Rotorcraft LTE Alert System Using Wind Data Overlay

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Solution Overview

Problem

Rotorcraft pilots face challenges in detecting unanticipated yaw (loss of tail rotor effectiveness) due to low airspeed and wind conditions, which can lead to increased susceptibility during operations, particularly in low airspeed and specific wind direction scenarios, necessitating improved alert systems to enhance situational awareness.

Innovation Solution

A system that processes data from an air data computer, performance database, and weather sources to determine if a rotorcraft is within a loss of tail rotor effectiveness (LTE) zone, overlaying visually distinguishable symbols on the cockpit display to indicate wind velocity and direction, thereby alerting the pilot to potential LTE conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of information

If the pilot relies on traditional cockpit displays (PFD and MFD) to monitor flight conditions, then the pilot can access comprehensive flight information, but the pilot cognitive workload increases and situational awareness of LTE risk decreases

Engineering Contradiction:
Improvesituational awareness of LTE riskVSAvoidpilot cognitive workload
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The system segments the complex flight information by extracting only the critical parameters (airspeed, wind velocity, wind direction, height) needed for LTE assessment and presenting them separately through dedicated LTE zone indicators on the PFD and MFD, rather than requiring the pilot to process all flight parameters simultaneously

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system performs preliminary assessment of LTE risk by continuously monitoring flight parameters and pre-calculating LTE zone conditions before the pilot needs to make decisions, then presents the results as ready-to-interpret visual indicators that require minimal cognitive processing

Inventive Principle:
Principle #10Preliminary action

2Productivity

If the system provides detailed flight information through traditional displays, then comprehensive data is available, but the pilot cannot quickly identify LTE risk conditions

Engineering Contradiction:
Improvepilot response speed to LTE conditionsVSAvoiddetection of LTE zone conditions
Core Design Contradiction:
ProductivityVSDifficulty of detecting and measuring

Solution Approach 1:

The system uses color-coded visual indicators (such as amber or red alerts) to signify LTE zone conditions on the PFD and MFD, allowing the pilot to instantly recognize hazardous conditions through color perception rather than numerically analyzing flight parameters

Inventive Principle:
Principle #32Color changes

Solution Approach 2:

The system adds a new visual dimension to the traditional flight display by overlaying LTE zone indicators that provide spatial and contextual information about tail rotor effectiveness risk, enabling the pilot to detect conditions at a glance without complex interpretation

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Reliability

If the pilot maintains acute awareness of wind conditions to prevent LTE, then safety improves, but the pilot cognitive workload increases

Engineering Contradiction:
Improvesafety against LTEVSAvoidpilot cognitive workload
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system provides continuous feedback to the pilot by monitoring wind velocity and direction alongside airspeed and height, then presenting integrated LTE risk assessment through visual indicators that automatically update as flight conditions change, eliminating the need for the pilot to manually assess multiple parameters

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system performs the complex assessment of LTE risk automatically by processing flight parameters and wind data through the LTE zone determination algorithm, then presents the results as intuitive visual indicators, allowing the pilot to benefit from enhanced safety without bearing the cognitive burden of the assessment process

Inventive Principle:
Principle #25Self-service

Data Source

PatentEP3144637B1Method and system for improving situational awareness of unanticipated YAW on a rotorcraft system
Publication Date: 2018.03.14 HONEYWELL INTERNATIONAL INC
  • EP3144637B1 patent drawingFigure 1
  • EP3144637B1 patent drawingFigure 2
  • EP3144637B1 patent drawingFigure 3

AI summary

A method and system for alerting a pilot to a potential unanticipated LTE with simple intuitive symbology on the cockpit display is provided. The provided method and system evaluates rotorcraft airspeed, wind velocity, wind direction, and rotorcraft height above ground to predict several scenarios for LTE zones. The provided method and system overlays or superimposes simple intuitive symbology (100, 402, 408, 410) on the existing PFD (400) and/or MFD to alert a pilot to a potential LTE.