Turbine Engine Electric Machine Integration via Rotating Coupler

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Solution Overview

Problem

There is a need for structures and architectures that facilitate the arrangement of an electric machine within the core of a gas turbine engine to reduce the overall size of the engine, as existing solutions do not effectively integrate the electric machine within the engine core.

Innovation Solution

The turbine engine assembly includes a rotating structure, a turbine engine apparatus with an electric machine and a gearbox, a rotating coupler, and a seal assembly, which allows for the integration of the electric machine within the engine core by using a rotating coupler to connect the electric machine rotor and stator, and a seal assembly to seal the annular gap between the rotating and stationary structures, enabling lubricant circuits to provide lubrication to various components.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Volume of moving object

If the electric machine is arranged within the engine core, then the overall size of the gas turbine engine is reduced, but the structural complexity increases due to the need for rotating couplers and seal assemblies

Engineering Contradiction:
Improveoverall engine sizeVSAvoidstructural complexity
Core Design Contradiction:
Volume of moving objectVSDevice complexity

Solution Approach 1:

The electric machine is nested within the engine core, with the rotor positioned inside the engine core and the stator arranged around it. The rotating coupler connects these components while passing through the seal assembly, creating a compact integrated structure that reduces overall engine volume.

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The rotating coupler acts as an intermediary component that connects the electric machine rotor and stator while allowing relative rotation. The seal assembly serves as another intermediary that maintains sealing between rotating and stationary parts, enabling the compact integration without compromising functional requirements.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Adaptability or versatility

If a rotating coupler is used to connect the electric machine rotor and stator, then the electric machine can be integrated within the engine core, but the difficulty of detecting and measuring increases due to the complex rotating connections

Engineering Contradiction:
Improveintegration capabilityVSAvoiddetection and measurement difficulty
Core Design Contradiction:
Adaptability or versatilityVSDifficulty of detecting and measuring

Solution Approach 1:

The rotating coupler and seal assembly serve as intermediary components that enable the integration of the electric machine within the engine core. These intermediaries facilitate the connection between rotating and stationary parts while maintaining the necessary functional requirements for detection and measurement.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If the seal assembly is used to seal the annular gap between rotating and stationary structures, then the integration is effective, but the device complexity increases

Engineering Contradiction:
Improvesealing effectivenessVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The seal assembly acts as an intermediary component that seals the annular gap between rotating and stationary structures. This sealing element is integrated into the rotating coupler assembly, providing reliable sealing while maintaining the compact design and functional requirements of the system.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS11994038B2Turbine engine module with electric machine
Publication Date: 2024.05.28 RTX CORP
  • US11994038B2 patent drawing
  • US11994038B2 patent drawing
  • US11994038B2 patent drawing

AI summary

An assembly is provided for a turbine engine. This turbine engine assembly includes a first rotating structure, a turbine engine apparatus, a rotating coupler and a seal assembly. The first rotating structure is configured to rotate about a rotational axis. The turbine engine apparatus includes an electric machine and a second rotating structure. The electric machine includes an electric machine rotor and an electric machine stator. The second rotating structure is configured to rotate about the rotational axis and is coupled to the electric machine rotor. The rotating coupler is coupled to the first rotating structure by a first connection. The rotating coupler is coupled to the second rotating structure by a second connection. The seal assembly includes a rotating seal land and a stationary seal element. The rotating seal land is mounted onto the rotating coupler. The stationary seal element sealingly engages the rotating seal land.