• Aucun résultat trouvé

D.Bizzarri - PhD Thesis - 2008 iii

N/A
N/A
Protected

Academic year: 2021

Partager "D.Bizzarri - PhD Thesis - 2008 iii "

Copied!
6
0
0

Texte intégral

(1)

D.Bizzarri - PhD Thesis - 2008 iii

ABSTRACT

A compact air separator demonstrator based on centrifugally enhanced distillation has been studied. The full size device is meant to be used on board of a Two Stage To Orbit vehicle launcher. The air separation system must be able to extract oxygen in highly concentrated liquid form (LEA, Liquid Enriched Air) from atmospheric air. The LEA is stored before being used in a subsequent rocket propulsion phase by the second stage of the launcher. Two reference vehicles are defined, one with a subsonic first stage and one with a supersonic first stage. In both cases, oxygen collection is performed during a cruise phase (M 0.7 and M 2.5 respectively). The aim of the project is to demonstrate the feasibility of the air separation system, investigate the separation cycle design, and assess that the separator design selected is suitable for the reference vehicles.

The project is described from original base ideas to design, construction, extended testing and analysis of experimental results. Preliminary computations for a realistic layout have been performed and the motivations for the choices made during the process are explained. Test rig design, separator design and technical discussion are provided for a subscale pilot unit. Mass transport parameters and flooding limits have been estimated and experimentally measured. Performance has been assessed and shown to be sufficient for the reference Two Stage To Orbit vehicles. The technology developed is found suitable without further optimization, although some volume and mass reduction would be desirable for the supersonic first stage concept. There are many ways of optimisation that can be further investigated. The aim of this program, however, is not to fully optimize the device, but to demonstrate that a device based on a simple, robust, low-risk design is already suitable for the launch vehicles. On top of that analysis, directions for improvements are suggested and their potentials estimated. A complete assessment of those improvements requires further maturation of the technological concept through further testing and practical implementations.

Directions for future work, general conclusions and a vehicle development roadmap

have also been provided.

(2)

D.Bizzarri - PhD Thesis - 2008 iv

STRUCTURE OF THE DOCUMENT

The document is made of a main thesis text complemented by more detailed specific appendices. Not all appendices have been written using the same word processor for practical reasons, and the composite structure comes out of the fact that appendices given here are based on reports and notes that were part of a set of different, evolving documents that had to be maintained over time.

A detailed Table of Contents is given at the beginning of the main text and each Appendix with the exception of Appendix D.

LIST OF APPENDICES

APPENDIX A: TECHNICAL DESCRIPTION OF THE TEST CELL AND ITS SPINDLE

APPENDIX B: SEPARATOR AND CYCLE STUDIES AND ESTIMATIONS

APPENDIX C: PREVIOUS WORK PERFORMED RELATED TO THE PROJECT

APPENDIX D: THERMO-CHEMICAL PROPERTIES OF OXYGEN AND NITROGEN

APPENDIX E: FLOODING, PRESSURE DROP AND MASS EXCHANGE IN A CENTRIFUGAL DISTILLATION COLLUMN

APPENDIX F: DESIGNING FOR OPERATION UNDER OXYGEN ENRICHED ATMOSPHERE

APPENDIX G: EXPERIMENTAL SET-UP APPENDIX G.1: INSTRUMENTATION

APPENDIX G.2: OXYGEN SEPARATION ANALYSIS

APPENDIX G.3: PRESSURE DROP ANALYSIS INSIDE THE SEPARATOR

(3)

