Tài liệu hạn chế xem trước, để xem đầy đủ mời bạn chọn Tải xuống
1
/ 353 trang
THÔNG TIN TÀI LIỆU
Thông tin cơ bản
Định dạng
Số trang
353
Dung lượng
3,21 MB
Nội dung
Fluid Mechanics,
Thermodynamics of
Turbomachinery
S.L. Dixon, B.Eng., PH.D.
Senior Fellow at the University of Liverpool
FOURTH EDITION in SI/METRIC UNITS
Fluid Mechanics,
Thermodynamics of
Turbomachinery
FOURTH EDITION in SI/METRIC UNITS
In memory of
Avril and baby Paul
Fluid Mechanics,
Thermodynamics of
Turbomachinery
S. L. Dixon, B.Eng., Ph.D.
Senior Fellow at the University of Liverpool
FOURTH EDITION in SI/METRIC UNITS
Butterworth-Heinemann
Linacre House, Jordan Hill, Oxford OX2 8DP
225 Wildwood Avenue, Woburn, MA 01801-2041
A division of Reed Educational and Professional Publishing Ltd
A member of the Reed Elsevier plc group
First published by Pergamon Press Ltd 1966
Second edition 1975
Third edition 1978
Reprinted 1979, 1982 (twice), 1984, 1986, 1989, 1992, 1995
Fourth edition 1998
S.L. Dixon 1978, 1998
All rights reserved. No part of this publication
may be reproduced in any material form (including
photocopying or storing in any medium by electronic
means and whether or not transiently or incidentally
to some other use of this publication) without the
written permission of the copyright holder except
in accordance with the provisions of the Copyright,
Designs and Patents Act 1988 or under the terms of a
license issued by the Copyright Licensing Agency Ltd,
90 Tottenham Court Road, London, England W1P 9HE.
Applications for the copyright holder’s written permission
to reproduce any part of this publication should be addressed
to the publishers
British Library Cataloguing in Publication Data
A catalogue record for this book is available from the British Library
ISBN 0 7506 7059 2
Library of Congress Cataloguing in Publication Data
A catalogue record for this book is available from the Library of Congress
Typeset by Laser Words, Madras, India
Printed and bound in
Contents
PREFACE TO FOURTH EDITION ix
P
REFACE TO THIRD EDITION xi
A
CKNOWLEDGEMENTS xiii
L
IST OF SYMBOLS xv
1. Introduction: Dimensional Analysis: Similitude
1
Definition of a turbomachine 1
Units and dimensions 3
Dimensional analysis and performance laws 4
Incompressible fluid analysis 6
Performance characteristics 7
Variable geometry turbomachines 9
Specific speed 10
Cavitation 12
Compressible gas flow relations 15
Compressible fluid analysis 16
The inherent unsteadiness of the flow within turbomachines 20
References 21
Problems 22
2. Basic Thermodynamics, Fluid Mechanics: Definitions of Efficiency 23
Introduction 23
The equation of continuity 23
The first law of thermodynamics
internal energy 24
The momentum equation
Newton’s second law of motion 25
The second law of thermodynamics
entropy 29
Definitions of efficiency 30
Small stage or polytropic efficiency 35
Nozzle efficiency 41
Diffusers 43
References 53
Problems 53
vi
Contents
3. Two-dimensional Cascades 55
Introduction 55
Cascade nomenclature 56
Analysis of cascade forces 57
Energy losses 59
Lift and drag 59
Circulation and lift 61
Efficiency of a compressor cascade 62
Performance of two-dimensional cascades 63
The cascade wind tunnel 63
Cascade test results 65
Compressor cascade performance 68
Turbine cascade performance 70
Compressor cascade correlations 71
Fan blade design (McKenzie) 80
Turbine cascade correlation (Ainley) 81
Comparison of the profile loss in a cascade and in a turbine stage 86
Optimum space-chord ratio of turbine blades (Zweifel) 87
References 88
Problems 90
4. Axial-flow Turbines: Two-dimensional Theory 93
Introduction 93
Velocity diagrams of the axial turbine stage 93
Thermodynamics of the axial turbine stage 94
Stage losses and efficiency 96
Soderberg’s correlation 97
Types of axial turbine design 99
Stage reaction 101
Diffusion within blade rows 103
Choice of reaction and effect on efficiency 107
Design point efficiency of a turbine stage 108
Maximum total-to-static efficiency of a reversible turbine stage 112
Stresses in turbine rotor blades 114
Turbine flow characteristics 120
Flow characteristics of a multistage turbine 122
The Wells turbine 124
References 132
Problems 133
5. Axial-flow Compressors and Fans 137
Introduction 137
Two-dimensional analysis of the compressor stage 138
Velocity diagrams of the compressor stage 140
Thermodynamics of the compressor stage 141
Contents
vii
Stage loss relationships and efficiency 142
Reaction ratio 143
Choice of reaction 143
Stage loading 144
Simplified off-design performance 145
Stage pressure rise 147
Pressure ratio of a multistage compressor 148
Estimation of compressor stage efficiency 149
Stall and surge phenomena in compressors 154
Control of flow instabilities 159
Axial-flow ducted fans 160
Blade element theory 162
Blade element efficiency 163
Lift coefficient of a fan aerofoil 164
References 165
Problems 166
6. Three-dimensional Flows in Axial Turbomachines 169
Introduction 169
Theory of radial equilibrium 169
The indirect problem 171
The direct problem 179
Compressible flow through a fixed blade row 180
Constant specific mass flow 181
