| Titre : | Design and Experimental Analysis of a Loop Heat Pipe for Thermal Control of Aircraft Engine Equipment |
| Type de document : | thèse |
| Auteurs : | Filippo PAGNONI, Auteur ; Yves BERTIN, Directeur de thèse ; Vincent AYEL, Directeur de thèse ; Institut PPRIME UPR CNRS 3346 - FTC, Commanditaire ; Valérie SARTRE, Rapporteur ; Sauro FILIPPESCHI, Rapporteur ; Lounes TADRIST, Examinateur ; Frédéric LEFEVRE, Examinateur |
| Année de publication : | 2019 |
| Importance : | 2016 p. |
| Note générale : | NNT 2019ESMA0004
Contents
List of Figures
List of Tables
Nomenclature
Bibliography
Annexes
Résumé étendu
Abstract
Keywords
|
| Catégories : | :Avions:Turboréacteurs
:Matériaux poreux:Fluides, Dynamique des
:Température:Régulation
Caloducs
Durée de vie (ingénierie)
Essais accélérés (technologie)
Hautes pressions
Hautes températures
Prototypes
|
| Résumé : | INTRODUCTION AND CONTEXT OF STUDY
HEAT PIPES RESEARCH AND TECHNOLOGY
Introduction
Why Two-Phase Passive Cooling
Heaat Pipes
Loop Heat Pipes
Conclusions
FEASABILITY STUDY: LHP FOR CORE COMPARTMENT THERMAL MANAGEMENT
Introduction
Thermal Requirements: Analysis of a Potential Application
Working Fluid and Construction Material Selection
Wick Resistance to Water Freezing Cycles
Identification of the Cold Spots within the Nacelle
Conclusions
WORKING FLUID SELECTION: COMPATIBILITY ANALYSIS
Introduction
Water-Titanium/Titanium Alloys Compatibility
Dowtherm J - Grade 9 Titanium and Z4CMN21 Steel Compatibility
Conclusions
LOOP HEAT PIPE DESIGN
Introduction
Evaporation and Reservoir
Porous Wick
Transport Lines
Condenser
Numerical Tools for Design Validation
Numerical Validation of the LHP Design
COnclusions
EXPERIMENTAL ANALYSIS
Introduction
Experimental Setup
Experimental Results
Conclusions
EXPERIMENTAL VS NUMERICAL
Introduction
Derivation of the Main Model Parameters Based on the Empirical Data
Results: Experimental vs Numerical
Conclusions
GENERAL CONCLUSIONS AND PERSPECTIVES |
Faire une suggestion Affiner la rechercheDesign and Experimental Analysis of a Loop Heat Pipe for Thermal Control of Aircraft Engine Equipment / Filippo PAGNONI
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