D.Bizzarri - PhD Thesis - 2008 v

TABLE OF CONTENTS

1. INTRODUCTION ... 1

1.1. WHY COLLECTING OXYGEN DURING FLIGHT... 2

1.2. THE CONCEPTUAL AND EXPERIMENTAL STUDIES ... 4

1.3. INHERITAGE FROM PREVIOUS EUROPEAN RESEARCH AND THE VORTEX SEPARATOR... 6

1.4. THE REFERENCE CONCEPT AND THE REFERENCE VEHICLES... 8

1.5. THE NEED FOR DESIGN WORK AND EXPERIMENTAL RESULTS... 13

1.6. PROJECT RATIONALE... 14

2. OVERVIEW OF THE RDS DEVELOPMENT... 15

2.1. CHOICE OF THE SEPARATION PRINCIPLE... 15

2.2. FIRST SKETCH ... 16

2.3. THE DESIGN PROCESS IN EXPERIMENTAL WORK ... 18

2.4. DEEP COOLING FACILITY... 18

2.4.1. AVAILABLE FACILITY ... 19

2.4.2. ORIGINAL PROPOSAL... 19

2.4.3. FINAL SELECTED OPTION... 20

2.4.4. HEAT EXCHANGERS ... 20

2.5. FIRST ISSUE: SEPARATOR ARRANGEMENT... 21

2.5.1. MASS EXCHANGER CONCEPT: LIMITING LAYOUT COMPLEXITY, PROVIDING TESTING STRATEGY, ENHANCING MODULARITY ... 21

2.5.2. ACCOMMODATING AND FEEDING THE SEPARATION MEDIUM ... 23

2.5.3. RELATION TO A REAL SEPARATION SYSTEM ... 24

2.6. CORE SEPARATOR DESIGN ... 27

2.6.1. ARRANGING COUNTERFLOWS AND MASS TRANSPORT... 27

2.6.2. CORE MANUFACTURING... 36

2.6.3. SELECTED SEPARATION MEDIUM CHARACTERISTICS ... 40

2.6.4. REFERENCE CONDITIONS... 41

2.7. SKETCH OF THE SEPARATION UNIT... 43

3. THEORETICAL PROCESS STUDIES ... 45

3.1. A PREREQUISITE: COLLECTION OF THERMO-PHYSICAL DATA FOR THE WORKING FLUID... 45

3.2. ANALYSIS TOOLS AND MODELS: MASS EXCHANGE MODELS ... 48

3.2.1. EQUILIBRIUM STAGE APPROXIMATION (McCabe and Thiele Method, ETP model) ... 48

3.2.2. CONTINUOUS NTU MODEL... 51

3.2.3. TAKING FLOW SECTION VARIATION INTO ACCOUNT... 55

3.2.4. RELATING NTU and NETP ... 57

3.2.5. RELATION BETWEEN MASS EXCHANGER AND COMPLETE SEPARATION SYSTEM ... 58

3.3. STUDIES OF COMPLETE SEPARATION SYSTEMS... 58

3.3.1. PREVIOUS WORK: USE OF THE DOUBLE PRESSURE COLUMN LAYOUT58 3.3.2. THE HALF COLUMN LAYOUT, A RADICAL OPTION ... 62

3.3.3. IMPROVEMENTS OF THE COLLECTION RATIO... 66

3.3.4. THE COMPLETE COLUMN LAYOUT... 67

3.3.5. RESULTS OF DETAILED CYCLE STUDY... 69

3.3.6. PARAMETRIC STUDY, A SIMPLIFIED MODEL... 70

3.3.7. CONCLUSION ... 72

(4)

D.Bizzarri - PhD Thesis - 2008 vi 4. FLOODING, PRESSURE DROP AND MASS EXCHANGE IN A

