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Faculté des Sciences appliquées
Faculté des Sciences appliquées
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Quick step compressor mapping tool for pre-design studies

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De Greef, Cyril ULiège
Promoteur(s) : Hillewaert, Koen ULiège
Date de soutenance : 25-jui-2020/26-jui-2020 • URL permanente : http://hdl.handle.net/2268.2/8976
Détails
Titre : Quick step compressor mapping tool for pre-design studies
Titre traduit : [fr] Outils avant-projet compresseur
Auteur : De Greef, Cyril ULiège
Date de soutenance  : 25-jui-2020/26-jui-2020
Promoteur(s) : Hillewaert, Koen ULiège
Membre(s) du jury : Princivalle, Remy 
Andrianne, Thomas ULiège
Langue : Anglais
Nombre de pages : 71
Mots-clés : [en] Compressor
[en] Booster
[en] VSV
[en] MFT
Discipline(s) : Ingénierie, informatique & technologie > Ingénierie aérospatiale
Organisme(s) subsidiant(s) : Safran Aero Boosters
Public cible : Professionnels du domaine
Institution(s) : Université de Liège, Liège, Belgique
Diplôme : Master en ingénieur civil en aérospatiale, à finalité spécialisée en "aerospace engineering"
Faculté : Mémoires de la Faculté des Sciences appliquées

Résumé

[en] During the first steps of an aircraft engine design project, it is important to rapidly answer to a tender process. For that, it is important to rapidly provide the first compressor maps. The aim of this study is to create a tool which is able to build compressor maps of a booster composed of three stages from geometry and MFT data of the individual stages.
The first part of this project presents the company where this internship was performed : Safran Aero Boosters. Then, the main different types of compressors, and more specifically the low pressure axial flow compressor are presented. Finally, a brief description of the parameters of interest are developed.
The second part of this work is a bibliographical study where four methods are exposed. These are the Map Fitting Tool method (MFT), the previous booster scaling, the -lines method and the booster map warping which relies on the relative warps method. The chosen method of this internship is the MFT one because it is judged as the more physical : its parameters rely on work coefficient and low coefficient. Furthermore, the data used later to confirm the efficiency of the tools created are based on these MFT parameters. With this in mind, a complete description of the MFT methodology is presented.
The third part of this report presents the multi-stage engine studied. Furthermore, a thorough description of the stacking methodology used to perform the construction of the compressor map of a three-stage booster is performed.
The fourth part presents the first tool created during the internship which allows to stack up three stages with the same VSV schedule at different speeds of rotation. After a brief presentation of the implemented tool, the development of an application is discussed.
The last part of this project gives a brief description of the use of VSV in a multi-stage compressor. Then, the second tool implemented is presented. This tool allows to enter up to three stages with three different VSV schedules but each at a given rotation speed.
Due to the outbreak of Covid-19 in Belgium, exceptional measures where taken within Safran Aero Boosters which forced the workers to work at home. Therefore, I could not end my last week at SAB and retrieve the data necessary to present concrete applications of the tools created.


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Access Master_Thesis_DE_GREEF_Cyril.pdf
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Access Summary_DE_GREEF_Cyril.pdf
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Auteur

  • De Greef, Cyril ULiège Université de Liège > Master ingé. civ. aérospat., à fin.

Promoteur(s)

Membre(s) du jury

  • Princivalle, Remy
  • Andrianne, Thomas ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale
    ORBi Voir ses publications sur ORBi
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