Verfügbarkeit: Coupling of tip leakage flow and blade vibration in transonic compressors

Coupling of tip leakage flow and blade vibration in transonic compressors: mechanism and countermeasures

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Bibliographische Detailangaben
1. Verfasser:	Holzinger, Felix (VerfasserIn)
Format:	Abschlussarbeit Buch
Sprache:	English
Veröffentlicht:	Aachen Shaker Verlag 2018
Schriftenreihe:	Forschungsberichte aus dem Institut für Gasturbinen, Luft- und Raumfahrtantriebe Band 9
Schlagworte:	Transsonischer Verdichter Schaufelschwingung Fluid-Struktur-Wechselwirkung Axialverdichter Aeroelastizität Blisk Acoustic resonance Aerodynamics Aeroelasticity Compressor Flutter Non-synchronous vibration Rotating instabilities Rotating stall Self-excited vibration Tip clearance vortex Tip leakage flow Transonic Flow Turbomachinery Vibration Hochschulschrift
Online-Zugang:	Inhaltsverzeichnis
Beschreibung:	XXI, 177, A54 Seiten Illustrationen, Diagramme 21 cm x 14.8 cm, 384 g
ISBN:	9783844058239 3844058230

Internformat

MARC


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245	1	0	\|a Coupling of tip leakage flow and blade vibration in transonic compressors \|b mechanism and countermeasures \|c Felix Holzinger
264		1	\|a Aachen \|b Shaker Verlag \|c 2018
300			\|a XXI, 177, A54 Seiten \|b Illustrationen, Diagramme \|c 21 cm x 14.8 cm, 384 g
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653			\|a Acoustic resonance
653			\|a Aerodynamics
653			\|a Aeroelasticity
653			\|a Blisk
653			\|a Compressor
653			\|a Flutter
653			\|a Non-synchronous vibration
653			\|a Rotating instabilities
653			\|a Rotating stall
653			\|a Self-excited vibration
653			\|a Tip clearance vortex
653			\|a Tip leakage flow
653			\|a Transonic Flow
653			\|a Turbomachinery
653			\|a Vibration
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Datensatz im Suchindex

