Turbomachine Cowling Screen for Engine Maintenance Data

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Solution Overview

Problem

Current monitoring systems for turbojet engines lack precision and safety, requiring improvements in speed, reliability, and information flow management during maintenance and data acquisition.

Innovation Solution

A turbojet engine design featuring a display screen integrated into the outer cowl, equipped with sensors and a communication system that allows for real-time data processing and visualization of engine parameters, enabling independent data acquisition and maintenance assistance, even when the engine is stopped or disconnected from the FADEC system.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a display screen is integrated into the outer cowl to enable real-time data visualization, then maintenance safety and information accessibility are improved, but device complexity and manufacturing cost increase

Engineering Contradiction:
Improvemaintenance safetyVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The display screen integrated into the outer cowl enables the engine to provide its own maintenance information directly at the location where maintenance personnel operate, eliminating the need for separate data transmission systems or remote monitoring setups. The screen self-services by displaying component information, sensor data, and maintenance alerts locally on the engine assembly.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The monitoring system is segmented into independent functional modules: the display screen integrated into the outer cowl, sensor units distributed on engine components, and a control unit that processes data. This segmentation allows each module to be independently manufactured, tested, and replaced, reducing overall system complexity despite the added functionality.

Inventive Principle:
Principle #1Segmentation

2Measurement precision

If sensors and communication systems are added to the outer cowl for independent data acquisition, then monitoring precision and reliability are improved, but weight and manufacturing cost increase

Engineering Contradiction:
Improvedata acquisition precisionVSAvoidengine weight
Core Design Contradiction:
Measurement precisionVSWeight of moving object

Solution Approach 1:

The outer cowl is designed with multi-functionality: it serves as the aerodynamic fairing for the engine while simultaneously housing the display screen, sensor mounting structures, and communication antennas. This universal design allows the same structural component to fulfill multiple functions, adding monitoring capabilities without requiring separate dedicated structures that would increase weight.

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

Solution Approach 2:

The display screen and sensor integration structures utilize thin-film technologies and flexible mounting solutions that minimize additional weight. The screen itself is a thin integrated display element, and sensors are mounted using lightweight adhesive or夹持 structures rather than heavy mechanical mountings.

Inventive Principle:
Principle #30Flexible shells and thin films

3Ease of operation

If the display screen is made visible from outside the turbojet engine, then ease of operation during maintenance is improved, but aerodynamic drag and manufacturing complexity increase

Engineering Contradiction:
Improvemaintenance accessibilityVSAvoidaerodynamic drag
Core Design Contradiction:
Ease of operationVSObject-affected harmful factors

Solution Approach 1:

The display screen is positioned on the outer cowl at a location that is visually accessible to maintenance personnel during ground operations, while the screen surface itself is designed with aerodynamic contours that match the local cowl geometry. Only the necessary portion of the cowl is modified to accommodate the screen, maintaining smooth airflow over the majority of the engine assembly.

Inventive Principle:
Principle #3Local quality

Data Source

PatentEP3378790B1Turbomachine cowling with screen
Publication Date: 2020.06.17 SAFRAN AERO BOOSTERS SA
  • EP3378790B1 patent drawingFigure 1
  • EP3378790B1 patent drawingFigure 2
  • EP3378790B1 patent drawingFigure 3

AI summary

The invention relates to a turbojet engine comprising an outer cowling (26), a component such as an oil reservoir (28), and a monitoring system (34) for the component, enabling the determination of information about the component. The outer cowling (26) includes a display screen (32) capable of communicating with the monitoring system (34) or directly with the component in order to display information specific to the component. Installed in the nacelle (24) of the turbojet engine, this cowling (26) becomes an intelligent cowling. The invention further provides a method for controlling a component of an aircraft turbojet engine and a corresponding computer program.