Füllekrug, Ulrich and Giese, Hubertus (2006) Vibration Tests on a Scheimpflugadapter. DLR-Interner Bericht. DLR IB 232-2006 C 05. 16 S.
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Abstract
A vibration test was performed on a camera support structure, a so-called Scheimpflugadapter. The tested structure was mounted on a multi-axial test facility and tested into the direction of the three translational axes. Sine sweep runs from 5 to 100 Hz with a maximum acceleration level of 4.5 g were performed. Also, a 10 min random excitation into the direction of one lateral axis was applied. The inspection of the Scheimpflugadapter after each test run showed that the adjustment mechanism was properly locked and that no displacements occured.
Item URL in elib: | https://elib.dlr.de/45875/ | ||||||||||||
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Document Type: | Monograph (DLR-Interner Bericht) | ||||||||||||
Title: | Vibration Tests on a Scheimpflugadapter | ||||||||||||
Authors: |
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Date: | 2006 | ||||||||||||
Open Access: | No | ||||||||||||
Number of Pages: | 16 | ||||||||||||
Status: | Published | ||||||||||||
Keywords: | Scheimpflugadapter, structural dynamics, dynamic qualification, vibration test, multi-axial test | ||||||||||||
HGF - Research field: | Aeronautics, Space and Transport (old) | ||||||||||||
HGF - Program: | Aeronautics | ||||||||||||
HGF - Program Themes: | Aircraft Research (old) | ||||||||||||
DLR - Research area: | Aeronautics | ||||||||||||
DLR - Program: | L ST - Starrflüglertechnologien | ||||||||||||
DLR - Research theme (Project): | L - Flexible Aircraft (old) | ||||||||||||
Location: | Göttingen | ||||||||||||
Institutes and Institutions: | Institute of Aeroelasticity | ||||||||||||
Deposited By: | Erdmann, Daniela | ||||||||||||
Deposited On: | 08 Jan 2007 | ||||||||||||
Last Modified: | 27 Apr 2009 13:17 |
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