CENTRIFUGAL DISTILLATION COLUMN: ESTIMATION OF

PARAMETERS ... 74

4.1. INTRODUCTION... 74

4.2. REFERENCE CONDITIONS USED FOR ESTIMATIONS ... 74

4.3. METAL FOAM CHARACTERIZATION... 74

4.4. SOME PREREQUISITE ... 75

4.4.1. Substitutes for the Specific Surface parameter ... 76

4.4.2. Gas Velocity in Porous Media... 76

4.5. F LOODING ... 77

4.5.1. Semi-empirical correlation from non-rotating systems ... 77

4.5.2. Data from rotating systems ... 81

4.5.3. Critical Assessment of Flooding Regressions for Random Packings ... 84

4.5.4. Comparison Chart (water-air system) ... 85

4.5.5. Flooding Prediction ... 87

4.6. P RESSURE D ROP ... 92

4.6.1. Viscous pressure drop ... 92

4.6.2. Centrifugal Pressure Drop... 95

4.6.3. Viscous Pressure Drop with Flooding... 95

4.6.4. Pressure Drop estimate... 96

4.6.5. Scaling Rule for Pressure Drop Decomposition (viscous+centrifugal) ... 96

4.7. L IQUID M ALDISTRIBUTION AND E FFECTIVE S PECIFIC A REA ... 97

4.7.1. Flow Visualization in a Rotating Contactor ... 97

4.7.2. Conclusion from Flow Visualization Data ... 98

4.7.3. Estimating Effective Surface of Liquid-Gas Interface... 99

4.7.4. Effect of Centrifugal Acceleration on Effective Surface ... 100

4.7.5. Conclusion on Effect of Centrifugal Acceleration on Effective Surface... 100

4.8. L IQUID S IDE M ASS TRANSPORT ... 101

4.9. M ASS T RANSPORT ... 102

4.9.1. Experimental Data ... 104

4.9.2. Phenomenological Considerations ... 104

4.9.3. Effect of Flow Maldistribution... 104

4.9.4. Reviewing Some Available Correlations... 105

4.9.5. Theoretical or Semi-Empirical Relations and Limit Cases ... 105

4.9.6. Using Distillation Correlations... 108

4.9.7. Using Heat Transfer Rate Analogy ... 108

4.9.8. Using Mass Transfer Correlations for Packed Beds ... 111

4.9.9. Comparison of All Correlations ... 112

4.10. A XIAL D ISPERSION ... 118

4.11. CONCLUSION ... 119

5. EXPERIMENTAL FACILITY: DEEP COOLING AND LIQUEFACTION120 5.1. OVERVIEW ... 120

5.2. SPECIFICATIONS OF THE SEPARATOR... 120

5.3. DEEP COOLING AND LIQUEFACTION PLANT ... 122

5.3.1. OVERVIEW ... 122

5.3.2. LN

2

TANK AND LN

2

CIRCUIT ... 123

5.3.3. AIR CIRCUIT ... 125

5.3.4. HEAT EXCHANGERS ... 125

5.3.5. DEEP COOLING AND CONDENSING ATMOSPHERIC AIR: some preliminary testing ... 128

6. EXPERIMENTAL SET-UP... 131

6.1. HARDWARE AND DETAILED FLOWSHEETS ... 131

6.1.1. OVERVIEW ... 131

6.1.2. TEST CELL DETAILS ... 134

6.1.3. INTEGRATION OF THE SEPARATOR BED... 135

(5)

