Aircraft Motor Controller Protection for Regenerated Fault Current

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Aircraft electric propulsion systems face challenges in fault tolerance due to high-power levels and unique grounding schemes, leading to potential safety issues and system instability during faults, as existing protection architectures are not adequately designed to handle the high fault energy and complex power flow dynamics.

Innovation Solution

A fault-tolerant power system architecture is proposed, featuring a motor controller with multiple inverters and inverter controllers that activate short circuits to redirect regenerated current within the system, allowing continued operation and controlled shutdown, while actively managing heat through liquid cooling, and implementing protection logic for various fault scenarios.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If existing protection architectures are used for high-power electric propulsion systems, then system complexity is reduced, but fault tolerance and safety are insufficient due to inadequate handling of high fault energy and complex power flow dynamics

Engineering Contradiction:
Improvefault toleranceVSAvoidprotection system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The protection system is segmented into multiple independent protection circuits, each monitoring specific fault conditions (overcurrent, undervoltage, overtemperature, etc.). This segmentation allows the system to handle high fault energy through specialized dedicated circuits while maintaining overall system reliability without excessive complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The protection system performs preliminary detection and assessment of fault conditions before they escalate. Protection circuits continuously monitor system parameters and trigger protective actions in advance, preventing high-energy faults from developing and maintaining reliability through proactive fault management.

Inventive Principle:
Principle #10Preliminary action

2Reliability

If motor controller opens all switches to protect against faults, then system safety is improved, but regenerated current from spinning motor feeds the fault through freewheeling diodes, creating high-current conditions

Engineering Contradiction:
Improvesystem safetyVSAvoidregenerated fault current
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The protection system converts the potentially harmful regenerated current into a beneficial braking force. By controlling power switches to create active short circuits across motor terminals, the system dissipates regenerated energy as heat in the motor windings and switch resistance, transforming the harmful current feedback into useful mechanical braking while maintaining system safety.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

Solution Approach 2:

The system dynamically changes the electrical parameters (switch states, connection topology) in response to detected faults. When a fault is detected, the control logic transitions the motor controller from normal operation mode to protection mode, altering switch configurations to redirect and dissipate regenerated current safely, thereby eliminating the harmful feedback effect.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If power switches are kept open to isolate faults, then fault propagation is prevented, but system functionality is lost and no controlled operation or shutdown is possible

Engineering Contradiction:
Improvefault isolationVSAvoidcontrolled shutdown capability
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The protection system dynamically adjusts switch states based on the type and severity of detected faults. Rather than statically opening all switches, the system selectively controls individual switches to isolate specific faulty components while maintaining operational capability of healthy sections, enabling both fault isolation and controlled shutdown/graceful degradation.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The protection logic applies different switch control strategies to different phases and components based on localized fault conditions. When a fault is detected in one phase or component, only the affected switches are opened or reconfigured, while other healthy phases continue to operate, providing local fault isolation without complete system shutdown.

Inventive Principle:
Principle #3Local quality

4Power

If multiple motor controllers drive a single multi-phase motor for high power levels, then power capability is increased, but coordination among controllers during faults becomes more complex

Engineering Contradiction:
Improvepropulsion power levelVSAvoidcontroller coordination complexity
Core Design Contradiction:
PowerVSDevice complexity

Solution Approach 1:

Multiple motor controllers are merged into a coordinated system with unified protection logic. The controllers share fault detection data and coordinate their switch control actions through centralized or distributed control architecture, enabling them to operate as an integrated unit that maintains simple coordination patterns even during fault conditions while delivering high combined power output.

Inventive Principle:
Principle #5Merging (Combining)

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

The solution enables safe and controlled operation of electric propulsion systems during faults, reducing exposure to high-energy conditions and maintaining system functionality, even in degraded modes, by effectively managing fault currents and heat dissipation.

Implementation Method 1

activating short circuits in power switches of inverters in a motor controller to redirect current regenerated by a motor

Methodology Applied
Scientific EffectJoule heating: Joule Heating

Implementation Method 2

actively managing heat through liquid cooling

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Implementation Method 3

actively managing heat through liquid cooling

Methodology Applied
Scientific EffectConvection: Convection

Data Source

PatentUS12028009B2Protection system for aircraft electric propulsion motor and motor controller
Publication Date: 2024.07.02 THE BOEING CO
  • US12028009B2 patent drawing
  • US12028009B2 patent drawing
  • US12028009B2 patent drawing

AI summary

A method for protecting an electric propulsion system in response to occurrence of a fault. The method includes the step of activating short circuits in power switches of inverters in a motor controller to redirect current regenerated by a motor which is electrically coupled to the motor controller and mechanically coupled to a propeller. The method further includes feathering the propeller while the motor is regenerating current. The protection logic is designed to address different types of faults, including faults in the high-voltage direct-current bus, faults in the motor controller, and faults in the motor.