IMPLEMENTATION OF A RIG TEST FOR ROTOR/STATOR INTERACTION OF LOWPRESSURE COMPRESSOR BLADES AND COMPARISON OF EXPERIMENTAL RESULTS WITH NUMERICAL MODEL

Pacyna, Laura; Bertret, Alexandre; Derclaye, Alain; Papeleux, Luc; Ponthot, Jean-Philippe

doi:10.1115/GT2020-14266

Paper published in a book (Scientific congresses and symposiums)

IMPLEMENTATION OF A RIG TEST FOR ROTOR/STATOR INTERACTION OF LOWPRESSURE COMPRESSOR BLADES AND COMPARISON OF EXPERIMENTAL RESULTS WITH NUMERICAL MODEL

Pacyna, Laura; Bertret, Alexandre; Derclaye, Alain et al.

2020 • In Proceedings of ASME Turbo Expo 2020

Peer reviewed

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https://hdl.handle.net/2268/248688

DOI
10.1115/GT2020-14266

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Keywords :

Rotor/stator interaction; nonlinear dynamics; abradable coating,; wear; friction

Abstract :

[en] To investigate the contact phenomenon between the blade tip and the abradable coated casing, a rig test was designed and built. This rig test fills the following constraints: simplification of the low-pressure compressor environment but realistic mechanical conditions, ability to test several designs in short time, at low cost and repeatability. The rig test gives the opportunity to investigate the behavior of different blade designs regarding the sought phenomenon, to refine and mature the phenomenon comprehension and to get data for the numerical tool validation. The numerical tool considers a 3D finite elements model of low-pressure compressor blades with a surrounding rigid casing combined with a specialized model to take into account the effects of the wear of the abradable coating on the blade dynamics. Numerical results are in good agreement with tests in terms of: critical angular speed, blade dynamics and wear pattern on the abradable coated casing

Disciplines :

Aerospace & aeronautics engineering

Author, co-author :

Pacyna, Laura; Safran Aero Boosters

Bertret, Alexandre; Safran Aero Boosters

Derclaye, Alain; Safran Aero Boosters

Papeleux, Luc ; Université de Liège - ULiège > Département d'aérospatiale et mécanique > LTAS-Mécanique numérique non linéaire

Ponthot, Jean-Philippe ; Université de Liège - ULiège > Département d'aérospatiale et mécanique > LTAS-Mécanique numérique non linéaire

Language :

English

Title :

IMPLEMENTATION OF A RIG TEST FOR ROTOR/STATOR INTERACTION OF LOWPRESSURE COMPRESSOR BLADES AND COMPARISON OF EXPERIMENTAL RESULTS WITH NUMERICAL MODEL

Publication date :

2020

Event name :

ASME Turbo Expo 2020 - Turbomachinery Technical Conference and Exposition - GT2020

Event organizer :

ASME

Event place :

London, United Kingdom

Event date :

June 22-26, 2020

Audience :

International

Main work title :

Proceedings of ASME Turbo Expo 2020

Pages :

GT2020-14266

Peer reviewed :

Peer reviewed

Name of the research project :

GREENOMAT/ABRAWAL

Funders :

DGTRE - Région wallonne. Direction générale des Technologies, de la Recherche et de l'Énergie

Available on ORBi :

since 21 June 2020

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