Aircraft Power Converter Control for Efficiency

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Solution Overview

Problem

Existing power management systems in electric aircraft do not effectively maximize the efficiency of power converters, as they often operate outside their optimal efficiency window due to inadequate management of on-board batteries.

Innovation Solution

A system comprising a battery pack with a battery monitoring component, a battery management component, and electric power converters, where an interlock component enables or disables these components based on battery data to maintain optimal operating conditions, adjusting the number of enabled power converters to ensure efficient operation within a specific voltage threshold.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If the number of enabled power converters is increased to handle higher power demands, then the power output capacity is improved, but the overall system efficiency deteriorates because converters operate outside their optimal efficiency window

Engineering Contradiction:
Improvepower output capacityVSAvoidconverter efficiency
Core Design Contradiction:
PowerVSLoss of energy

Solution Approach 1:

The system dynamically adjusts the number of enabled power converters based on real-time battery pack voltage conditions. When voltage sags occur, the controller enables additional converters to share the load and maintain efficiency. When voltage is sufficient, fewer converters are enabled to reduce complexity and potential failure points. This dynamic configuration allows the system to adapt between power capacity needs and efficiency optimization.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the operational parameters of power converters by adjusting their enable/disable states based on battery voltage thresholds. The controller monitors battery pack voltage and compares it against predetermined thresholds, then modifies the number of active converters accordingly. This parameter change strategy ensures converters operate within their optimal efficiency window while meeting power demands.

Inventive Principle:
Principle #35Parameter changes

2Loss of energy

If battery voltage sags are allowed to persist to maintain converter efficiency, then energy loss is reduced, but voltage stability deteriorates affecting component operation

Engineering Contradiction:
Improveconverter efficiencyVSAvoidvoltage stability
Core Design Contradiction:
Loss of energyVSStability of the object's composition

Solution Approach 1:

The system implements a feedback control mechanism where the controller continuously monitors battery pack voltage and adjusts the number of enabled power converters based on voltage threshold comparisons. When voltage sags below the threshold, the controller enables additional converters to share the load, which stabilizes the voltage by reducing the burden on individual converters. This closed-loop feedback ensures voltage stability is maintained while minimizing energy loss.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system takes preliminary action by enabling additional power converters before voltage instability severely impacts component operation. The controller is configured with predetermined voltage thresholds that trigger converter enablement in advance, preventing voltage sag from reaching critical levels. This proactive approach maintains both voltage stability and converter efficiency.

Inventive Principle:
Principle #10Preliminary action

3Stability of the object's composition

If the number of enabled power converters is increased to stabilize voltage, then voltage stability is improved, but device complexity increases

Engineering Contradiction:
Improvevoltage stabilityVSAvoidconverter configuration complexity
Core Design Contradiction:
Stability of the object's compositionVSDevice complexity

Solution Approach 1:

The system uses dynamic configuration where the number of enabled power converters is adjusted in real-time based on battery voltage conditions. Rather than maintaining a fixed complex configuration, the system activates only the necessary number of converters at any given moment. This dynamic approach simplifies the operational complexity by having a clear enable/disable logic based on voltage thresholds, while still providing voltage stability when needed.

Inventive Principle:
Principle #15Dynamics

4Power

If power converters are operated at high load to maximize power output, then power delivery is improved, but converter efficiency deteriorates

Engineering Contradiction:
Improvepower delivery capacityVSAvoidconverter efficiency
Core Design Contradiction:
PowerVSLoss of energy

Solution Approach 1:

The system segments the power delivery function across multiple power converters rather than relying on a single converter operating at high load. When power demand increases or battery voltage sags, the controller enables additional converters to share the total power delivery requirement. This segmentation allows each individual converter to operate at moderate, efficient load levels while collectively meeting high power demands, thus maintaining both power delivery capacity and converter efficiency.

Inventive Principle:
Principle #1Segmentation

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 system ensures that electric power converters operate within their peak efficiency window, enhancing overall power management and distribution efficiency in electric aircraft.

Implementation Method 1

each electric power converter converts an input at a first voltage level to an output at a second voltage level

Methodology Applied
Scientific EffectElectrical energy conversion: Electromagnetic Induction

Data Source

PatentUS20230145830A1Systems and methods for aircraft power management and distribution
Publication Date: 2023.05.11 BETA AIR LLC
  • US20230145830A1 patent drawing
  • US20230145830A1 patent drawing
  • US20230145830A1 patent drawing

AI summary

A system for aircraft power management and distribution, including a sensor suite configured to measure battery pack data. The system includes a battery pack with a plurality of batteries and a battery monitoring component. This battery monitoring component is configured to measure battery pack data. The system also has electric power converters, each connected to a battery of the plurality of batteries. The system also includes a controller configured to control each electric power converter; receive an estimated charge from each battery; select and enable electric power converters based on the estimated charge; compare the total output of the enabled electric power converters against an optimal operating region; and adjust the number of the one or more enabled electric power converters accordingly.