Power Module Coolant Flow Monitoring Without Separate Flow Sensors

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Solution Overview

Problem

Existing cooling systems for power semiconductor modules, particularly in aircraft, lack effective monitoring methods to ensure proper coolant flow, relying on temperature-sensitive devices that provide only temperature data without indicating if the coolant flow is within designed parameters, necessitating additional flow sensors.

Innovation Solution

Implementing a monitoring method and unit with integrated temperature sensors along the coolant flow path that measure and compare actual temperature differences with expected values based on module losses and nominal flow conditions to determine coolant flow status, eliminating the need for separate flow sensors.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If temperature-sensitive devices are used to monitor cooling systems, then temperature measurement is achieved, but coolant flow status cannot be determined

Engineering Contradiction:
Improvetemperature measurementVSAvoidcoolant flow status information
Core Design Contradiction:
Measurement precisionVSLoss of information

Solution Approach 1:

The patent changes the parameter being monitored from absolute temperature to temperature difference. By measuring the temperature difference between two points in the coolant flow path and comparing it to an expected temperature difference (calculated from power losses and nominal flow conditions), the system can determine coolant flow status without requiring additional flow sensors. This parameter transformation enables flow status detection using only temperature measurements.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If additional flow sensors are installed to monitor coolant flow, then coolant flow status can be determined, but device complexity and cost increase

Engineering Contradiction:
Improvecoolant flow monitoringVSAvoidsensor quantity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent makes the temperature sensors serve multiple functions: they simultaneously measure both the absolute temperature (for thermal management) and the temperature difference (for flow status monitoring). This multi-functionality eliminates the need for separate flow sensors, reducing device complexity and cost while maintaining reliable coolant flow monitoring.

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

Solution Approach 2:

The patent combines the flow monitoring function with the existing temperature measurement function. By using the same temperature sensors to determine both temperature and flow status through temperature difference measurement, the system merges what would traditionally require separate sensing systems into a single integrated approach.

Inventive Principle:
Principle #5Merging (Combining)

3Reliability

If multiple temperature sensors are arranged along the coolant flow path, then coolant flow status can be inferred, but device complexity increases

Engineering Contradiction:
Improvecoolant flow detectionVSAvoidsensor arrangement
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The temperature sensors arranged along the coolant flow path serve dual purposes: monitoring absolute temperature for thermal management and measuring temperature differences for flow status detection. This multi-functionality justifies the sensor arrangement and eliminates the need for additional dedicated flow sensors.

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

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 coolant flow monitoring by saving space and cost while maintaining redundancy, ensuring reliable coolant flow detection without additional sensors, particularly suitable for aircraft applications.

Implementation Method 1

providing several temperature sensors arranged along the coolant flow path, measuring temperatures at different locations of the coolant flow path by the temperature sensors

Methodology Applied
Scientific EffectTemperature sensing: Thermocouple

Data Source

PatentUS20250314559A1Monitoring a coolant flow of a power electronic semiconductor device
Publication Date: 2025.10.09 AIRBUS (SAS)
  • US20250314559A1 patent drawing
  • US20250314559A1 patent drawing

AI summary

A method for monitoring a cooling system for power electronics, especially on aircraft. For improving monitoring of a cooling system of a power electronic semiconductor device, wherein the cooling system can generate a coolant flow along a coolant flow path over at least one semiconductor power module of the power electronic semiconductor device, the method includes providing several temperature sensors arranged along the coolant flow path, measuring temperatures at different locations of the coolant flow path by the temperature sensors, comparing an actual temperature difference between the temperatures measured with an expected temperature difference calculated on basis of losses of the at least one semiconductor power module and on basis of nominal coolant flow conditions, and determining the status of the coolant flow on basis of the comparison.