Aircraft Fuel Metering Hardware Detection for Adaptive Control Current
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Existing turbomachine fuel metering systems require manual software updates when hardware configurations change, risking operational issues due to mismatched control currents, and lack a method to automatically adapt to different hardware configurations.
Innovation Solution
A method to detect fuel metering unit hardware configurations by measuring output voltages at the equipment, using a control voltage to identify specific voltage responses, allowing automatic adaptation of control currents based on the detected configuration.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If manual software updates are used to adapt to hardware configuration changes, then control current accuracy can be maintained, but operational complexity and maintenance time increase
Solution Approach 1:
The protection computer automatically detects the FMU hardware configuration by measuring output voltages and autonomously adapts the control current parameters without requiring manual software updates. The system performs self-identification and self-adjustment during the power-up phase, eliminating the need for human intervention in configuration adaptation.
Solution Approach 2:
The system performs hardware configuration detection and control current adaptation during the initial power-up phase before normal operation begins. This preliminary action ensures that the correct control parameters are established before fuel metering operations start, preventing operational issues from the outset.
2Manufacturing precision
If protection computers manually update software to match hardware changes, then control precision is maintained, but device complexity increases
Solution Approach 1:
The protection computer automatically detects the FMU hardware configuration by measuring output voltages and autonomously adapts the control current parameters without requiring manual software updates. The system performs self-identification and self-adjustment during the power-up phase, eliminating the need for human intervention in configuration adaptation.
Solution Approach 2:
The patent replaces the manual software update process with an automated electrical measurement and processing system. Instead of requiring human operators to manually configure software parameters, the system uses voltage measurement circuits and processor-based automatic parameter adaptation to achieve the same control precision.
3Adaptability or versatility
If different FMU models are used during maintenance, then operational flexibility improves, but risk of mismatched control currents increases
Solution Approach 1:
The system automatically adjusts control current parameters based on the detected FMU hardware configuration. By measuring output voltages and identifying the specific FMU model, the protection computer modifies the control current parameters to match the actual hardware characteristics, ensuring proper operation across different FMU models.
Solution Approach 2:
The system uses voltage measurement at the FMU output as feedback to identify the hardware configuration and adjust control parameters accordingly. This feedback mechanism allows the protection computer to adapt to different FMU models based on their actual electrical characteristics, ensuring reliable control current matching.
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
Enables automatic detection and adaptation of control currents to different fuel metering unit models, ensuring reliable turbomachine protection without manual software updates, thus preventing catastrophic events.
Implementation Method 1
a first channel comprising a first measuring unit capable of measuring a first voltage Vs1 at the equipment output and a second channel comprising a second measuring unit capable of measuring a second voltage Vs2 at the equipment output
Data Source
Figure 1
Figure 2
Figure 3
AI summary
The invention relates to a method for detecting a hardware configuration of a device intended to be housed on board an aircraft and controlled by a protection computer (8), comprising a power supply able to supply power to the device, a first measurement module (16) able to measure a first voltage Vs1 at the output of the device and a second measurement module (18) able to measure a second voltage Vs2 at the output of the device: a) Send a control voltage Vc at the input of the device; b) Measure the first voltage Vs1 and the second voltage Vs2; c) Deduce the hardware configuration of the device from the values of the measured first and second voltages Vs1 and Vs2.