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

Bach, Malte (2012) Inbetriebnahme eines Teststandes für ein Turbinentriebwerk und Identizierung der Parameter des Triebwerks. Bachelor's, Hochschule Bremen.

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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.

Item URL in elib:https://elib.dlr.de/103244/
Document Type:Thesis (Bachelor's)
Title:Inbetriebnahme eines Teststandes für ein Turbinentriebwerk und Identizierung der Parameter des Triebwerks
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Bach, MalteUNSPECIFIEDUNSPECIFIED
Date:January 2012
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:EAGLE Triebwerk Jet Engine
Institution:Hochschule Bremen
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Technik für Raumfahrtsysteme
DLR - Research theme (Project):R - Lageregelungstechnik / Formationsflug (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Navigation and Control Systems
Deposited By: Dumke, Michael
Deposited On:03 Mar 2016 10:09
Last Modified:17 Nov 2016 10:53

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