Hybrid Propulsion Cockpit Throttle for Multi-Mode Power Control

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Solution Overview

Problem

Hybrid propulsion systems face challenges in efficiently managing power distribution between electrical energy storage systems and generators, requiring advanced control mechanisms to optimize propulsion and energy usage in vehicles.

Innovation Solution

The implementation of a hybrid propulsion system with a pilot interface that includes throttle controls and a controller to manage power distribution between electrical energy storage systems and generators, allowing for various operational modes such as regeneration, electric-only, and dual-source operation, enabling efficient propulsion and energy management.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If power distribution between electrical energy storage systems and generators is managed using conventional control mechanisms, then system operation is maintained, but power management efficiency is insufficient

Engineering Contradiction:
Improvepower management efficiencyVSAvoidcontrol mechanism complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The control mechanism is segmented into multiple independent controllers, each managing specific functions: a power management controller that receives pilot inputs and generates control signals, a generator controller that manages generator output, and an energy storage controller that manages battery charge/discharge. This segmentation allows each controller to specialize in specific power management tasks, improving overall efficiency while maintaining manageable complexity through modular design.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The control system dynamically adjusts power distribution between the generator and energy storage system based on real-time operating conditions. The power management controller continuously monitors system state and modifies control signals to optimize the ratio of electrical to mechanical power, enabling adaptive power management that responds to changing flight conditions and power demands.

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If multiple operational modes are implemented for power distribution, then versatility of operation is improved, but control system complexity increases

Engineering Contradiction:
Improveoperational mode versatilityVSAvoidcontrol system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The power management controller is designed as a universal control device that handles multiple operational modes through a single integrated system. It can manage electric-only operation, hybrid operation with generator support, battery charging modes, and various power distribution ratios, all through one controller that adapts its control strategy based on the selected mode and current system state.

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

Solution Approach 2:

The system provides preliminary action by pre-configuring multiple operational modes and having the power management controller automatically select and transition between them based on system conditions. The controller is pre-programmed with control algorithms for different operating scenarios, allowing seamless mode transitions without requiring complex real-time decision-making logic.

Inventive Principle:
Principle #10Preliminary action

3Use of energy by moving object

If electrical power ratio is dynamically adjusted between generator and energy storage system, then power utilization efficiency is improved, but control precision requirements increase

Engineering Contradiction:
Improvepower utilization efficiencyVSAvoidpower ratio control precision
Core Design Contradiction:
Use of energy by moving objectVSMeasurement precision

Solution Approach 1:

The control system incorporates feedback mechanisms where the power management controller continuously monitors the actual power output from the generator and energy storage system, compares it with the desired power distribution, and adjusts control signals accordingly. This closed-loop feedback ensures precise control of the electrical to mechanical power ratio while maintaining efficient power utilization.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system dynamically changes operational parameters including the power distribution ratio, generator output level, and battery charge/discharge rate based on flight conditions and power demands. The power management controller adjusts these parameters in real-time to optimize power utilization efficiency while maintaining control precision through coordinated parameter modification across multiple system components.

Inventive Principle:
Principle #35Parameter changes

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 solution enables efficient power management, allowing vehicles to operate optimally in different modes, extending operational times and reducing fuel consumption by effectively utilizing both electrical and combustion energy sources.

Implementation Method 1

a first generator configured to convert the rotational mechanical energy into electrical energy for output onto the first electrical bus

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Implementation Method 2

electrical machines may be configured to drive a respective propulsor of one or more propulsors using electrical energy received from at least one of the one or more electrical busses

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Data Source

PatentUS11905026B2Hybrid propulsion system cockpit interface
Publication Date: 2024.02.20 ROLLS ROYCE DEUT LTD & CO KG
  • US11905026B2 patent drawing
  • US11905026B2 patent drawing
  • US11905026B2 patent drawing

AI summary

An example system includes a throttle control for managing power in a hybrid propulsion system that includes an electrical propulsion unit configured to operate using electrical energy sourced from an electrical energy storage system (ESS) and/or one or more electrical generators, the throttle control comprising: a control lever movable through a plurality of positions, the plurality of positions including: a regeneration position; an off position; a maximum electric only position; a maximum continuous dual source position; and a maximum non-continuous dual source position.