Differential Gearbox for Boost Spool Power Distribution

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Solution Overview

Problem

Turbine engines face inefficiencies in power generation during low and partial power conditions, as existing systems lack effective mechanisms to optimize power distribution and augmentation between the core engine and accessory systems.

Innovation Solution

A differential gear system is introduced, coupling a first differential gear to the core engine and a second differential gear to the accessory gearbox, with a boost spool providing additional power through a secondary turbine engine or electric motor-generator, allowing for tailored gear ratios and operational configurations to enhance power transmission and engine efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If a traditional direct-drive connection is used between the core engine and accessory gearbox, then the structure is simple, but the engine cannot efficiently augment power during low and partial power conditions

Engineering Contradiction:
Improvepower augmentation capabilityVSAvoidgearbox system complexity
Core Design Contradiction:
PowerVSDevice complexity

Solution Approach 1:

The power transmission system is segmented into multiple independent pathways: a primary drive path from the core engine through the tower shaft, and a secondary boost path from the boost spool through the differential gear system. This segmentation allows each pathway to operate independently and contribute power according to engine conditions, enabling power augmentation while maintaining structural organization.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The differential gearbox is designed to perform multiple functions: it can operate in direct-drive mode during high power conditions, engage the boost spool during low and partial power conditions, and provide variable gear ratios to optimize power transmission. This multi-functionality resolves the contradiction by enabling power augmentation without requiring entirely separate systems for each operating mode.

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

2Adaptability or versatility

If fixed gear ratios are used in the gearbox, then the manufacturing is simpler, but the system cannot optimize power distribution under varying engine operating conditions

Engineering Contradiction:
Improveadaptability to operating conditionsVSAvoidgearbox manufacturing complexity
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

The gearbox incorporates a differential mechanism that dynamically adjusts power distribution between the core engine and boost spool based on operating conditions. The differential carrier and planet gears automatically vary the effective gear ratio according to the relative speeds and torques of the input shafts, providing adaptability without requiring complex controllable variable ratio mechanisms.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes operational parameters by engaging different clutch configurations and differential states depending on engine operating conditions. During ground operations or low power modes, the boost clutch engages to activate the differential gear system with specific ratios; during flight or high power modes, the configuration changes. This parameter switching provides adaptability while maintaining manufacturing simplicity through discrete, well-defined states.

Inventive Principle:
Principle #35Parameter changes

3Power

If the boost spool is always engaged, then power augmentation is maximized, but energy loss increases during high power conditions when augmentation is not needed

Engineering Contradiction:
Improvepower outputVSAvoidenergy loss
Core Design Contradiction:
PowerVSLoss of energy

Solution Approach 1:

The boost spool engagement is implemented as a periodic or conditional action rather than continuous operation. The boost clutch selectively engages the boost spool to the differential gearbox only during specific operating conditions such as ground operations, takeoff, or low power flight modes. During high power conditions or cruise flight, the clutch disengages the boost spool, eliminating energy losses while maintaining the capability for power augmentation when needed.

Inventive Principle:
Principle #19Periodic action

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

The differential gear system enables efficient power augmentation during low power conditions, improving overall engine efficiency by allowing different gear ratios and operational modes, thereby optimizing power distribution between the core engine and accessory systems.

Implementation Method 1

A differential gear system is introduced, coupling a first differential gear to the core engine and a second differential gear to the accessory gearbox, with a boost spool providing additional power

Methodology Applied
Scientific EffectGear mechanism: Gear

Data Source

PatentEP3987166B1Gearbox for boost spool turbine engine
Publication Date: 2025.03.26 RTX CORP
  • EP3987166B1 patent drawingFigure 1~2
  • EP3987166B1 patent drawingFigure 3
  • EP3987166B1 patent drawingFigure 4

AI summary

A turbine engine includes a core engine including a first spool and a second spool rotatable about a main engine longitudinal axis, a boost spool powered by a secondary drive system, and an accessory gearbox coupled to the core engine and the boost spool. A differential gear system is coupled between the core engine, the boost spool and the accessory gearbox for distributing power between the boost spool, the core engine and the accessory gearbox.