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adam_text	TABLE OF CONTENTS NOMENCLATURE XI LIST OF FIGURES XVII LIST OF TABLES XXI 1 INTRODUCTION 1 2 PROBLEM STATEMENT 7 3 FUNDAMENTALS 11 3.1 FOREWORD TO THE FUNDAMENTALS S E C TIO N ........................................ 11 3.2 GAS TURBINE LAYOUT AND C Y C LE ....................................................... 12 3.2.1 THE GAS GENERATOR - HEART OF ANY GAS TU RB IN E .................. 12 3.2.2 MOTIVATION FOR GLOBAL DESIGN TRENDS ................................ 16 3.3 AXIAL COMPRESSORS.......................................................................... 18 3.3.1 AXIAL LA Y O U T ....................................................................... 18 3.3.2 MULTISTAGE LAYOUT ............................................................... 19 3.3.3 EULER E Q U A TIO N .................................................................. 20 3.3.4 TRANSONIC LA Y O U T ............................................................... 23 3.3.5 SECONDARY FLOW IN AXIAL COMPRESSORS................................ 26 3.3.6 3D-DESIGN OF AXIAL COMPRESSOR ROTORS ............................. 29 3.3.7 COMPRESSOR PERFORMANCE AND OPERATION .......................... 31 3.4 BLADE TIP CLEARAN CE ....................................................................... 36 3.4.1 TRANSIENT VARIATION OF THE GLOBAL TIP CLEARANCE ................. 37 3.4.2 TIP CLEARANCE VARIATIONS OF THE INDIVIDUAL BLADES ........... 39 3.5 BLADE VIBRATION ............................................................................. 42 3.5.1 INFERIOR DAMPING OF RO TO R S ................................................ 42 3.5.2 RELATION OF MEAN AND ALTERNATING STRESSES ........................ 43 3.5.3 BLADE EIGENM ODES............................................................. 45 3.5.4 CAMPBELL D IAGRAM ............................................................. 48 3.5.5 NODAL DIAMETERS AND TRAVELING W A V E S ............................. 51 3.5.6 M ISTUNING.......................................................................... 55 4 FLOW INDUCED BLADE VIBRATION 57 4.1 NEED FOR A NEW CATEGORIZATION OF FLOW INDUCED BLADE VIBRATION . 57 4.2 NOVEL CATEGORIZATION OF FLOW INDUCED BLADE V IB RA TIO N ................ 59 4.2.1 SYNCHRONOUS V IB RA TIO N ..................................................... 60 4.2.2 NON-SYNCHRONOUS VIBRATION ............................................. 61 5 TEST RIG, TEST COMPRESSOR AND TRANSIENT EXPERIMENTS 67 5.1 TU DARMSTADT TRANSONIC COMPRESSOR TEST R IG ............................. 67 5.1.1 RESEARCH BACKGROUND........................................................ 68 5.1.2 RESEARCH FA C ILITY ................................................................ 69 5.2 TRANSONIC RESEARCH COMPRESSOR V1R5S3 ..................................... 69 5.3 AERODYNAMIC PERFORMANCE INSTRUM ENTATION................................ 71 5.4 INSTRUMENTATION FOR AEROELASTIC EXPERIMENTS ................................ 72 5.4.1 ROTOR STRAIN GAUGES (S G ) .................................................. 72 5.4.2 BLADE TIP CLEARANCE / BLADE TIP TIMING (BTC/BTT) ........... 74 5.4.3 FAST RESPONSE WALL PRESSURE TRANSDUCERS (W P T ) ............. 75 5.5 INVESTIGATED CONFIGURATIONS .......................................................... 76 5.5.1 REFERENCE CLEARANCE .......................................................... 77 5.5.2 LARGE CLEARANCE .................................................................. 77 5.5.3 NON-AXISYMMETRIC CASING TRE A TM E N T ................................ 77 5.5.4 BLADE TIP CLEARANCE COMPARISON........................................ 77 5.6 ROTOR 5 BLISK WITH ONE LOCALLY DAMAGED ROTOR BLADE T I P ............. 79 5.7 TRANSIENT EXPERIM ENTS .................................................................. 80 5.7.1 EXPERIMENTAL P RO C E D U RE .................................................. 80 5.7.2 DETERMINATION OF THE TRANSIENT AERODYNAMIC PERFORMANCE 82 5.7.3 DETERMINATION OF ACTIVE BLADE MODE AND NODAL DIAMETER 82 6 EXPERIMENTAL RESULTS 85 6.1 OVERVIEW OF THE STABILITY LIM ITS..................................................... 85 6.2 IDENTIFICATION OF THE LIMITING PHENOMENA ..................................... 