Superconducting Motor Power Link Quench Detection Control
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Solution Overview
Problem
Existing methods struggle to reliably detect a quench phenomenon in superconducting power supply links for AC current in aircraft electric motors due to the inductive component masking the resistive component, which can lead to excessive Joule losses and damage.
Innovation Solution
A controller for the power supply circuit that multiplies a voltage signal with a synchronized sinusoidal signal to isolate the resistive component, using a low-pass filter to detect quench phenomena, and inhibits the inverter control if the threshold is exceeded, thereby preventing excessive current supply.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of manufacture
If conventional voltage monitoring is used to detect quench in superconducting AC links, then the detection method is simple, but the inductive component masks the resistive component making detection unreliable
Solution Approach 1:
The voltage signal is segmented into resistive and inductive components through multiplication with synchronized sinusoidal signals. This segmentation allows the resistive component (which indicates quench) to be isolated and detected separately from the dominant inductive component, resolving the masking problem while maintaining detection reliability
Solution Approach 2:
Synchronized sinusoidal signals act as intermediaries to extract the resistive component from the total voltage signal. By multiplying the measured voltage with these intermediary sinusoidal signals, the method transforms the uninterpretable total voltage into a usable resistive component signal that reliably indicates quench conditions
2Duration of action of stationary object
If the inverter continues to supply current during a quench transition, then power supply continuity is maintained, but excessive Joule losses occur causing damage to electrical circuits
Solution Approach 1:
The control system takes preliminary action by detecting the resistive component increase before excessive Joule losses occur. The method continuously monitors the resistive component and inhibits the inverter control output as soon as quench is detected, preventing the harmful effects of continued current supply during the transition to normal resistive state
Solution Approach 2:
The system uses feedback by continuously monitoring the resistive component of the voltage signal and using this information to control the inverter output. When the resistive component exceeds a threshold indicating quench, the feedback loop immediately inhibits the control signal, creating a closed-loop protection system that prevents damage while maintaining normal operation during superconducting state
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 rapid and reliable detection of quench phenomena, preventing damage by limiting current supply and maintaining system integrity.
Implementation Method 1
multiplying the first signal and a sinusoidal signal synchronized with the second signal to obtain a third signal that is representative of the resistive component of the voltage measured across the terminals of the superconducting power supply link
Implementation Method 2
The controller also comprises electronic circuitry configured to low-pass filter the result of the multiplication to obtain the third signal
Implementation Method 3
a superconducting power supply link configured to supply the electric motor with power
Implementation Method 4
detect warning signs of such a transition in order to avoid excessive losses through the Joule effect that could damage the electrical power supply circuits
Data Source
AI summary
A method, which is executed by a controller, for controlling a power supply circuit of an electric motor, the power supply circuit comprising an inverter supplying the motor with power via a power supply link, the method comprising detecting an increase in the voltage across the terminals of the power supply link while overcoming the inductive component of the impedance of the power supply link, and inhibiting an output for controlling the inverter if the increase in voltage exceeds a predetermined value for a predetermined duration. Also a controller for a power supply circuit that is configured to execute the method, an electrical power supply system for a motor and an aircraft comprising such a system and a control method.


