Piston Crown Protrusions for Combustion Flow Control

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Solution Overview

Problem

Direct-injection engines face inefficiencies and increased emissions due to fuel dispersion and interaction with combustion chamber surfaces, leading to uneven fuel-air mixing and higher temperatures, which are exacerbated by swirling air momentum making it difficult to achieve quiescent conditions consistently.

Innovation Solution

The design incorporates a piston crown with a concave bowl and protrusions having asymmetrical side surfaces to redirect and segregate fuel jets radially, counteracting swirling air momentum and guiding the flame towards the center of the combustion chamber for improved mixing and burning.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Use of energy by moving object

If fuel is injected directly into the combustion chamber, then engine efficiency is improved, but fuel dispersion and interaction with chamber surfaces cause increased emissions and uneven mixing

Engineering Contradiction:
Improveengine efficiencyVSAvoidemissions
Core Design Contradiction:
Use of energy by moving objectVSObject-generated harmful factors

Solution Approach 1:

The piston crown is segmented into multiple protrusions (typically 3-6) arranged radially around the combustion chamber center. Each protrusion acts as an independent flow control element that segments the fuel jet into multiple sub-jets, preventing premature dispersion and interaction with chamber surfaces while maintaining efficient combustion.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Each protrusion features asymmetric surface geometry with a concave leading surface facing the fuel injector and a convex trailing surface. This asymmetry creates a flow redirection effect that directs fuel radially outward while preventing backflow, improving mixing uniformity and reducing localized rich/lean zones that cause emissions.

Inventive Principle:
Principle #4Asymmetry

2Quantity of substance

If fuel jets interact with combustion chamber surfaces, then fuel dispersion occurs, but this causes localized rich and lean burning areas increasing emissions

Engineering Contradiction:
Improvefuel dispersionVSAvoidemissions
Core Design Contradiction:
Quantity of substanceVSObject-generated harmful factors

Solution Approach 1:

The protrusions serve as intermediary flow control elements positioned between the fuel injector and the combustion chamber walls. They mediate the fuel jet by redistributing it radially outward in a controlled manner, preventing direct impingement on chamber surfaces while ensuring uniform fuel-air mixing before combustion.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Power

If swirling air momentum is present, then combustion occurs, but flames are carried to one side towards cylinder wall decreasing efficiency

Engineering Contradiction:
ImprovecombustionVSAvoidheat rejection
Core Design Contradiction:
PowerVSLoss of energy

Solution Approach 1:

The protrusions create localized flow control zones at specific radial positions around the combustion chamber. Each protrusion generates a localized counter-swirl effect that opposes the global air swirl, creating a more quiescent central region where combustion can occur more efficiently with reduced heat transfer to cylinder walls.

Inventive Principle:
Principle #3Local quality

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 solution enhances fuel efficiency, reduces heat rejection, and lowers emissions by achieving a more uniform fuel-air mixture and directing flames towards oxygen-rich areas, effectively transforming a swirling combustion system into a quiescent one.

Implementation Method 1

a first side surface having a generally concave shape, the second side surface having a generally flat or convex shape. During operation of the engine, a swirling air mass provided into the combustion chamber through the air intake valve is mixed with a counter-swirling mass of burning air and fuel that has been provided through the fuel injector.

Methodology Applied
Scientific EffectFlow redirection:

Implementation Method 2

The expanding flame counters the swirling air such that the flame is directed towards a center of the combustion chamber where additional oxygen is present to promote an efficient burning of fuel in the cylinder.

Methodology Applied
Scientific EffectMomentum counteraction: Conservation of Momentum

Data Source

PatentUS10774782B2Piston design for flow re-direction
Publication Date: 2020.09.15 CATERPILLAR INC
  • US10774782B2 patent drawing
  • US10774782B2 patent drawing
  • US10774782B2 patent drawing

AI summary

A piston for an internal combustion engine includes a crown portion having a bowl that includes a plurality of protrusions. Each of the plurality of protrusions includes a first side surface and a second side surface, the first side surface having a generally concave shape, the second side surface having a generally flat or convex shape.