Estimating Turbomachine Fuel Temperature via Oil and Spool Data

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Solution Overview

Problem

Existing turbomachines require multiple temperature sensors to determine fuel temperature, making them heavy and costly, which complicates control and measurement processes.

Innovation Solution

A method that estimates the fuel temperature leaving the oil/fuel exchanger by measuring the temperature of oil entering the engine spaces and the rotational speed of the high-pressure spool, reusing existing data to calculate the fuel temperature without a specific sensor, achieving precision within ±10°C.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If a temperature sensor is installed at the inlet of the injectors to measure fuel temperature, then the fuel temperature measurement accuracy is improved, but the device complexity and cost increase due to additional sensors

Engineering Contradiction:
Improvefuel temperature measurement accuracyVSAvoidmultiplicity of measuring means
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system uses existing sensors (oil temperature sensor and rotational speed sensor) to calculate fuel temperature through a computational model, rather than adding a dedicated fuel temperature sensor. The calculation method allows the system to self-determine fuel temperature using available data about oil temperature, rotational speed, and exchanger efficiency

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent introduces a calculation method that acts as an intermediary between existing sensor measurements and the desired fuel temperature information. By using the oil temperature and rotational speed as intermediate parameters, the system derives fuel temperature without direct measurement, reducing sensor requirements

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If multiple temperature sensors are installed in the turbomachine to monitor fuel and oil temperatures, then the temperature measurement reliability is improved, but the weight of the turbomachine increases

Engineering Contradiction:
Improvetemperature monitoring reliabilityVSAvoidturbomachine weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The system reuses existing sensor data (oil temperature and rotational speed measurements) to calculate fuel temperature, eliminating the need for additional temperature sensors. This approach maintains temperature monitoring reliability while avoiding the weight penalty of extra sensors

Inventive Principle:
Principle #25Self-service

3Measurement precision

If multiple temperature sensors are installed to accurately measure fuel temperature, then the measurement precision is improved, but the manufacturing cost increases

Engineering Contradiction:
Improvefuel temperature measurement precisionVSAvoidmanufacturing cost
Core Design Contradiction:
Measurement precisionVSEase of manufacture

Solution Approach 1:

The patent replaces expensive dedicated fuel temperature sensors with a computational approach using existing inexpensive sensors. The calculation method provides sufficient precision for fuel temperature measurement without the high cost of additional sensing hardware

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

Solution Approach 2:

The existing oil temperature sensor and rotational speed sensor serve multiple functions: monitoring oil conditions and calculating fuel temperature. This multi-functionality eliminates the need for separate fuel temperature sensing equipment, reducing manufacturing costs

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 method allows for accurate estimation of fuel temperature entering the injectors without adding sensors, reducing the complexity and cost of turbomachine systems while maintaining precision.

Implementation Method 1

an oil/fuel exchanger upstream of the hydromechanical unit, fuel and oil from the engine spaces passing through the oil/fuel exchanger

Methodology Applied
Scientific EffectHeat exchange: Heat Exchanger

Data Source

PatentUS10018519B2Method of estimating the temperature of the fuel leaving a turbomachine exchanger
Publication Date: 2018.07.10 SAFRAN AIRCRAFT ENGINES SAS
  • US10018519B2 patent drawing
  • US10018519B2 patent drawing
  • US10018519B2 patent drawing

AI summary

A method for estimating the temperature of the fuel entering a turbomachine injector, the turbomachine including engine spaces and an oil/fuel exchanger upstream of the injector, the engine spaces and the oil/fuel exchanger having oil passing through them, the oil/fuel exchanger having an efficiency, the engine spaces including a high-pressure spool, the method including (a) measuring the temperature of the oil entering the engine spaces; (b) measuring the rotational speed of the high-pressure spool; (c) calculating the temperature of the fuel leaving the oil/fuel exchanger using the temperature of the oil entering the engine spaces and the rotational speed of the high-pressure spool.