Experimental identification of an aircraft piccolo tube exhibiting nonsmooth nonlinearities

T. Dossogne, M. Schoukens, B. Bernay, J.M.M.G. Noël, G. Kerschen

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademic

Abstract

Piccolo tubes are parts of aircraft wings anti-icing system and consist of titanium pipes inserted into the internal structure of the slat. Due to thermal expansion, clearances between the tube and its support are unavoidable, and cause the overall system to exhibit highly nonlinear behaviour, resulting from impacts and friction. This paper aims the complete nonlinear vibration analysis of an aircraft Piccolo tube, from measurements and identification to a thorough understanding of the dynamics and improvements of the
design.
Original languageEnglish
Title of host publicationProceedings of the 9th European Nonlinear Oscillations Conference (ENOC)
EditorsG. Stépán, G. Csernák
Place of PublicationBudapest
Number of pages2
Publication statusPublished - Jun 2017
Externally publishedYes
Event9th European Nonlinear Oscillations Conference (ENOC 2017) - Budapest University of Technology and Economics, Budapest, Hungary
Duration: 25 Jun 201730 Jun 2017
Conference number: 9
http://congressline.hu/enoc2017/

Conference

Conference9th European Nonlinear Oscillations Conference (ENOC 2017)
Abbreviated titleENOC 2017
Country/TerritoryHungary
CityBudapest
Period25/06/1730/06/17
Internet address

Fingerprint

Dive into the research topics of 'Experimental identification of an aircraft piccolo tube exhibiting nonsmooth nonlinearities'. Together they form a unique fingerprint.

Cite this