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Faculté des Sciences appliquées
Faculté des Sciences appliquées
MASTER THESIS
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Master thesis and internship[BR]- Master's thesis : Modelling of Gas Foil Bearing with a high order Discontinuous Galerkin Method[BR]- Integration Internship

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Alshikh Saleh, Ammar ULiège
Promotor(s) : Hillewaert, Koen ULiège
Date of defense : 5-Sep-2022/6-Sep-2022 • Permalink : http://hdl.handle.net/2268.2/15884
Details
Title : Master thesis and internship[BR]- Master's thesis : Modelling of Gas Foil Bearing with a high order Discontinuous Galerkin Method[BR]- Integration Internship
Translated title : [fr] Modélisation d'un palier à air avec une méthode Galerkin discontinue d'ordre élevé
Author : Alshikh Saleh, Ammar ULiège
Date of defense  : 5-Sep-2022/6-Sep-2022
Advisor(s) : Hillewaert, Koen ULiège
Committee's member(s) : Boman, Romain ULiège
Levaux, Nayan ULiège
Heylen, Martin 
Language : English
Number of pages : 86
Keywords : [en] Discontinuous Galerkin, Gas foil bearing, Reynolds equation, Bearing number, Load capacity
Discipline(s) : Engineering, computing & technology > Aerospace & aeronautics engineering
Target public : Researchers
Professionals of domain
Student
General public
Institution(s) : Université de Liège, Liège, Belgique
Degree: Master en ingénieur civil en aérospatiale, à finalité spécialisée en "aerospace engineering"
Faculty: Master thesis of the Faculté des Sciences appliquées

Abstract

[en] In recent years, foil bearings, a special class of gas bearings, began to receive widespread converge in many scientific publications because of their advantages of environmental durability, higher reliability in operation (oil-free), and higher load capacity at high speed. Air Foil Bearing (AFB) supporting direct drive compressors or/and turbines have been gaining popularity in recent years. Mitis SA is developing a new generation of clean energy converters for decentralized Combined Heat and Power (CHP) based on flameless combustion chamber microturbines. Mitis SA is using AFB in their systems to guarantee an oil-free system and increase reliability.
The overall objective of this work is to contribute to a better understanding of the AFB technology. The work focuses particularly on the behaviour of the lubrication gas film. Numerical simulations of the isothermal, steady state Reynolds equation using the Discontinuous Galerkin Finite Element Method (DG-FEM) are performed. Compared to classical FD and FV methods, such a method provides high accuracy in terms of interpolation and spectral properties on unstructured meshes without opting for large stencils. The work comprises the development and implementation of a numerical prediction code with the use of DG-FEM. The numerical aspect of the hyperbolic-elliptic problem has been addressed with the implementation of specific approaches. First, upwind flux has been proposed for the convective formulation, and then an incomplete internal penalty method (IIPM) has been considered to evaluate the diffusive interface flux. Newton-Raphson method has been used to solve the nonlinear equation. The residual and the inverse of the Jacobian have been computed using direct solver, which is based upon the LU factorization technique. All these strategies were implemented in ForDGe, an immersed boundary, and in turn, Adaptive Mech Refinement (AMR) on multiple order Cartesian grids, still under development at the University of Liège.
The modelling of the foil structure is built based upon existing models. The coupling between structural and fluid parts has been done at the level of the film thickness using the Simple Elastic Foundation Model (SEFM). The validity of the analysis and numerical code has been assessed by comparing predictions to experimental and/or numerical published data.
This work would be recognized as the reference, providing numerical results for GFBs used by Mitis SA and/or any kind of GFBs with variable geometries and different working gases and operating conditions.


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Author

  • Alshikh Saleh, Ammar ULiège Université de Liège > Master ingé. civ. aérospat., à fin.

Promotor(s)

Committee's member(s)

  • Boman, Romain ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Département d'aérospatiale et mécanique
    ORBi View his publications on ORBi
  • Levaux, Nayan ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Design of Turbomachines
    ORBi View his publications on ORBi
  • Heylen, Martin Mitis
  • Total number of views 287
  • Total number of downloads 373










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