Aircraft Motor Drive Charging With Bidirectional Converter Switching

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Solution Overview

Problem

Existing aircraft battery charging systems require separate converters and controllers for DC and AC power sources, leading to inefficiencies and the need for dedicated equipment.

Innovation Solution

An adaptive battery charging system that integrates a bidirectional converter, controllable contactors, and a motor controller to enable charging from both DC and AC power sources, utilizing the onboard motor drive system without additional converters, and supports multiple charging modes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If separate dedicated converters and controllers are used for DC and AC charging systems, then charging functionality for different power sources is achieved, but device complexity and equipment quantity increase

Engineering Contradiction:
Improvecharging compatibilityVSAvoidsystem complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The motor controller is designed to perform multiple functions: it controls the AC motor for propulsion and simultaneously serves as a charging controller for both DC and AC power sources. The bidirectional converter also operates in multiple modes (inverter mode for motor drive, rectifier mode for charging). This multi-functionality eliminates the need for separate dedicated charging equipment, reducing system complexity while maintaining charging compatibility across different power sources.

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

2Reliability

If separate dedicated converters are used for DC and AC charging, then proper power conversion is achieved, but the need for additional equipment increases

Engineering Contradiction:
Improvepower conversion reliabilityVSAvoidequipment quantity
Core Design Contradiction:
ReliabilityVSQuantity of substance

Solution Approach 1:

The patent merges the motor controller and bidirectional converter into an integrated system that handles both motor control and battery charging functions. The same power electronic components used for motor drive are utilized for power conversion during charging operations. This consolidation reduces the total equipment quantity while maintaining reliable power conversion through the proven motor control system.

Inventive Principle:
Principle #5Merging (Combining)

3Quantity of substance

If the motor controller is used for both motor control and charging control, then equipment quantity is reduced, but control precision requirements increase

Engineering Contradiction:
Improveequipment quantityVSAvoidcontrol precision
Core Design Contradiction:
Quantity of substanceVSMeasurement precision

Solution Approach 1:

The control system dynamically switches between different operational modes (motor drive mode, DC charging mode, AC charging mode) based on system requirements. The bidirectional converter dynamically adjusts its operation between inverter mode and rectifier mode. This dynamic adaptability allows the same hardware to achieve precise control in different contexts by optimizing control parameters for each specific mode, maintaining control precision while reducing equipment quantity.

Inventive Principle:
Principle #15Dynamics

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 flexible charging from various voltage levels and power sources, optimizing battery charging efficiency and safety by integrating the motor drive system, reducing the need for separate charging equipment.

Implementation Method 1

a bidirectional converter, wherein the bidirectional converter is capable of an inverter mode and a rectifier mode

Methodology Applied
Scientific EffectElectromagnetic conversion: Electromagnetic Induction

Data Source

PatentUS20250273980A1Machine and process for driving an electric motor
Publication Date: 2025.08.28 THE BOEING CO
  • US20250273980A1 patent drawing
  • US20250273980A1 patent drawing
  • US20250273980A1 patent drawing

AI summary

An aircraft adaptive battery charging system is provided. The adaptive battery charging system comprises: a battery system; a bidirectional converter, wherein the bidirectional converter is capable of an inverter mode and a rectifier mode; an alternating current (AC) motor; a number of controllable contactors that control electrical current between the battery system, bidirectional converter, AC motor, and a power source wherein the controllable contactors can be switched between a closed position to allow electrical current flow and an open position to prevent electrical current flow; a motor controller; a battery charging system controller configured to send control signals to the battery system, motor controller, and controllable contactors in response to system command signals; and a vehicle system controller that sends system command signals to the motor controller and battery charging system controller.