Turbojet Thrust Reverser Control via Segmented Computing

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current control and monitoring systems for turbojet engines with thrust reversers are complex due to the need for compatibility between the electronic control unit and the turbojet regulation system, complicating construction and maintenance.

Innovation Solution

A control and monitoring system comprising sensors for the thrust reverser status, a control unit controlled by computing means, and a turbojet regulating device, where the computing means directly controls both units independently, eliminating the need for compatibility between them.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the electronic control unit and turbojet regulation system are made compatible, then the control system can function properly, but the system complexity increases and maintenance becomes more difficult

Engineering Contradiction:
Improvecontrol system functionalityVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent segments the control architecture by introducing a central computing means that independently controls both the control unit and regulating device. This segmentation allows each component to operate autonomously without requiring compatibility between previously interconnected systems, thereby reducing overall system complexity while maintaining functionality.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The computing means acts as an intermediary that receives information from sensors and independently processes control signals to both the control unit and regulating device. This intermediary role eliminates the need for direct compatibility between the control unit and regulating device, as all communication flows through the centralized computing means.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If the electronic control unit and turbojet regulation system are made compatible, then the control system can function properly, but maintenance complexity increases

Engineering Contradiction:
Improvecontrol system functionalityVSAvoidmaintenance complexity
Core Design Contradiction:
ReliabilityVSEase of repair

Solution Approach 1:

By segmenting the control system into independent components (sensors, computing means, control unit, regulating device), the patent enables isolated maintenance and repair of individual components without affecting the entire system. This segmentation simplifies maintenance procedures compared to previously interconnected compatible systems.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent extracts the compatibility requirement from the system architecture by introducing a centralized computing means that handles all processing. This extraction allows the control unit and regulating device to be maintained independently without needing to maintain compatibility relationships, thereby easing maintenance complexity.

Inventive Principle:
Principle #2Taking out (Extraction)

3Device complexity

If a centralized computing means controls both control unit and regulating device independently, then system simplicity increases, but control precision may be affected

Engineering Contradiction:
Improvesystem simplicityVSAvoidcontrol precision
Core Design Contradiction:
Device complexityVSManufacturing precision

Solution Approach 1:

The patent implements feedback mechanisms where sensors continuously monitor system status and provide information to the computing means. This feedback loop enables the centralized computing means to maintain precise control by continuously adjusting control signals based on actual system state, thereby preserving control precision despite the simplified architecture.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The computing means is designed as a universal control platform that can perform multiple functions including sensor data processing, control signal generation, and system monitoring. This multi-functionality allows a single centralized unit to maintain the precision previously requiring multiple specialized components, thereby simplifying the system without sacrificing control accuracy.

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

Data Source

PatentUS8892295B2Control and monitoring system and method
Publication Date: 2014.11.18 AIRBUS OPERATIONS (SAS)
  • US8892295B2 patent drawing
  • US8892295B2 patent drawing
  • US8892295B2 patent drawing

AI summary

A monitoring system and a monitoring method applied to the monitoring system, in which the monitoring system includes detectors detecting a state of a turbojet thrust reverser, a monitoring computer device controlling the reverser monitored by the computer as a function of information from the detectors provided to the computer by way of the control device, and a device regulating the turbojet monitored by the computer as a function of the information from the detectors provided to the computer by way of the control device.