Off-design performance of a stage 183
Free-vortex turbine stage 184
Actuator disc approach 186
Blade row interaction effects 190
Computer-aided methods of solving the through-flow problem 191
Secondary flows 193
References 195
Problems 196
7. Centrifugal Pumps, Fans and Compressors 199
Introduction 199
Some definitions 200
Theoretical analysis of a centrifugal compressor 202
Inlet casing 203
Impeller 203
Conservation of rothalpy 204
Diffuser 205
Inlet velocity limitations 205
Optimum design of a pump inlet 206
Optimum design of a centrifugal compressor inlet 208
Slip factor 213
Head increase of a centrifugal pump 218
viii
Contents
Performance of centrifugal compressors 219
The diffuser system 227
Choking in a compressor stage 230
References 232
Problems 233
8. Radial Flow Gas Turbines 236
Introduction 236
Types of inward flow radial turbine 237
Thermodynamics of the 90 deg IFR turbine 239
Basic design of the rotor 241
Nominal design point efficiency 242
Mach number relations 246
Loss coefficients in 90 deg IFR turbines 247
Optimum efficiency considerations 248
Criterion for minimum number of blades 253
Design considerations for rotor exit 256
Incidence losses 260
Significance and application of specific speed 263
Optimum design selection of 90 deg IFR turbines 266
Clearance and windage losses 269
Pressure ratio limits of the 90 deg IFR turbine 269
Cooled 90 deg IFR turbines 271
References 272
Problems 273
9. Hydraulic Turbines 277
Introduction 277
Hydraulic turbines 278
The Pelton turbine 281
Reaction turbines 290
The Francis turbine 290
The Kaplan turbine 296
Effect of size on turbomachine efficiency 299
Cavitation 301
References 305
Problems 306
Bibliography 309
Appendix 1. Conversion of British and US Units to SI Units 310
Appendix 2. Answers to Problems 311
Index 315
Preface to the Fourth Edition
It is now twenty years since the third edition of this book was published and in
that period many advances have been made to the art and science of turboma-
chinery design. Knowledge of the flow processes within turbomachines has increased
dramatically resulting in the appearance of new and innovative designs. Some of
the long-standing, apparently intractable, problems such as surge and rotating stall
have begun to yield to new methods of control. New types of flow machine have
made their appearance (e.g. the Wells turbine and the axi-fuge compressor) and
some changes have been made to established design procedures. Much attention
is now being given to blade and flow passage design using computational fluid
dynamics (CFD) and this must eventually bring forth further design and flow effi-
ciency improvements. However, the fundamentals do not change and this book is
still concerned with the basics of the subject as well as looking at new ideas.
The book was originally perceived as a text for students taking an Honours degree
in engineering which included turbomachines as well as assisting those undertaking
more advanced postgraduate courses in the subject. The book was written for engi-
neers rather than mathematicians. Much stress is laid on physical concepts rather
than mathematics and the use of specialised mathematical techniques is mostly kept
to a minimum. The book should continue to be of use to engineers in industry
and technological establishments, especially as brief reviews are included on many
important aspects ofturbomachinery giving pointers to more advanced sources of
information. For those looking towards the wider reaches of the subject area some
interesting reading is contained in the bibliography. It might be of interest to know
that the third edition was published in four languages.
A fairly large number of additions and extensions have been included in the
book from the new material mentioned as well as “tidying up” various sections
no longer to my liking. Additions include some details of a new method of fan
blade design, the determination of the design point efficiency of a turbine stage,
sections on centrifugal stresses in turbine blades and blade cooling, control of flow
instabilities in axial-flow compressors, design of the Wells turbine, consideration of
rothalpy conservation in impellers (and rotors), defining and calculating the optimum
efficiency of inward flow turbines and comparison with the nominal design. A
number of extensions of existing topics have been included such as updating and
extending the treatment and application of diffuser research, effect of prerotation
of the flow in centrifugal compressors and the use of backward swept vanes on
their performance, also changes in the design philosophy concerning the blading of
axial-flow compressors. The original chapter on radial flow turbines has been split
into two chapters; one dealing with radial gas turbines with some new extensions
and the other on hydraulic turbines. In a world striving for a ‘greener’ future it was
felt that there would now be more than just a little interest in hydraulic turbines. It
is a subject that is usually included in many mechanical engineering courses. This
chapter includes a few new ideas which could be of some interest.
