Dual Fuel Engine Combustion Control via Segmented Pilot Injection

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Solution Overview

Problem

Dual fuel engines face challenges in controlling combustion timing and stability when switching between gaseous fuel spark-ignited and liquid pilot-ignited modes, particularly due to variations in fuel quality and emissions issues.

Innovation Solution

A method and system for controlling a dual fuel engine by producing a phasing signal indicative of combustion phasing in the gaseous fuel spark-ignited mode, adjusting phasing control parameters to limit errors, and switching to a dual fuel liquid pilot-ignited mode through direct injection of early and second pilot shots of liquid fuel, with or without a spark, to ignite gaseous fuel.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-generated harmful factors

If gaseous fuel is used in spark-ignited mode, then emissions properties are improved, but combustion stability deteriorates

Engineering Contradiction:
ImproveemissionsVSAvoidcombustion stability
Core Design Contradiction:
Object-generated harmful factorsVSReliability

Solution Approach 1:

The fuel injection is segmented into multiple shots (early pilot shot and main injection) rather than a single injection. The early pilot shot creates a premixed charge that ignites first, providing stable combustion initiation, while the main gaseous fuel charge follows. This segmentation allows the engine to maintain emissions benefits of gaseous fuel while achieving combustion stability through the staged injection approach.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

An early pilot shot of liquid fuel is injected and vaporized before the main gaseous fuel charge to create a premixed charge that ignites first. This preliminary action establishes stable combustion conditions that enable reliable ignition and combustion of the subsequent gaseous fuel, solving the combustion stability issue while maintaining the emissions advantages of gaseous fuel operation.

Inventive Principle:
Principle #10Preliminary action

2Adaptability or versatility

If multiple operating modes are implemented, then fuel flexibility is improved, but device complexity increases

Engineering Contradiction:
Improvefuel flexibilityVSAvoidcombustion control complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The fuel injection system is designed to universally handle both liquid fuel and gaseous fuel types using the same injection hardware. The system can operate in multiple modes (liquid-only compression ignition, gaseous fuel spark-ignition, and dual fuel modes) without requiring separate injection systems, thereby achieving fuel flexibility while minimizing the increase in device complexity through a unified multi-functional injection approach.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Productivity

If combustion timing is controlled in premixed charge mode, then combustion efficiency is improved, but measurement precision deteriorates

Engineering Contradiction:
Improvecombustion efficiencyVSAvoidcombustion phasing measurement
Core Design Contradiction:
ProductivityVSMeasurement precision

Solution Approach 1:

A premixed charge indicator is introduced as an intermediary signal to detect and indicate the phasing of the premixed charge combustion. This indicator provides a measurable reference point that allows precise measurement of combustion timing and phasing in premixed charge mode, thereby resolving the measurement precision issue while maintaining the combustion efficiency benefits of premixed charge operation.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS10982601B2Combustion control system and method for switching between spark and pilot-ignited operating modes in dual fuel engine
Publication Date: 2021.04.20 CATERPILLAR INC
  • US10982601B2 patent drawing
  • US10982601B2 patent drawing

AI summary

A method of controlling a dual fuel engine system includes adjusting a phasing control parameter such as air-fuel ratio (AFR), based on a phasing signal to limit an error in a phasing of combustion of gaseous fuel. The cylinder is switched to a dual fuel liquid pilot-ignited mode by commanding direct injection of an early pilot shot of liquid fuel, based on the adjustment to the phasing control parameter, and production of a spark to ignite gaseous fuel in the cylinder. Switching the cylinder to the dual fuel liquid pilot-ignited mode is completed by commanding direct injection of an early pilot shot and a second pilot shot of liquid fuel to ignite gaseous fuel in response to combustion of the early and second pilot shots in the cylinder.