Sprag-Clutch Variable Drive for Hybrid Turbine Power Split

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Solution Overview

Problem

Hybrid-electric gas turbine engines face increased complexity, mass, and expense due to the inclusion of generators, motors, and drive elements, which hinder efficient power redistribution and fault tolerance in aerospace applications.

Innovation Solution

The implementation of variable drive arrangements using sprag clutches to couple motors and generators to the engine's low spool, providing efficient load paths for hybrid power distribution with reduced mass and complexity, including epicyclic gear systems for enhanced compactness and passive operability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If generators, motors, and drive elements are added to redistribute power in hybrid-electric architectures, then operating efficiencies are improved and component lifetimes are extended, but engine complexity, mass, and expense increase

Engineering Contradiction:
Improveoperating efficiencyVSAvoidengine complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The sprag clutch mechanism serves multiple functions simultaneously: it acts as a one-way coupling device, a passive disconnect mechanism, and a load path selector. This single component performs what would traditionally require multiple separate systems, thereby improving operating efficiency while limiting the increase in engine complexity.

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

Solution Approach 2:

The sprag clutch operates passively without requiring external control systems, actuators, or power sources. It automatically engages and disengages based on the direction of torque flow, eliminating the need for complex control mechanisms and reducing overall system complexity while maintaining the ability to redistribute power for improved efficiency.

Inventive Principle:
Principle #25Self-service

2Duration of action of stationary object

If generators, motors, and drive elements are added to redistribute power, then operating efficiencies are improved and component lifetimes are extended, but mass and expense increase

Engineering Contradiction:
Improvecomponent lifetimeVSAvoidengine mass
Core Design Contradiction:
Duration of action of stationary objectVSWeight of moving object

Solution Approach 1:

The sprag clutch enables a single drive element to serve multiple functions: power redistribution for load balancing (extending component lifetime) and passive disconnect for fault protection. This multi-functionality allows lifetime extension without proportionally increasing mass, as the same hardware provides multiple benefits.

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

Solution Approach 2:

The passive operation of the sprag clutch eliminates the need for additional actuators, sensors, and control systems that would increase mass. The component automatically performs load balancing and fault protection functions without adding significant weight, thereby extending component lifetime with minimal mass penalty.

Inventive Principle:
Principle #25Self-service

3Adaptability or versatility

If traditional drive arrangements are used for hybrid power distribution, then power redistribution is achieved, but device complexity and mass increase significantly

Engineering Contradiction:
Improvepower redistribution capabilityVSAvoiddrivetrain complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The sprag clutch provides a universal coupling mechanism that handles multiple drive configurations (series, parallel, hybrid) without requiring different hardware for each mode. This single component enables adaptable power redistribution across various operating modes while maintaining simple drivetrain architecture.

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

Solution Approach 2:

The passive, self-actuating nature of the sprag clutch allows the drivetrain to automatically adapt to different power distribution requirements without complex control systems. The component responds autonomously to torque direction changes, enabling versatile power redistribution while keeping drivetrain complexity low.

Inventive Principle:
Principle #25Self-service

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 hybrid power distribution with reduced mass and complexity, improving engine efficiency, extending component lifetimes, and providing fallback power without adding significant weight or cost, while maintaining compactness and simplicity in the drivetrain.

Implementation Method 1

variable drive arrangements using sprag clutches to couple motors and generators to the engine's low spool

Methodology Applied
Scientific EffectMechanical advantage through one-way coupling: Ratchet

Data Source

PatentEP3722577B1Variable multiple-drive gas turbine engine
Publication Date: 2024.04.03 RTX CORP
  • EP3722577B1 patent drawingFigure 1
  • EP3722577B1 patent drawingFigure 2
  • EP3722577B1 patent drawingFigure 3

AI summary

A gas turbine engine (10; 310; 510) includes an engine spool (24) with a turbine section (22), a propeller (12), a motor (34), and a variable drive arrangement (28; 328; 528). The variable drive arrangement (28; 328; 528) mechanically couples the engine spool (24) to the propeller (12), and includes a first gear connection (38; 338; 538) rotationally coupled to the propeller (12), a second gear connection (42; 342; 542) rotationally coupled to the engine spool (24), and a sprag clutch rotationally coupled to the first gear connection (38; 338; 538). The sprag clutch is configured to passively decouple the motor (34) from the first gear connection (38; 338; 538) when a torque input from the engine spool (24) exceeds a torque input from the motor (34), and is configured to passively couple the motor (34) to the first gear connection (38; 338; 538) when the torque input from motor (34) exceeds a torque input from the engine spool (24).