Assessment of geometric nonlinearities influence on NASA rotor 37 response to blade tip/casing rubbing events

Delhez, Elise; Nyssen, Florence; Golinval, Jean-Claude; Batailly, Alain

doi:10.1115/GT2021-58931

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Assessment of geometric nonlinearities influence on NASA rotor 37 response to blade tip/casing rubbing events

Delhez, Elise; Nyssen, Florence; Golinval, Jean-Claude et al.

2021 • In Proceedings of ASME Turbo Expo 2021

Peer reviewed

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https://hdl.handle.net/2268/257608

DOI
10.1115/GT2021-58931

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Keywords :

Structural dynamics; Model reduction; Geometrical nonlinearities; Contact nonlinearities

Abstract :

[en] This paper uses a recently derived reduction procedure to study the contact interactions of an industrial blade undergoing large displacements. The reduction technique consists in projecting the dynamical problem onto a reduction basis composed of Craig-Bampton modes and a selection of their modal derivatives. The internal nonlinear forces due to large displacements are evaluated with the stiffness evaluation procedure and contact is numerically handled using Lagrange multipliers. The numerical strategy is applied on an open industrial compressor blade model based on the NASA rotor 37 blade in order to promote reproducibility of results. Two contact scenarios are investigated: one with direct contact between the blade and the casing and one with an abradable material deposited on the casing. The influence of geometric nonlinearities is assessed in both cases. In particular, contact interaction maps and abradable coating wear pattern maps are used to identify the main interactions that can be detrimental for the engine integrity.

Disciplines :

Aerospace & aeronautics engineering

Author, co-author :

Delhez, Elise ; Université de Liège - ULiège > Département d'aérospatiale et mécanique > LTAS - Vibrations et identification des structures

Nyssen, Florence ; Université de Liège - ULiège > Département d'aérospatiale et mécanique > Département d'aérospatiale et mécanique

Golinval, Jean-Claude ; Université de Liège - ULiège > Département d'aérospatiale et mécanique > LTAS - Vibrations et identification des structures

Batailly, Alain; Polytechnique Montréal > Département de génie mécanique > Laboratoire d'Analyse Vibratoire et Acoustique

Language :

English

Title :

Assessment of geometric nonlinearities influence on NASA rotor 37 response to blade tip/casing rubbing events

Publication date :

June 2021

Event name :

ASME Turbo Expo 2021

Event organizer :

ASME

Event date :

du 7 juin 2021 au 11 juin 2021

Audience :

International

Main work title :

Proceedings of ASME Turbo Expo 2021

Peer reviewed :

Peer reviewed

Funders :

F.R.S.-FNRS - Fonds de la Recherche Scientifique [BE]

Available on ORBi :

since 03 March 2021

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