[...]... section of this chapter concerned with specific speed Turbomachines are further categorised according to the nature of the flow path through the passages of the rotor When the path of the through-flow is wholly or mainly parallel to the axis of rotation, the device is termed an axial flow turbomachine (e.g 1 2 Fluid Mechanics, ThermodynamicsofTurbomachinery FIG 1.1 Diagrammatic form of various types of turbomachine... defined above, is at the point of maximum efficiency of a turbomachine, it becomes a parameter of great importance in selecting the type of machine required for a given duty The maximum efficiency condition replaces the condition of geometric similarity, so that any alteration in specific 12 FluidMechanics,ThermodynamicsofTurbomachinery FIG 1.7 Range of pump impellers of equal inlet area speed implies... mechanics and thermodynamics are the metre (m), kilogram (kg), second (s) and thermodynamic temperature (K) All the other units used in this book are derived from these basic units The unit of force is the 4 FluidMechanics,ThermodynamicsofTurbomachinery newton (N), defined as that force which, when applied to a mass of 1 kilogram, gives an acceleration to the mass of 1 m/s2 The recommended unit of pressure... University of Liverpool for his encouragement of the idea of a fourth edition of this book as well as providing papers and suggestions for some new items to be included Professor F A Lyman of Syracuse University, New York and Professor J Moore of Virginia Polytechnic Institute and State University, Virginia, for their helpful correspondence and ideas concerning the vexed question of the conservation of rothalpy... considered as a control volume 6 Fluid Mechanics, ThermodynamicsofTurbomachinery variables on the performance must now be included The size of machine is characterised by the impeller diameter D, and the shape can be expressed by a number of length ratios, l1 /D, l2 /D, etc Incompressible fluid analysis The performance of a turbomachine can now be expressed in terms of the control variables, geometric... occurring simulataneously in the fluid The definition of a turbomachine as stated above, is rather too general for the purposes of this book as it embraces open turbomachines such as propellers, wind turbines and unshrouded fans, all of which influence the state of a not readily quantifiable flow of a fluid The subject fluid mechanics,thermodynamicsof turbomachinery, therefore, is limited to machines enclosed... pressures in excess of the vapour pressure Vapour cavitation requires the presence of nuclei submicroscopic gas bubbles or solid non-wetted 14 Fluid Mechanics, ThermodynamicsofTurbomachinery particles in sufficient numbers It is an interesting fact that in the absence of such nuclei a liquid can withstand negative pressures (i.e tensile stresses)! Perhaps the earliest demonstration of this phenomenon... examples In SI the units of all forms of energy are the same as for work The unit of energy is the joule (J) which is the work done when a force of 1 newton is displaced through 1 a distance of 1 metre in the direction of the force, e.g kinetic energy ( 2 mc2 ) has the 2 2 2 dimensions kg ð m /s ; however, 1 kg D 1 N s /m from the definition of the newton given above Hence, the units of kinetic energy must... unit of power; when 1 watt is applied for 1 second to a system the input of energy to that system is 1 joule (i.e 1 J) The hertz (Hz) is the number of repetitions of a regular occurrence in 1 second Instead of writing c/s for cycles/sec, Hz is used instead The unit of thermodynamic temperature is the kelvin (K), written without the ° sign, and is the fraction 1/273.16 of the thermodynamic temperature of. .. angle constants nozzle velocity coefficient lift force, length of diffuser wall blade chord length, pipe length Mach number mass, molecular ‘weight’ rotational speed, axial length of diffuser specific speed (rev) power specific speed (rev) suction specific speed (rev) number of stages, polytropic index pressure xvi Fluid Mechanics, ThermodynamicsofTurbomachinery pa pv Q q R Re RH Ro r S s T t U u V, v W W . UNITS
Fluid Mechanics,
Thermodynamics of
Turbomachinery
FOURTH EDITION in SI/METRIC UNITS
In memory of
Avril and baby Paul
Fluid Mechanics,
Thermodynamics of
Turbomachinery
S Fluid Mechanics,
Thermodynamics of
Turbomachinery
S.L. Dixon, B.Eng., PH.D.
Senior Fellow at the University of Liverpool
FOURTH EDITION