Rotorcraft Flight Mode Annunciation System

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Solution Overview

Problem

The increasing complexity of rotorcraft systems makes it challenging for pilots to manage different flight modes and control inputs, as flight characteristics in various regimes are tightly coupled, leading to increased workload and potential instability, especially when transitioning between flight modes.

Innovation Solution

A system and method for automated flight mode annunciation using a flight control computer that selects and sets active flight modes based on pilot inputs, sensor data, and flight director coupling, with indicators on the instrument panel to clearly show the current flight mode, reducing pilot workload and enhancing stability by decoupling flight characteristics.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If automated flight mode selection is implemented, then pilot workload is reduced, but system complexity increases

Engineering Contradiction:
Improvepilot workloadVSAvoidsystem complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The flight control computer automatically monitors flight parameters and selects appropriate flight modes without requiring manual intervention from the pilot. The system serves itself by autonomously determining when to transition between flight modes based on sensed flight conditions, thereby reducing pilot workload while managing complexity through automation.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system continuously monitors flight parameters through sensors and uses this feedback to automatically adjust flight mode selections. The flight control computer receives real-time data about flight conditions and adjusts modes accordingly, creating a closed-loop system that reduces pilot workload while maintaining appropriate complexity through intelligent feedback mechanisms.

Inventive Principle:
Principle #23Feedback

2Adaptability or versatility

If multiple flight modes are available, then adaptability is improved, but ease of operation deteriorates

Engineering Contradiction:
Improveflight mode adaptabilityVSAvoidcontrol management
Core Design Contradiction:
Adaptability or versatilityVSEase of operation

Solution Approach 1:

The system dynamically adjusts the available flight modes based on current flight conditions. Rather than presenting all possible modes to the pilot at all times, the system adapts the mode selection to match the current flight regime, providing adaptability when needed while maintaining ease of operation by limiting choices to relevant options.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The flight modes are segmented into different categories or subsets based on flight conditions. The system divides the comprehensive set of flight modes into manageable groups, presenting only the appropriate subset to the pilot for each flight regime, thereby maintaining adaptability across all conditions while improving ease of operation within each segment.

Inventive Principle:
Principle #1Segmentation

3Stability of the object's composition

If flight mode transitions are automated, then flight stability is improved, but loss of information increases

Engineering Contradiction:
Improveflight stabilityVSAvoidpilot awareness
Core Design Contradiction:
Stability of the object's compositionVSLoss of information

Solution Approach 1:

The system provides continuous feedback to the pilot about the current flight mode and any upcoming transitions. By maintaining an information feedback loop to the cockpit displays, the system ensures pilot awareness is maintained even as automated transitions occur, balancing flight stability with information retention.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system performs preliminary actions by preparing for flight mode transitions in advance and notifying the pilot before actual mode changes occur. This advance notice maintains pilot awareness and understanding of system status while allowing smooth, stable transitions to occur automatically.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS11136136B2System and method for flight mode annunciation
Publication Date: 2021.10.05 TEXTRON INNOVATIONS INC
  • US11136136B2 patent drawing
  • US11136136B2 patent drawing
  • US11136136B2 patent drawing

AI summary

In an embodiment, a method of indicating flight modes of a rotorcraft includes: detecting a change in flight mode of the rotorcraft from a previous flight mode to an active flight mode, the active flight mode and the previous flight mode each being from one of a first subset or a second subset of a plurality of flight modes; determining whether the active flight mode and the previous flight mode are from different subsets of the plurality of flight modes; and updating one or more flight mode indicators on an instrument panel of the rotorcraft in response to the active flight mode and the previous flight mode being from different subsets of the plurality of flight modes.