Gas Turbine Distributed Control With Remote Computation Modules

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Solution Overview

Problem

Current gas turbine engine control systems face challenges with high data throughput, harsh environmental conditions, rapid processor obsolescence, and cybersecurity requirements, necessitating a distributed control system architecture that can handle these demands effectively.

Innovation Solution

A distributed control system architecture for gas turbine engines, featuring a computation module and an I/O module with distinct processing units, where the computation module is located in a benign environment and the I/O module in a harsh environment, utilizing a high-bandwidth network for communication and employing software abstraction to manage functionality allocation and cybersecurity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If control systems use multiple I/O data connections to handle high data throughput rates, then data throughput capability is improved, but physical location constraints and system complexity increase due to harness length limitations

Engineering Contradiction:
Improvedata throughput rateVSAvoidsystem complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent replaces physical I/O data connections (mechanical/electrical harnesses) with wireless communication technology. This substitution eliminates the need for physical connection constraints while maintaining high data throughput capability, allowing control systems to handle future data rates without being limited by harness length or physical proximity requirements

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

Solution Approach 2:

The control system is divided into multiple independent functional modules (engine control module, airframe module, remote interface units) that can be physically separated and located optimally. Each module operates semi-independently, reducing the need for extensive physical interconnections and allowing distributed placement without increasing overall system complexity

Inventive Principle:
Principle #1Segmentation

2Reliability

If control systems are designed in a bespoke manner with customized components, then specific performance requirements are met, but manufacturing cost and development time increase

Engineering Contradiction:
Improveperformance optimizationVSAvoidmanufacturing cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent employs universal, off-the-shelf components and standardized communication protocols that can be used across multiple control system applications. The modular architecture allows the same basic modules to be configured for different engine types and applications, reducing development costs and manufacturing complexity while maintaining optimized performance through software configuration rather than hardware customization

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

Solution Approach 2:

The system uses configurable software and programmable modules that can be dynamically adjusted to meet specific performance requirements without requiring custom hardware design. This allows the same physical platform to be adapted to different applications, reducing manufacturing costs while maintaining performance optimization

Inventive Principle:
Principle #15Dynamics

3Adaptability or versatility

If control systems use commercially available processors, then cost is reduced and adaptability is improved, but processor obsolescence and cybersecurity vulnerabilities increase

Engineering Contradiction:
Improvecost effectivenessVSAvoidcybersecurity and obsolescence
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The control system separates critical safety functions from general control functions, placing them in different modules with different security requirements. This segmentation allows commercially available processors to be used in less critical areas while maintaining security and reliability in critical functions through architectural isolation and dedicated hardware where necessary

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent introduces secure communication interfaces and authentication protocols as intermediaries between commercial processors and the control system. These intermediaries provide cybersecurity protection, allowing the use of commercially available processors while mitigating security vulnerabilities through layered defense mechanisms

Inventive Principle:
Principle #24Intermediary (Mediator)

4Device complexity

If control systems are located close to engine components, then connection length is minimized, but exposure to harsh environmental conditions increases

Engineering Contradiction:
Improveconnection lengthVSAvoidenvironmental exposure
Core Design Contradiction:
Device complexityVSObject-affected harmful factors

Solution Approach 1:

By replacing physical I/O connections with wireless communication, the system eliminates the trade-off between connection length and environmental exposure. Modules can be located remotely in environmentally benign areas while maintaining full communication capability, as wireless signals are not constrained by physical connection length limitations

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

Solution Approach 2:

Wireless communication signals act as intermediaries, allowing data transmission between remotely located control modules and engine components without requiring physical proximity. This enables modules to be positioned in protected environments while still functioning with components in harsh environments

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentEP3608733B1Distributed control and monitoring system for gas turbine engine
Publication Date: 2022.09.21 ROLLS ROYCE CORP
  • EP3608733B1 patent drawingFigure 1
  • EP3608733B1 patent drawingFigure 2A
  • EP3608733B1 patent drawingFigure 2B

AI summary

Control systems and methods for controlling an engine. The control system (202, 300) includes a computation module (204, 306) and an input/output (I/O) module attached to the engine. The computation module is located in an area of the engine, or off-engine, which provides a more benign environment than the environment that the I/O module is subject to during operation of the engine. The I/O module includes a first processor (210, 324) and a first network interface device (330). The computation module includes a second processor (208, 320) with higher processing power than the first processor, and a second network interface device (322). The control system also includes a sensor (318) configured to provide sensor readings to the first processor. The first processor transmits data based on the sensor readings to the second processor. The control system also includes an actuator (316) operably coupled to the I/O module and that is controlled by the first processor based on commands from the second processor.