Experimental identification of an aircraft piccolo tube exhibiting nonsmooth nonlinearities

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

Experimental identification of an aircraft piccolo tube exhibiting nonsmooth nonlinearities

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

Onderzoeksoutput: Hoofdstuk in Boek/Rapport/Congresprocedure › Conferentiebijdrage › Academic

Samenvatting

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.

Originele taal-2	Engels
Titel	Proceedings of the 9th European Nonlinear Oscillations Conference (ENOC)
Redacteuren	G. Stépán, G. Csernák
Plaats van productie	Budapest
Aantal pagina's	2
Status	Gepubliceerd - jun. 2017
Extern gepubliceerd	Ja
Evenement	9th European Nonlinear Oscillations Conference, ENOC 2017 - Budapest University of Technology and Economics, Budapest, Hongarije Duur: 25 jun. 2017 → 30 jun. 2017 Congresnummer: 9 http://congressline.hu/enoc2017/

Congres

Congres	9th European Nonlinear Oscillations Conference, ENOC 2017
Verkorte titel	ENOC 2017
Land/Regio	Hongarije
Stad	Budapest
Periode	25/06/17 → 30/06/17
Internet adres	http://congressline.hu/enoc2017/

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title = "Experimental identification of an aircraft piccolo tube exhibiting nonsmooth nonlinearities",

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.",

author = "T. Dossogne and M. Schoukens and B. Bernay and J.M.M.G. No{\"e}l and G. Kerschen",

year = "2017",

month = jun,

language = "English",

isbn = "978 - 963 - 12 - 9168 - 1",

editor = "G. St{\'e}p{\'a}n and G. Csern{\'a}k",

booktitle = "Proceedings of the 9th European Nonlinear Oscillations Conference (ENOC)",

note = "9th European Nonlinear Oscillations Conference, ENOC 2017, ENOC 2017 ; Conference date: 25-06-2017 Through 30-06-2017",

url = "http://congressline.hu/enoc2017/",

}

Dossogne, T, Schoukens, M, Bernay, B, Noël, JMMG & Kerschen, G 2017, Experimental identification of an aircraft piccolo tube exhibiting nonsmooth nonlinearities. in G Stépán & G Csernák (uitgave), Proceedings of the 9th European Nonlinear Oscillations Conference (ENOC). Budapest, 9th European Nonlinear Oscillations Conference, ENOC 2017, Budapest, Hongarije, 25/06/17.

TY - GEN

T1 - Experimental identification of an aircraft piccolo tube exhibiting nonsmooth nonlinearities

AU - Dossogne, T.

AU - Schoukens, M.

AU - Bernay, B.

AU - Noël, J.M.M.G.

AU - Kerschen, G.

N1 - Conference code: 9

PY - 2017/6

Y1 - 2017/6

N2 - 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.

AB - 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.

M3 - Conference contribution

SN - 978 - 963 - 12 - 9168 - 1

BT - Proceedings of the 9th European Nonlinear Oscillations Conference (ENOC)

A2 - Stépán, G.

A2 - Csernák, G.

CY - Budapest

T2 - 9th European Nonlinear Oscillations Conference, ENOC 2017

Y2 - 25 June 2017 through 30 June 2017

ER -

Experimental identification of an aircraft piccolo tube exhibiting nonsmooth nonlinearities

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