Fuel Cell Gas Temperature Correction via Iterative Thermal Modeling

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Solution Overview

Problem

In fuel cell systems, accurately measuring the temperature of gases flowing through conduits is challenging due to turbulent flow and varying speeds, which can lead to inaccurate measurements by physical sensors, especially when these sensors are exposed to environmental conditions in confined spaces.

Innovation Solution

A controller system that uses a temperature sensor within the conduit and a wall temperature sensor to iteratively apply a thermal model, accounting for conductive, convective, and radiative heating effects, to calculate a predicted temperature value, adjusting input values based on differences between measured temperatures until a predetermined criterion is met, thereby correcting the temperature measurement.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If physical sensors are placed directly in the gas flow within confined conduits to measure temperature, then measurement accessibility is improved, but measurement accuracy deteriorates due to conductive and radiative heating from conduit walls

Engineering Contradiction:
Improvesensor accessibilityVSAvoidtemperature measurement accuracy
Core Design Contradiction:
Ease of operationVSMeasurement precision

Solution Approach 1:

The patent introduces an intermediary computational model that acts as a mediator between the physical sensor reading and the actual gas temperature. The model uses the sensor measurement along with conduit wall temperature and flow conditions to calculate the true gas temperature, effectively decoupling the sensor from direct thermal interference while preserving measurement capability

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent replaces the direct physical measurement approach with a computational/algorithmic system. Instead of relying solely on physical sensor accuracy, the system uses mathematical modeling incorporating heat transfer equations to compute the actual temperature, substituting physical measurement limitations with computational correction

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

2Reliability

If sensors are sheltered to protect from environmental conditions and turbulent gas flow, then sensor durability is improved, but measurement accuracy deteriorates due to additional thermal interference

Engineering Contradiction:
Improvesensor durabilityVSAvoidtemperature measurement accuracy
Core Design Contradiction:
ReliabilityVSMeasurement precision

Solution Approach 1:

The computational model serves as an intermediary that compensates for the thermal interference introduced by protective sheltering. By incorporating the shelter geometry and material properties into the heat transfer model, the system calculates the true gas temperature despite the sensor being thermally isolated by the protective structure

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent changes the approach from directly measuring physical temperature to measuring multiple parameters (sensor temperature, wall temperature, flow velocity, shelter properties) and computationally deriving the gas temperature. This parameter transformation allows the system to account for shelter-induced thermal effects

Inventive Principle:
Principle #35Parameter changes

3Measurement precision

If iterative thermal modeling is applied to correct temperature measurements, then measurement accuracy is improved, but computational complexity increases

Engineering Contradiction:
Improvetemperature measurement accuracyVSAvoidcontrol system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent implements a feedback mechanism where the iterative thermal model continuously compares predicted sensor temperatures with actual measurements and adjusts the gas temperature calculation accordingly. This feedback loop refines the temperature estimate until convergence, improving accuracy through systematic error correction

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent applies partial action by performing iterative corrections only when necessary (when initial measurements indicate significant thermal interference) rather than continuously. The iteration stops when a predetermined accuracy threshold is met or a maximum number of iterations is reached, balancing computational effort with measurement accuracy

Inventive Principle:
Principle #16Partial or excessive 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 approach enhances the accuracy of temperature measurement and control within fuel cell systems, improving efficiency and extending sensor lifespan by accounting for complex heating effects, and is applicable to other enclosed spaces beyond fuel cell systems.

Implementation Method 1

conductive, convective and radiative heating effects on the sensor

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Implementation Method 2

conductive, convective and radiative heating effects on the sensor

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 3

conductive, convective and radiative heating effects on the sensor

Methodology Applied
Scientific EffectThermal radiation: Thermal Radiation

Data Source

PatentUS10608269B2Temperature measuring method
Publication Date: 2020.03.31 CERES INTELLECTUAL PROPERTY COMPANY LIMITED
  • US10608269B2 patent drawing
  • US10608269B2 patent drawing
  • US10608269B2 patent drawing

AI summary

A fuel cell system comprising a controller, a temperature sensor that has a physical presence in a conduit within the system to measure the temperature of the fluid at a point within the conduit (Tg) and a wall temperature sensor for sensing a temperature of a wall of the conduit (Tw). The controller takes Tg and Tw as inputs and applies an equation with known constants to calculate measurement error of Tg based on the local flow temperature and geometry and arrives at a calculated temperature. The equation may be applied iteratively until the difference between the calculated temperature and Tg is below an acceptable value when the calculated temperature can then be assumed to be an accurate representation of the actual gas temperature at the Tg measurement point. The direction of calculation is controlled by the relative difference between Tg and Tw.