or very high flow fields

Methodology Applied
Scientific EffectFlow field forces:

Implementation Method 6

the configuration of the prechamber may not mix in-filling streams with residual gases to sufficiently lower the temperature inside of the prechamber

Methodology Applied
Scientific EffectMixing: Convection

Implementation Method 7

the configuration of the prechamber may not result in sufficiently fast burn rates with lean fuel mixtures resulting in deployment of flame jets into the main combustion chamber

Methodology Applied
Scientific EffectCombustion: Combustion

Implementation Method 8

which can exhibit both radial and axial air-fuel ratio stratification to afford particular combustion performance characteristics

Methodology Applied
Scientific EffectFlame jets: Jet

Data Source

PatentEP2751408B1Method and apparatus for achieving high power flame jets and reducing quenching and autoignition in prechamber spark plugs for gas engines
Publication Date: 2024.03.20 PROMETHEUS APPLIED TECHNOLOGIES LLC
  • EP2751408B1 patent drawingFigure 1~2
  • EP2751408B1 patent drawingFigure 3~4
  • EP2751408B1 patent drawingFigure 5~6

AI summary

A prechamber spark plug may have a prechamber having a pre-determined aspect ratio and hole pattern to achieve particular combustion performance characteristics. The aspect ratio and hole pattern may induce a rotational flow of fuel-air in-filling streams inside the prechamber volume. The rotational flow of the fuel-air mixture may include both radial flow and axial flow characteristics based on the aspect ratio and hole pattern. Axial flow characteristics can include a first axial direction proximate the periphery of the rotational flow and a counter second axial direction approaching the center of the rotational flow. The rotational flow, the radial flow and the axial flow may be adjusted by alteration of the aspect ratio and hole pattern to achieve particular combustion performance characteristics in relation to a wide variety of spark gap geometries.