Rotorcraft Drive System Anomaly Detection via Sub-Synchronous Spectrum Analysis

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Solution Overview

Problem

Current diagnostic systems for aircraft drive systems, such as rotorcraft, have limited effectiveness in monitoring and identifying anomalies due to the sinusoidal or oscillatory vibratory forces produced during operation, which are not adequately addressed by existing methods like cepstrum analysis and wavelet techniques.

Innovation Solution

A method and system that involves obtaining vibration and tachometer signals, generating a time synchronous average vibration signal, processing it to produce a frequency-domain spectrum, selecting a sub-synchronous band, and determining a condition indicator to diagnose anomalies in drive train components, which includes using discrete Fourier transform and accelerometers for real-time monitoring.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If cepstrum analysis and wavelet techniques are used for vibration monitoring, then diagnostic capability is provided, but the method has limited use and cannot adequately address sinusoidal or oscillatory vibratory forces in rotorcraft drive systems

Engineering Contradiction:
Improvediagnostic effectivenessVSAvoidapplicability to oscillatory vibrations
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The patent transforms the vibration signal from time domain to frequency domain using Fast Fourier Transform (FFT), and then to a different representation using the Hilbert transform. This parameter transformation allows the system to effectively analyze sinusoidal and oscillatory vibratory forces that were not adequately addressed by conventional cepstrum analysis and wavelet techniques, thereby improving both diagnostic effectiveness and adaptability to rotorcraft drive systems

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If traditional vibration monitoring methods are implemented, then some diagnostic information is obtained, but early identification of unhealthy components is not achieved

Engineering Contradiction:
Improveanomaly detection accuracyVSAvoidtime to detect component failure
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The patent applies envelope analysis and Hilbert transform to extract modulating frequencies from the vibration signal, which reveals early signs of component degradation before they develop into critical failures. This preliminary detection capability allows maintenance to be scheduled proactively, preventing catastrophic failures and reducing unplanned downtime in rotorcraft operations

Inventive Principle:
Principle #10Preliminary action

3Loss of information

If comprehensive vibration analysis is performed on rotorcraft drive systems, then diagnostic information is obtained, but the complexity of processing oscillatory signals increases

Engineering Contradiction:
Improvevibration signal information retentionVSAvoidsignal processing complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The patent extracts the envelope signal from the complex vibration data using Hilbert transform, isolating the modulating frequencies that contain the diagnostic information. This extraction process simplifies the signal representation while retaining the essential information about component health, making the data more manageable for analysis without losing critical diagnostic content

Inventive Principle:
Principle #2Taking out (Extraction)

Data Source

PatentUS10424134B2Diagnostic method, system and device for a rotorcraft drive system
Publication Date: 2019.09.24 BELL HELICOPTER TEXTRON INC
  • US10424134B2 patent drawing
  • US10424134B2 patent drawing
  • US10424134B2 patent drawing

AI summary

There is a method, system, and device for diagnosing an anomaly of a monitored component in a drive train, the method including obtaining original data based on samples of a vibration signal and a tachometer signal; generating a time synchronous average vibration signal; processing the time synchronous average vibration signal to produce a frequency-domain spectrum; determining the complex magnitudes of the frequency-domain spectrum; selecting a sub-synchronous band of the complex magnitudes of the frequency-domain spectrum to generate a sub-synchronous spectrum; and determining the mean of the sub-synchronous spectrum to generate a condition indicator.