VTOL Roll Rate Scale Display for Flight Stability Control

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Vertical take-off and landing (VTOL) aircraft require effective systems for displaying aircraft roll rate due to their complex propulsion and control systems, which make stability sensitive to roll rates.

Innovation Solution

A system comprising geospatial sensors, a display device, and a controller that receives aircraft roll data, generates a roll rate scale, determines the aircraft's roll rate, and displays a graphical representation of the roll rate on the display device.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If complex propulsion and control systems are used in VTOL aircraft, then the aircraft can achieve vertical take-off and landing capability, but the stability of the aircraft becomes more sensitive to roll rates

Engineering Contradiction:
ImproveVTOL capabilityVSAvoidflight stability
Core Design Contradiction:
Adaptability or versatilityVSStability of the object's composition

Solution Approach 1:

The patent implements a feedback mechanism by continuously monitoring roll rate through geospatial sensors and providing real-time visual feedback to the pilot through a display device. The system measures actual roll rate, compares it against desirable ranges, and displays both the current value and the acceptable range boundaries, enabling the pilot to make corrective control inputs to maintain stability.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent introduces an intermediary system between the complex propulsion/control systems and the pilot - a roll rate display system that processes sensor data and presents processed information about roll rate status. This intermediary translates complex system behavior into comprehensible visual indicators, helping the pilot manage the stability challenges introduced by VTOL systems.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If roll rate awareness is enhanced through display systems, then operational safety is improved, but the device complexity increases

Engineering Contradiction:
Improveoperational safetyVSAvoiddisplay system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent achieves multi-functionality by integrating the roll rate display system into the existing aircraft display infrastructure. The same display device used for other flight parameters is utilized to show roll rate information, and the controller leverages existing geospatial sensor systems. This approach provides enhanced safety information without requiring entirely separate dedicated hardware systems.

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

Solution Approach 2:

The patent changes the parameter presentation by displaying roll rate as a visual indicator on an existing display device rather than adding physical instrumentation. The system transforms sensor data into graphical representations showing current roll rate position relative to desirable ranges, providing safety-critical information through parameter visualization rather than additional physical components.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentEP4513143A1Systems and methods for displaying aircraft roll rate on a vertical take-off and landing aircraft display
Publication Date: 2025.02.26 HONEYWELL INTERNATIONAL INC
  • EP4513143A1 patent drawingFigure 1
  • EP4513143A1 patent drawingFigure 2
  • EP4513143A1 patent drawingFigure 3

AI summary

Systems and methods are provided for displaying roll rate on a vertical take-off and landing (VTOL) aircraft display. Aircraft roll data is received from at least one geospatial sensor of the VTOL aircraft. A roll rate scale associated with a desirable roll rate range of the VTOL aircraft is generated. An aircraft roll rate of the VTOL aircraft is determined based on the aircraft roll data. The VTOL aircraft display, including a graphical representation of the roll rate scale and the aircraft roll rate with respect to the roll rate scale, is generated for display on the display device.