87 6.2.1 M2 F LU TTE R .......................................................................... 87 6.2.2 ROTATING S T A L L ..................................................................... 90 6.2.3 ROTATING INSTABILITIES .......................................................... 91 6.2.4 ML F LU TTE R .......................................................................... 94 6.2.5 NASCT RESONANCE FOLLOWED BY ROTATING S T A L L ................... 97 6.3 AEROELASTIC SENSITIVITY TO TRANSIENT BLADE TIP CLEARANCE VARIATIONS 101 6.4 COUPLING M ECHANISM ..................................................................... 105 6.4.1 ROLE OF THE TIP LEAKAGE F L O W ............................................. 105 6.4.2 TIP FLOW FLUCTUATION AND UNSTEADY BLADE FO RC E ................ 109 6.4.3 EVOLUTION OF THE TRAVELING W A V E S ..................................... 114 6.4.4 COUPLING OF AERODYNAMIC AND STRUCTURAL TRAVELING WAVES 119 6.4.5 SUMMARY OF THE COUPLING M ECHANISM ............................. 122 6.5 COUNTERM EASURES.......................................................................... 124 6.5.1 REDUCTION OF TIP FLOW UNSTEADINESS .................................. 125 6.5.2 AERODYNAMIC MISTUNING THROUGH NASCT ........................ 128 6.5.3 LIMITATIONS OF COUNTERMEASURES........................................ 130 6.6 AEROELASTIC IMPACT OF REAL GEOMETRY EFFECTS ................................ 131 6.6.1 INHOMOGENEOUS ROTOR BLADE TIP CLEARANCE........................ 131 6.6.2 LOCAL BLADE D A M A G E .......................................................... 136 6.6.3 IMPACT ON INDIVIDUAL BLADE VIBRATION AM P LITU D ES........... 138 6.7 GLOBAL ASSESSMENT OF THE EXPERIMENTAL RESULTS .......................... 143 6.7.1 CRITICAL SPEEDS RELATED TO NON-SYNCHRONOUS VIBRATION . . . 143 6.7.2 WAVE S P E E D ....................................................................... 144 6.7.3 WAVE MACH N U M B E R.......................................................... 148 6.7.4 EVALUATION.......................................................................... 151 7 CONCLUSION 153 7.1 SUM M ARY....................................................................................... 153 7.2 O UTLOOK.......................................................................................... 159 7.2.1 DEEPENING THE INSIGHT ....................................................... 159 7.2.2 EXTENDING THE SCO P E.......................................................... 160 7.3 ACKNOWLEDGEMENT ....................................................................... 162 8 APPENDIX A1 8.1 GLOBALLY AVERAGED CONCENTRATION OF GREENHOUSE GASES ................ A1 8.2 TURBOJET AND TURBOFAN T H R U S T ....................................................... A2 8.3 TURBOJET AND TURBOFAN H-S-DIAGRAMS............................................. A3 8.4 RELATION OF ADIABATIC AND POLYTROPIC COMPRESSOR EFFICIENCIES . . . A6 8.5 HISTORICAL ASPECTS CONCERNING THE STAGE PRESSURE R A TIO ................ A6 8.6 AMENDMENT TO BLADE TIP CLEARANCE................................................ A8 8.7 AMENDMENT TO FLOW INDUCED V IB RA TIO N ........................................ A LL 8.8 AMENDMENT TO CRITICAL NSV-RELATED SPEEDS .................................. A15 8.9 AMENDMENT TO AEROELASTIC INSTRUM ENTATION................................ A17 8.9.1 UNSTEADY CASING INSTRUM ENTATION ..................................... A17 8.9.2 RADIAL PRESSURE TRANSDUCER A R R A Y ..................................... A22 8.10 AMENDMENT TO AERODYNAMIC PERFORMANCE INSTRUMENTATION . . . A23 8.11 AMENDMENT TO FUTURE COM PRESSOR .......................................... A25 8.12 AMENDMENT TO EXPERIMENTAL RESULTS............................................. A26 8.12.1 LARGE CLEARANCE (LG) ....................................................... A28 8.12.2 REFERENCE CLEARANCE (RC) .................................................. A39 8.12.3 NON-AXISYMMETRIC CASING TREATMENT (NASCT) A50
