Inbetriebnahme eines Teststandes für ein Turbinentriebwerk und Identizierung der Parameter des Triebwerks

Abstract

The content of the bachelor thesis includes the construction and commissioning of a test bench for a model jet engine with thrust vector control and a thrust of 400N. In addition, for the identification of the dynamic characteristic of the jet engine is a six-componentsensor selected and the test setup is analyzed of natural frequencies in order to prevent falsification of the measured values. The thesis also includes the commissioning and calibration of the test setup. For the determination of the dynamic characteristic of the engine test sequences were created with consideration of the critical operating range of a compressor.