Adaptive Vibration Data Averaging for Aircraft Displays

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Solution Overview

Problem

Aircraft systems face delays in accurately representing vibration data due to averaging methods that result in longer 'recovery times' when data values vary, leading to delayed representation of accurate information on displays for pilots and co-pilots.

Innovation Solution

A method involving a control module that receives data from sensors, calculates a delta between data points, compares it to a reference threshold, and dynamically adjusts the number of data points for averaging, providing immediate indications on displays when the delta exceeds or falls below the threshold, thereby reducing recovery time.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of time

If a set number of samples is used for averaging vibration data, then the averaging process is simple and consistent, but the recovery time increases and tracking of varied data values is delayed

Engineering Contradiction:
Improverecovery timeVSAvoidaveraging process complexity
Core Design Contradiction:
Loss of timeVSDevice complexity

Solution Approach 1:

The patent applies dynamics by making the averaging window size adaptive rather than fixed. The control module dynamically adjusts the number of data points included in the averaging calculation based on real-time comparison of consecutive data values against a threshold. When variation exceeds the threshold, the system reduces the averaging window to accelerate recovery time, thereby resolving the contradiction between simple averaging and fast tracking of varied data.

Inventive Principle:
Principle #15Dynamics

2Stability of the object's composition

If more data points are averaged, then the data representation is smoother and more stable, but the delay in matching varied data values increases

Engineering Contradiction:
Improvedata stabilityVSAvoidtracking delay
Core Design Contradiction:
Stability of the object's compositionVSLoss of time

Solution Approach 1:

The system dynamically adjusts the averaging window size based on data stability assessment. When consecutive data values vary beyond a threshold, the system automatically reduces the number of data points in the averaging calculation, enabling faster tracking of varied values. When data is stable, a larger averaging window maintains smooth representation. This dynamic adaptation resolves the contradiction between data stability and tracking speed.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent changes the parameter of averaging window size based on the calculated delta between consecutive data points. By comparing the absolute difference to a threshold and adjusting the number of data points accordingly, the system optimizes the balance between stability and responsiveness. This parameter change strategy enables the system to maintain data stability during normal operation while quickly adapting to sudden changes.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS10703503B2Method of displaying data in an aircraft
Publication Date: 2020.07.07 GENERAL ELECTRIC CO
  • US10703503B2 patent drawing
  • US10703503B2 patent drawing
  • US10703503B2 patent drawing

AI summary

A method and apparatus of displaying data in an aircraft, the method including receiving data, from at least one sensor operably coupled to the aircraft, averaging, by a control module, at least two data points of the received data to define a delta and averaged data, comparing, by the control module, the delta to a reference threshold value, and providing an indication, on a display of the aircraft, of the averaged data based on the comparing.