Gaseous Fuel Specific Gravity Estimation via Acoustic Pressure Waves

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Solution Overview

Problem

Multi-fuel engines face challenges in regulating fuel flow rate and air/fuel ratio when operating with gaseous fuels of unknown composition, such as natural gas, due to unknown specific gravity and lower heating value, which can lead to performance issues.

Innovation Solution

A method and system that estimate the specific gravity of gaseous fuels by generating a pressure wave in the gas rail of the engine and determining its frequency, using this information to calculate the speed of sound and subsequently the specific gravity, allowing for accurate fuel flow regulation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If analytical techniques are employed to continuously monitor fuel composition, then measurement precision of specific gravity is improved, but device complexity and cost increase

Engineering Contradiction:
Improvespecific gravity measurementVSAvoidanalytical monitoring system
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent replaces complex analytical instruments with a simple acoustic measurement system. By measuring the speed of sound in the fuel through a transducer and using the relationship between sound speed and specific gravity, the system achieves accurate fuel property monitoring without expensive gas chromatographs or mass spectrometers. The sound speed measurement is converted to specific gravity through established thermodynamic relationships.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The fuel itself serves as the measurement medium. The acoustic properties of the fuel (sound speed) directly provide the information needed for specific gravity determination. The fuel's own physical properties are exploited for measurement rather than requiring external analytical reagents or complex sampling systems.

Inventive Principle:
Principle #25Self-service

2Measurement precision

If fuel composition is unknown and changing, then adaptability of multi-fuel engine is reduced, but measurement precision of fuel properties becomes more critical

Engineering Contradiction:
Improvefuel property measurementVSAvoidmulti-fuel operation capability
Core Design Contradiction:
Measurement precisionVSAdaptability or versatility

Solution Approach 1:

The system continuously monitors fuel specific gravity and provides real-time feedback to the engine control unit. Based on the measured specific gravity, the ECU dynamically adjusts fuel injection timing, duration, and quantity to optimize combustion. This closed-loop control maintains engine performance across varying fuel compositions without requiring manual intervention or fuel identification.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The measurement and control system is designed to handle dynamic changes in fuel properties. The acoustic sensing system continuously tracks specific gravity variations, and the control system adapts injection parameters in real-time. This dynamic response capability allows the engine to maintain optimal performance even when fuel composition changes during operation.

Inventive Principle:
Principle #15Dynamics

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 approach enables precise regulation of fuel flow and air/fuel ratio, improving engine performance even when operating with fuels of unknown properties, by accurately determining the specific gravity of gaseous fuels in real-time.

Implementation Method 1

establishing a pressure wave in the gas rail by opening and closing the gas valve, wherein the pressure wave travels at a speed of sound in the gaseous fuel

Methodology Applied
Scientific EffectSpeed of sound: Speed of Sound

Data Source

PatentUS9546941B2Method and system for estimating the specific gravity of an unknown fuel source in a multi-fuel engine
Publication Date: 2017.01.17 CATERPILLAR INC
  • US9546941B2 patent drawing
  • US9546941B2 patent drawing
  • US9546941B2 patent drawing

AI summary

A method for estimating a specific gravity of a gaseous fuel is described. The gaseous fuel may power an engine and the engine may include a cylinder, a gas valve configured to supply an intake port of the cylinder with the gaseous fuel, a gas rail configured to deliver the gaseous fuel to the gas valve, and a microprocessor adapted to perform the method. The method may comprise establishing a pressure wave in the gas rail by opening and closing the gas valve, wherein the pressure wave travels at the speed of sound in the gaseous fuel. The method may further comprise determining a frequency of the pressure wave in the gas rail, and estimating the specific gravity of the gaseous fuel based on the frequency of the pressure wave.