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series2	Forschungsberichte aus dem Institut für Gasturbinen, Luft- und Raumfahrtantriebe
spelling	Holzinger, Felix Verfasser (DE-588)1158600410 aut Coupling of tip leakage flow and blade vibration in transonic compressors mechanism and countermeasures Felix Holzinger Aachen Shaker Verlag 2018 XXI, 177, A54 Seiten Illustrationen, Diagramme 21 cm x 14.8 cm, 384 g txt rdacontent n rdamedia nc rdacarrier Forschungsberichte aus dem Institut für Gasturbinen, Luft- und Raumfahrtantriebe Band 9 Dissertation Technische Universität Darmstadt 2017 Transsonischer Verdichter (DE-588)4409352-4 gnd rswk-swf Schaufelschwingung (DE-588)4179424-2 gnd rswk-swf Fluid-Struktur-Wechselwirkung (DE-588)4314754-9 gnd rswk-swf Axialverdichter (DE-588)4004037-9 gnd rswk-swf Aeroelastizität (DE-588)4202469-9 gnd rswk-swf Blisk (DE-588)7606328-8 gnd rswk-swf Acoustic resonance Aerodynamics Aeroelasticity Blisk Compressor Flutter Non-synchronous vibration Rotating instabilities Rotating stall Self-excited vibration Tip clearance vortex Tip leakage flow Transonic Flow Turbomachinery Vibration (DE-588)4113937-9 Hochschulschrift gnd-content Transsonischer Verdichter (DE-588)4409352-4 s Axialverdichter (DE-588)4004037-9 s Blisk (DE-588)7606328-8 s Aeroelastizität (DE-588)4202469-9 s Schaufelschwingung (DE-588)4179424-2 s Fluid-Struktur-Wechselwirkung (DE-588)4314754-9 s DE-604 Shaker Verlag (DE-588)1064118135 pbl Forschungsberichte aus dem Institut für Gasturbinen, Luft- und Raumfahrtantriebe Band 9 (DE-604)BV042674606 9 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=030393715&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis
spellingShingle	Holzinger, Felix Coupling of tip leakage flow and blade vibration in transonic compressors mechanism and countermeasures Forschungsberichte aus dem Institut für Gasturbinen, Luft- und Raumfahrtantriebe Transsonischer Verdichter (DE-588)4409352-4 gnd Schaufelschwingung (DE-588)4179424-2 gnd Fluid-Struktur-Wechselwirkung (DE-588)4314754-9 gnd Axialverdichter (DE-588)4004037-9 gnd Aeroelastizität (DE-588)4202469-9 gnd Blisk (DE-588)7606328-8 gnd
subject_GND	(DE-588)4409352-4 (DE-588)4179424-2 (DE-588)4314754-9 (DE-588)4004037-9 (DE-588)4202469-9 (DE-588)7606328-8 (DE-588)4113937-9
title	Coupling of tip leakage flow and blade vibration in transonic compressors mechanism and countermeasures
title_auth	Coupling of tip leakage flow and blade vibration in transonic compressors mechanism and countermeasures
title_exact_search	Coupling of tip leakage flow and blade vibration in transonic compressors mechanism and countermeasures
title_full	Coupling of tip leakage flow and blade vibration in transonic compressors mechanism and countermeasures Felix Holzinger
title_fullStr	Coupling of tip leakage flow and blade vibration in transonic compressors mechanism and countermeasures Felix Holzinger
title_full_unstemmed	Coupling of tip leakage flow and blade vibration in transonic compressors mechanism and countermeasures Felix Holzinger
title_short	Coupling of tip leakage flow and blade vibration in transonic compressors
title_sort	coupling of tip leakage flow and blade vibration in transonic compressors mechanism and countermeasures
title_sub	mechanism and countermeasures
topic	Transsonischer Verdichter (DE-588)4409352-4 gnd Schaufelschwingung (DE-588)4179424-2 gnd Fluid-Struktur-Wechselwirkung (DE-588)4314754-9 gnd Axialverdichter (DE-588)4004037-9 gnd Aeroelastizität (DE-588)4202469-9 gnd Blisk (DE-588)7606328-8 gnd
topic_facet	Transsonischer Verdichter Schaufelschwingung Fluid-Struktur-Wechselwirkung Axialverdichter Aeroelastizität Blisk Hochschulschrift
url	http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=030393715&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA
volume_link	(DE-604)BV042674606
work_keys_str_mv	AT holzingerfelix couplingoftipleakageflowandbladevibrationintransoniccompressorsmechanismandcountermeasures AT shakerverlag couplingoftipleakageflowandbladevibrationintransoniccompressorsmechanismandcountermeasures

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