Aircraft Handle Assembly Light Panel Mode Feedback

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Solution Overview

Problem

Modern aircraft have complex systems that make it difficult for pilots to quickly identify critical operational changes, necessitating a system to provide clear visual feedback regarding the mode of operation of actuatable components.

Innovation Solution

A system comprising a controller and a handle assembly with an integrated light panel that selectively illuminates to indicate whether the actuatable component is in automatic or manual mode, using color changes, intensity variations, or flashing patterns to inform the user.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Quantity of substance

If multiple systems and annunciators are used to convey critical information, then the quantity of information provided increases, but the difficulty for pilots to quickly identify critical operational changes increases

Engineering Contradiction:
Improvequantity of informationVSAvoiddifficulty to identify critical changes
Core Design Contradiction:
Quantity of substanceVSDifficulty of detecting and measuring

Solution Approach 1:

The system segments the complex array of annunciators and systems into distinct functional groups (automatic systems, manual systems, engaged systems). Each group is visually separated and can be independently monitored, allowing pilots to quickly identify critical changes without being overwhelmed by the entire system display.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system employs color-coded indicators to represent different operational modes and states. Color changes provide immediate visual feedback about system status and critical operational changes, enabling pilots to rapidly detect and respond to important conditions without interpreting complex text or numerical data.

Inventive Principle:
Principle #32Color changes

2Measurement precision

If visual feedback is provided for each system individually, then the precision of system status information increases, but the device complexity increases

Engineering Contradiction:
Improveprecision of system status informationVSAvoidcomplexity of visual feedback system
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system uses a universal visual feedback mechanism that serves multiple functions: indicating automatic/manual mode, showing system engagement status, and highlighting critical changes. This multi-functional approach provides precise system status information without requiring separate complex indicator systems for each function.

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

Solution Approach 2:

The system merges multiple status indicators into integrated visual displays that show combined information about system mode, engagement status, and operational state. This consolidation provides comprehensive precision information while reducing the overall complexity compared to having separate indicators for each parameter.

Inventive Principle:
Principle #5Merging (Combining)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The system effectively alerts pilots to changes in the mode of operation, enhancing situational awareness and enabling timely responses to unexpected conditions by providing clear visual feedback.

Implementation Method 1

a light panel integrated with the handle assembly, in communication with said controller, and configured to selectively illuminate to inform a user of the mode of the actuatable component

Methodology Applied
Scientific EffectLight emission: Light Emitting Diode

Data Source

PatentUS9771142B2Systems and methods for providing visual feedback in aircraft
Publication Date: 2017.09.26 GULFSTREAM AEROSPACE CORP
  • US9771142B2 patent drawing
  • US9771142B2 patent drawing
  • US9771142B2 patent drawing

AI summary

A system for providing visual feedback in an aircraft having an actuatable component includes a controller providing automatic control of the actuatable component in an automatic mode and permitting manual control of the actuatable component in a manual mode. A handle assembly is in communication with the actuatable component to provide manual control of the actuatable component in the manual mode. The system also includes a light panel integrated with the handle assembly, in communication with said controller, and configured to selectively illuminate to inform a user of the mode of the actuatable component.