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NASA NTRS ยท 19900000213

System Detects Vibrational Instabilities

Abstract

Sustained vibrations at two critical frequencies trigger diagnostic response or shutdown. Vibration-analyzing electronic system detects instabilities of combustion in rocket engine. Controls pulse-mode firing of engine and identifies vibrations above threshold amplitude at 5.9 and/or 12kHz. Adapted to other detection and/or control schemes involving simultaneous real-time detection of signals above or below preset amplitudes at two or more specified frequencies. Potential applications include rotating machinery and encoders and decoders in security systems.

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BibTeXRIS

Bozeman, Richard J., Jr.. 1990-05-01. System Detects Vibrational Instabilities. https://ntrs.nasa.gov/citations/19900000213

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