Hybrid Electric Multi-Shaft Core With Variable Gear Ratio Speed Control

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Solution Overview

Problem

Traditional gas turbine engines face inefficiencies in operational stages requiring different power sources, such as electrical versus fuel, and lack flexibility in rapidly adjusting compressor speed to enhance performance and prevent stalls.

Innovation Solution

A hybrid electric engine with a variable gear ratio gearbox and an electric motor connected to the gearbox, allowing selective acceleration or deceleration of the compressor relative to the turbine, enhancing speed control and efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If a traditional gas turbine engine uses fuel combustion to drive the turbine and compressor, then the engine can operate continuously, but the ability to rapidly adjust compressor speed is limited and fuel efficiency varies during different operational stages

Engineering Contradiction:
Improvecompressor speed adjustabilityVSAvoidfuel efficiency
Core Design Contradiction:
SpeedVSUse of energy by moving object

Solution Approach 1:

The patent combines a fuel-based turbine-compressor system with an electric motor-compressor system into a hybrid configuration. The electric motor is coupled to the compressor via a gearbox, allowing it to directly drive the compressor independently of the turbine. This merging of two different power sources (fuel combustion and electrical power) enables the system to select the most efficient power source for each operational stage, thereby improving overall fuel efficiency while maintaining rapid speed adjustability through the electric motor.

Inventive Principle:
Principle #5Merging (Combining)

2Power

If the compressor speed is increased rapidly to increase engine airflow and power, then engine power output improves, but the risk of engine surge increases

Engineering Contradiction:
Improveengine power outputVSAvoidengine surge risk
Core Design Contradiction:
PowerVSReliability

Solution Approach 1:

The control system continuously monitors engine operating parameters including compressor speed, turbine speed, and airflow conditions. Based on this feedback, the controller dynamically adjusts the electric motor speed and torque output, as well as fuel flow to the combustor, to maintain optimal operating conditions. This feedback control prevents the compressor from entering surge conditions by detecting approaching surge margins and reducing power input accordingly, while still enabling rapid power increases when operating within safe margins.

Inventive Principle:
Principle #23Feedback

3Adaptability or versatility

If an electric motor is added to drive the compressor independently, then rapid speed adjustment capability improves, but the device complexity increases

Engineering Contradiction:
Improveoperational flexibilityVSAvoidengine system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The electric motor-gearbox assembly is designed to serve multiple functions: it can drive the compressor during electrical power mode, assist the turbine during hybrid mode, and potentially generate electrical power during turbine-driven mode if configured as a generator. The gearbox is designed with variable ratio capability to optimize compressor speed across different operating conditions. This multi-functionality justifies the added complexity by providing operational flexibility and potential fuel efficiency improvements.

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

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 thrust or power increase during engine stalls, improves fuel efficiency, and reduces the risk of engine surges by dynamically controlling compressor speed, thus optimizing engine performance and reducing noise.

Implementation Method 1

a combustor configured to drive the turbine via a flow of combustion products

Methodology Applied
Scientific EffectCombustion: Combustion

Implementation Method 2

An electric motor is operably connected to the variable gear ratio rear box and configured to input rotational energy into the gearbox

Methodology Applied
Scientific EffectElectromagnetic conversion: Electromagnetic Induction

Implementation Method 3

a variable gear ratio gearbox... The input of rotational energy into the gearbox from the electric motor changes a rotational speed of one of the compressor or the turbine

Methodology Applied
Scientific EffectGear mechanism: Gear

Data Source

PatentUS12480450B2Hybrid electric multiple shaft core
Publication Date: 2025.11.25 RTX CORP
  • US12480450B2 patent drawing
  • US12480450B2 patent drawing
  • US12480450B2 patent drawing

AI summary

A hybrid electric engine of an aircraft includes a compressor, a turbine operably connected to the compressor via a variable gear ratio gearbox and a combustor configured to drive the turbine via a flow of combustion products. An electric motor is operably connected to the variable gear ratio rear box and configured to input rotational energy into the gearbox. The input of rotational energy into the gearbox from the electric motor changes a rotational speed of one of the compressor or the turbine relative to the other of the compressor or the turbine.