D.Bizzarri - PhD Thesis - 2008 vii

6.1.4. SEPARATOR BED HOLDER-ROTOR ... 138

6.1.5. INJECTION SYSTEM... 139

6.1.6. THE TEST CELL AND ITS PERIPHERALS... 140

6.1.7. CONCENTRATION MEASUREMENTS AND SAMPLE ANALYSIS... 143

6.2. TEST RIG CONTROL... 145

6.2.1. FLOW CONTROL AND PRESSURE CONTROL ... 145

6.2.2. CONTROL OF LIQUID DISPOSAL... 145

6.2.3. MACHINE OPERATION AND COOL DOWN PROCEDURE... 147

7. EXPERIMENTAL RESULTS... 149

7.1. OPERATIONAL EXPERIENCE ... 149

7.2. OVERVIEW OF RUNS PERFORMED ... 149

7.3. PRELIMINARY SEPARATION RESULTS ... 153

7.3.1. FIRST TESTS SIMULATING CLOSE-TO-FLIGHT CONDITIONS... 153

7.3.2. SIMULATING CLOSE-TO-FLIGHT CONDITIONS WITH INCREASED THROUGHPUT ... 157

7.4. COMPLETE SEPARATION ANALYSIS... 158

7.4.1. APPLICATION OF THE CONTINUOUS MODEL ... 158

7.4.2. SUMMARY AND DISCUSSION OF SEPARATION ANALYSIS ... 161

7.5. HIGH FLOW OPERATION AND PRESSURE DROP ANALYSIS ... 163

7.5.1. HIGHER THROUGHPUT CONDITIONS... 163

7.5.2. PRESSURE DROP ANALYSIS... 163

8. ASSESSMENT OF EXPERIMENTAL RESULTS ... 167

8.1. SIZING THE SEPARATOR UNITS ... 167

8.1.1. A MODULAR DESIGN... 167

8.1.2. MAXIMUM THROUGHPUT ... 168

8.1.3. RADIAL DEPTH OF A PACKING EQUIVALENT TO A THEORETICAL PLATE ... 169

8.1.4. SUBSONIC CASE ... 171

8.1.5. SUPERSONIC CASE ... 172

8.1.6. CONCLUSION FROM SIZING EXERCISE... 175

8.2. COMPARISON WITH PREVIOUS EXPERIMENTS ... 175

8.3. POTENTIAL IMPROVEMENTS ... 178

8.3.1. Compacity trend, parametric study ... 178

8.3.2. Predicting potential compacity improvements ... 180

9. RECOMMENDATIONS AND FUTURE WORK... 182

9.1. MEASUREMENTS - EXPERIMENTATION... 182

9.1.1. FOAM CHARACTERISATION- Scientific investigation ... 182

9.1.2. 4.1.2. INVESTIGATION ON LIMITING FLOW, SEPARATION and HYDRODYNAMICS ... 183

9.2. ANALYSIS AND STUDY WORK ... 184

9.3. CONSTRUCTION OF OTHER DEMONSTRATORS... 185

10. GENERAL CONCLUSIONS... 186

11. LIST OF ABBREVIATIONS AND VARIABLES... 190

11.1. ABBREVIATION LIST... 190

11.2. TABLE OF VARIABLES ... 191

11.3. DIMENSIONLESS GROUPS ... 193

11.4. RELATED TO SEPARATOR SPECIFICATIONS ... 195

11.5. INDICES... 195

11.6. OTHER CONVENTIONS... 195

12. TEST MEASUREMENTS AND RESULTS REFERENCE... 196

12.1. TABULATION OF TEST CONDITIONS... 196

12.2. SUMMARY OF NTU ANALYSIS ... 207

(6)

D.Bizzarri - PhD Thesis - 2008 viii 12.3. COMPARISON OF DISTILLATION CALCULATIONS AND

MEASUREMENTS ... 208

12.4. SUMMARY OF SEPARATION RESULTS... 209

13. REFERENCES AND BIBLIOGRAPHY ... 210

13.1. ESA NOTES AND REPORTS ... 210

13.2. GENERAL... 210

13.3. TRANSPORT UNIT CONCEPT SEMINAL ARTICLE... 215

13.4. OXYGEN COMPATIBILITY REFERENCES... 215

13.5. STANDARDS AND RECOGNIZED GUIDELINES ... 216

13.6. SAFETY GIDELINES, SAFETY RELATED ( EXCL . O2 COMPATIBILITY )... 216

13.7. DISTILLATION AND SEPARATION ... 216

13.8. MASS TRANSPORT... 217

13.9. MASS TRANSPORT AND FLOODING ... 218

13.10. HUGHMARK ( HEAT AND MASS TRANFER AND FLOODING ) ... 218

13.11. CELLULAR MATERIALS ((METAL OR CERAMIC) ) ... 218

13.12. PACKING (MATHEMATICAL)... 219

13.13. PATENT BIBLIOGRAPHY ... 219

13.14. BIBLIOGRAPHY FROM PROF. CRINE AND STAFF ... 220

14. CREDITS AND ACKNOWLEDGEMENTS ... 223

Références

Documents relatifs

But I disagree with him that this norm is more basic than the norm of knowledge (2001: 289- 90) 15 The objection is well formulated by David 2001: “Although knowledge is certainly

However, this value was determined for the following working parameters: velocity at the inlet – 1.18 m/s, gauge pressure at the inlet and outlet – 0.4 MPa, discrete phase

The thesis requires competence in existing building blocks, namely, IEEE 802.15.4 PHY and MAC layers, routing protocols for wireless sensor networks, open software such as

Among these, only 74 cases reported concomitant treatment with antipsychotics (aripiprazole, olanzapine, quetiapine, risperidone and/or ziprasidone) which are known to cause

The signals in this Newsletter are based on information derived from reports of suspected adverse drug reactions available in the WHO global database of individual case safety

Those physiological loadings served as basis to define boundary conditions for Finite Element (FE) analysis and for experimental testing in order to get closer

I It can be chosen such that the components with variance λ α greater than the mean variance (by variable) are kept. In normalized PCA, the mean variance is 1. This is the Kaiser

We advocate a design methodology including high level specifications using the modularity and reusability features of the S IGNAL programming; formal verification and per-