Low-Pressure Compressor Speed Control via Epicyclic Gear Coupling

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Solution Overview

Problem

Conventional two-spool gas turbine engines face inefficiencies due to competing operating speed demands of the two spools, leading to suboptimal operation and reduced thrust and efficiency.

Innovation Solution

The implementation of an epicyclic gear system mechanically coupled to the high speed spool, allowing the low pressure compressor to be independently controlled and mechanically decoupled from the low speed spool, with the assistance of motor-generators for improved power transfer and control.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If the low pressure compressor is mechanically coupled to the low speed spool in a conventional two-spool gas turbine engine, then the engine structure is simpler, but the low pressure compressor cannot operate at optimal speed during transient power demands, leading to reduced efficiency and thrust

Engineering Contradiction:
Improveengine efficiencyVSAvoidengine structure
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent segments the traditional coupled spool-compressor system by mechanically decoupling the low pressure compressor from the low speed spool. The low pressure compressor is now independently driven through the epicyclic gear system, allowing separate control of compressor speed from spool speed. This segmentation enables the compressor to operate at optimal conditions independent of transient spool speed changes.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The epicyclic gear system acts as an intermediary mechanism between the high speed spool and the low pressure compressor. This gear system provides the necessary mechanical interface to transmit power while allowing speed transformation and independent control. The intermediary enables the compressor to receive power from the high speed spool through controlled mechanical coupling, resolving the contradiction between structural simplicity and operational independence.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Adaptability or versatility

If the low pressure compressor is independently controlled via epicyclic gear system, then the operating speed optimization is achieved, but the device complexity increases

Engineering Contradiction:
Improvespeed control flexibilityVSAvoidgear system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The epicyclic gear system is designed to perform multiple functions: power transmission from the high speed spool, speed transformation to match compressor requirements, and providing a mechanical interface for independent compressor control. This multi-functionality reduces the need for additional separate systems, thereby limiting the increase in overall device complexity while achieving speed control flexibility.

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

Solution Approach 2:

The gear system incorporates dynamic elements that allow the low pressure compressor to adapt its operating speed independently of the spool speed. The mechanical coupling through the epicyclic gears enables continuous adjustment of the compressor speed ratio, providing dynamic adaptability across different operating conditions without requiring complex electronic control systems.

Inventive Principle:
Principle #15Dynamics

3Power

If motor-generators are added to the epicyclic gear system, then power transfer and control are improved, but the device complexity and weight increase

Engineering Contradiction:
Improvepower transfer capabilityVSAvoidengine weight
Core Design Contradiction:
PowerVSWeight of moving object

Solution Approach 1:

The patent merges the motor-generator functions directly into the epicyclic gear system architecture. By integrating the motor-generators with the existing gear components, the design eliminates the need for separate mounting structures and support systems. This merging approach provides improved power transfer capability while minimizing the additional weight that would result from completely separate motor-generator assemblies.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The motor-generators replace traditional mechanical power transmission components with electromagnetic systems. This substitution provides superior power transfer capability and control precision compared to purely mechanical systems. The electromagnetic actuation through motor-generators enables more efficient power transmission with reduced mechanical losses, offsetting the weight penalty through improved overall system efficiency.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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 configuration enables independent control of the low pressure compressor and high speed spool operating speeds, optimizing stability and efficiency by allowing different speed 'matches' between the spools, thereby enhancing overall engine performance.

Implementation Method 1

a first motor-generator may be mechanically coupled to the sun gear, a second motor-generator may be mechanically coupled to the gear carrier, and a third motor-generator may be mechanically coupled to the high speed spool

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Implementation Method 2

an epicyclic gear system mechanically coupled to the high speed spool... wherein the plurality of planet gears are disposed between the sun gear and the ring gear

Methodology Applied
Scientific EffectMechanical advantage through gear transmission: Gear

Data Source

PatentUS12331689B2Low pressure compressor control for a gas turbine engine
Publication Date: 2025.06.17 RTX CORP
  • US12331689B2 patent drawing
  • US12331689B2 patent drawing
  • US12331689B2 patent drawing

AI summary

A gas turbine engine includes a low speed spool mechanically interconnecting a low pressure turbine and at least one of a fan and a prop, a high speed spool mechanically interconnecting a high pressure turbine and a high pressure compressor, and an epicyclic gear system mechanically coupled to the high speed spool. The gas turbine engine also includes a low pressure compressor mechanically coupled to the high speed spool via the epicyclic gear system. The low pressure compressor may be mechanically independent of the low speed spool. The gas turbine engine may include a plurality of motor-generators for transferring power between the high speed spool and the low pressure compressor.