Aircraft Cockpit Configuration by Pilot and Mission Profiles

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Solution Overview

Problem

Airlines face challenges in managing heterogeneous aircraft equipment across different models and generations, requiring pilots to undergo extensive training or limiting the use of upgraded aircraft, which affects operational efficiency and flight mission flexibility.

Innovation Solution

A method and system for configuring cockpit functionalities based on pilot profiles and mission profiles, using an acquisition, determination, and activation module to adapt control and display elements according to specific training levels and flight requirements.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If equipment is upgraded in aircraft, then equipment functionality is improved, but pilot training requirements increase and operational flexibility decreases

Engineering Contradiction:
Improveequipment functionalityVSAvoidtraining requirements
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The cockpit system dynamically adapts its functionality based on the pilot's profile and the selected flight mission. The system can switch between different operational modes (e.g., simplified mode for less trained pilots, full functionality mode for highly trained pilots), allowing the same physical equipment to provide different levels of complexity as needed.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes operational parameters (available functionalities, display options, control modes) based on the pilot's training level and the mission requirements. This allows the equipment to maintain high functionality when needed while reducing complexity for pilots with lower training levels, without requiring physical hardware changes.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If all pilots are trained to the same high level, then operational safety is improved, but training time and cost increase

Engineering Contradiction:
Improveoperational safetyVSAvoidtraining time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

Instead of requiring all pilots to have uniform high-level training, the system provides localized quality enhancement by enabling advanced functionalities only when appropriate. Each pilot operates with the level of complexity they need for their specific role and training level, while the system adapts to provide safety-critical functions as needed.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The system acts as an intermediary between pilots of varying training levels and the complex aircraft equipment. It translates pilot inputs and system capabilities into appropriate operational modes, ensuring safety is maintained regardless of the pilot's training level while avoiding the need for extensive uniform training.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If cockpit functionalities are fixed, then system reliability is improved, but adaptability to different missions and pilots decreases

Engineering Contradiction:
Improvesystem reliabilityVSAvoidmission adaptability
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The cockpit system is designed with multi-functionality, where the same physical equipment can serve multiple purposes depending on the configured mode. The system can operate in different functional configurations (e.g., basic navigation mode, advanced mission mode) allowing it to adapt to various flight missions while maintaining reliable operation through standardized underlying systems.

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

Data Source

PatentUS12358641B2Method and system for configuring functionalities of an aircraft cockpit
Publication Date: 2025.07.15 AIRBUS OPERATIONS (SAS)
  • US12358641B2 patent drawing
  • US12358641B2 patent drawing
  • US12358641B2 patent drawing

AI summary

A method and system for configuring functionalities of an aircraft cockpit. The configuration system includes at least one processing unit to acquire profiles, to determine at least one combination of functionalities corresponding to the acquired profiles, based on a mapping table, and to activate at least the determined combination of functionalities. The configuration system makes it possible to adapt the functionalities of the cockpit of the aircraft to the profiles.