EFB Turbulence Guidance Using FMS Pilot Intent

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Solution Overview

Problem

Existing flight management systems (FMS) are slow and expensive to update due to stringent certification processes, limiting the implementation of new features for turbulence mitigation, while Electronic Flight Bags (EFB) offer a quicker and less rigorous update path but lack integration with FMS data for personalized turbulence suggestions.

Innovation Solution

A turbulence management system integrated with an EFB infers pilot intent from FMS inputs, receives aircraft metrics, and generates personalized suggestions to mitigate turbulence while satisfying pilot intent, using a turbulence manager to communicate with the FMS and provide user-friendly interface adjustments during turbulent conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If FMS is updated with new turbulence mitigation features, then turbulence mitigation capability is improved, but certification time and cost increase

Engineering Contradiction:
Improveturbulence mitigation capabilityVSAvoidcertification time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system separates the turbulence mitigation functionality into a distinct module that operates independently from the core FMS. The processor identifies pilot intent and generates suggestions without requiring certification of the entire FMS system, only the standalone turbulence mitigation module needs validation.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

An intermediary suggestion generation module is introduced between the pilot input and the aircraft control systems. This module processes pilot intent and generates turbulence mitigation suggestions that can be implemented without direct FMS updates, bypassing the lengthy certification process while still improving turbulence handling capability.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If FMS is updated with new turbulence mitigation features, then turbulence mitigation capability is improved, but update cost increases

Engineering Contradiction:
Improveturbulence mitigation capabilityVSAvoidupdate cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The turbulence mitigation functionality is segmented as a separate process that runs on existing FMS hardware without requiring system-wide updates. This reduces development, testing, and certification costs since only the specific turbulence module needs validation rather than the entire FMS.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system uses existing FMS resources (processors, memory, sensors) to provide turbulence mitigation suggestions without requiring additional hardware or expensive system-wide updates. The existing infrastructure serves the new function at minimal marginal cost.

Inventive Principle:
Principle #25Self-service

3Loss of energy

If turbulence mitigation suggestions are provided, then fuel burn is reduced, but system complexity increases

Engineering Contradiction:
Improvefuel burnVSAvoidsystem complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The system continuously monitors pilot inputs and aircraft state, using feedback loops to identify pilot intent and adjust turbulence mitigation suggestions in real-time. This feedback mechanism enables fuel savings through optimized flight paths and altitude adjustments without requiring complex manual calculations or multiple separate systems.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The FMS uses its own existing data and processing capabilities to generate turbulence mitigation suggestions, rather than requiring external complex systems. The processor leverages already-collected flight data, weather information, and aircraft performance parameters to provide suggestions that reduce fuel burn without adding significant system complexity.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS12562065B2Assisted turbulence EFB interaction
Publication Date: 2026.02.24 THE BOEING CO
  • US12562065B2 patent drawing
  • US12562065B2 patent drawing
  • US12562065B2 patent drawing

AI summary

The present disclosure provides a turbulence management system for providing suggestions to a pilot that mitigate the effects of turbulence. These suggestions can be output to the pilot using an EFB. As mentioned above, an EFB can be communicatively coupled to a FMS such that the EFB has access to the data in the FMS. From the pilot's interactions with the FMS, the EFB can identify the pilot's intent such as landing, taking off, plotting a course change, changing altitude, maintaining a cruising altitude, etc. Once the intent is known, the EFB can output a suggestion to the pilot that satisfies the intent, but mitigates the harmful effects of turbulence. In one aspect, this suggestion is generated using the flight plant and aircraft metrics available from the FMS.