Turbojet blade vibration data acquisition design and feasibility testing

A turbojet blade vibration data acquisition system was designed to allow the measurement of blade vibration. The data acquisition system utilizing 96 microprocessors to gather data from optical probes, store, sort and transmit to the central computer is described. Areas of high technical risk were i...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Frarey, J. L., Petersen, N. J., Hess, D. A.
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft Propulsion And Power
Online-Zugang:	Volltext bestellen
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