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Dynamic analysis of fretting-wear in joint interface by a multiscale harmonic balance method coupled with explicit or implicit integration schemes
Salles, Loïc; Gouskov, Alexander M.; Blanc, Laurent et al.
2010In ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010
Peer reviewed
 

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Keywords :
Bladed disk; Contact interface; Friction damper; Harmonic Balance method; Implicit and explicit integration; Implicit integration; Implicit schemes; Joint interfaces; Lagrangian; Life expectancies; Multiscales; Non-linear solver; Numerical experiments; Numerical investigations; Prediction-correction; Relative displacement; Time algorithms; Time-scales; Engineering (all)
Abstract :
[en] Assembled bladed disks have many contact interfaces (blade-disk joint, blade shrouds, friction damper, etc). Because of relative displacements at these interfaces, fretting-wear can occur, which shortens the life expectancy of the structure. Moreover, vibrations that occur in bladed-disks can increase this fretting-wear phenomenon. Two previous papers in Turboexpo have introduced a numerical method based on the Dynamical Lagrangian Frequency Time algorithm (DLFT) to calculate worn geometry, especially wear of bladed-disks' dovetail roots. Numerical investigations have illustrated the performances of this method and shown the coupling between dynamical and tribological phenomena. The basic idea of the DLFT-with-wear method is to separate time in two scales, slow scale for tribological phenomena and fast scale for dynamics. In the present paper, implicit and explicit integration schemes on the slow time scale are compared. An ad hoc prediction-correction method is used in both methods to accelerate the convergence of the non-linear solver. Numerical experiments on bladed-disk show that the implicit scheme is more appropriate to deal with fretting-wear under dynamical loading. Copyright © 2010 by ASME.
Disciplines :
Aerospace & aeronautics engineering
Mechanical engineering
Author, co-author :
Salles, Loïc  ;  Université de Liège - ULiège > Aérospatiale et Mécanique (A&M) ; Moscow State Technical University Named after Bauman, Moscow, Russian Federation ; École Centrale de Lyon, Laboratoire de Tribologie et Dynamique des Syst Èmes, 69134 Ecully Cedex, France ; Snecma - Safran Group, 77550 Moissy-Cramayel, France
Gouskov, Alexander M.;  Moscow State Technical University Named after Bauman, Moscow, Russian Federation
Blanc, Laurent;  École Centrale de Lyon, Laboratoire de Tribologie et Dynamique des Syst Èmes, 69134 Ecully Cedex, France
Thouverez, Fabrice;  École Centrale de Lyon, Laboratoire de Tribologie et Dynamique des Syst Èmes, 69134 Ecully Cedex, France
Jean, Pierrick;  Snecma - Safran Group, 77550 Moissy-Cramayel, France
Language :
English
Title :
Dynamic analysis of fretting-wear in joint interface by a multiscale harmonic balance method coupled with explicit or implicit integration schemes
Publication date :
December 2010
Event name :
Volume 6: Structures and Dynamics, Parts A and B
Event place :
Gbr
Event date :
14-06-2010 => 18-06-2010
Audience :
International
Main work title :
ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010
Publisher :
ASMEDC
ISBN/EAN :
978-0-7918-4401-4
Peer review/Selection committee :
Peer reviewed
Funders :
IGTI - International Gas Turbine Institute
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