Rotor blade integrated sensor for monitoring of BVI caused pressures fluctuations

C. Gradolph, A. Friedberger, T. Ziemann, G. Müller, J. Wilde

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Scopus citations

Abstract

BVI is a main reason for undesired emitted noise levels in different helicopter flight situations and can be monitored and quantified with a rotor blade integrated pressure sensor. The sensor presented is robust against harsh environmental conditions in helicopter flight and on ground. It can be quickly installed and demounted in case of malfunctions and therefore needs low maintenance effort and time.

Original languageEnglish
Title of host publicationProceedings of the 3rd European Workshop - Structural Health Monitoring 2006
Pages331-338
Number of pages8
StatePublished - 2006
Externally publishedYes
Event3rd European Workshop on Structural Health Monitoring 2006 - Granada, Spain
Duration: 5 Jul 20067 Jul 2006

Publication series

NameProceedings of the 3rd European Workshop - Structural Health Monitoring 2006

Conference

Conference3rd European Workshop on Structural Health Monitoring 2006
Country/TerritorySpain
CityGranada
Period5/07/067/07/06

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