CHAPTER 12 Turbomachinery

Similar documents
CIVE HYDRAULIC ENGINEERING PART II Pierre Julien Colorado State University

Introduction to Fluid Machines (Lectures 49 to 53)

Chapter Four Hydraulic Machines

Chapter Four Hydraulic Machines

Conservation of Angular Momentum

( 4. AP Exam Practice Questions for Chapter 7. AP Exam Practice Questions for Chapter 7 1 = = x dx. 1 3x So, the answer is A.

Dr. S. Ramachandran Prof. R. Devaraj. Mr. YVS. Karthick AIR WALK PUBLICATIONS

3 Energy Exchange in Turbomachines

CHAPTER 1 Basic Considerations

CHAPTER 4 The Integral Forms of the Fundamental Laws

Centrifugal Machines Table of Contents

Department of Civil and Environmental Engineering CVNG 1001: Mechanics of Fluids

CHAPTER EIGHT P U M P I N G O F L I Q U I D S

Chapter 7 The Energy Equation

TOTAL HEAD, N.P.S.H. AND OTHER CALCULATION EXAMPLES Jacques Chaurette p. eng., June 2003

CHAPTER 2 Limits and Their Properties

Department of Energy Fundamentals Handbook. THERMODYNAMICS, HEAT TRANSFER, AND FLUID FLOW, Module 3 Fluid Flow

Problem 1.6 Make a guess at the order of magnitude of the mass (e.g., 0.01, 0.1, 1.0, 10, 100, or 1000 lbm or kg) of standard air that is in a room 10

Chapter Four fluid flow mass, energy, Bernoulli and momentum

Homework 6. Solution 1. r ( V jet sin( θ) + ω r) ( ρ Q r) Vjet

Theory of turbo machine Effect of Blade Configuration on Characteristics of Centrifugal machines. Unit 2 (Potters & Wiggert Sec

Hydraulic Turbines. Table 6.1 Parameters of hydraulic turbines. Power P (kw) Speed N (rpm)

SUMMER 14 EXAMINATION

ENERGY TRANSFER BETWEEN FLUID AND ROTOR. Dr. Ir. Harinaldi, M.Eng Mechanical Engineering Department Faculty of Engineering University of Indonesia

Fluid Statics, Hydrodynamics and Hydraulic Machines

Applied Fluid Mechanics

BME-A PREVIOUS YEAR QUESTIONS

CE 6403 APPLIED HYDRAULIC ENGINEERING UNIT - V PUMPS

where = rate of change of total energy of the system, = rate of heat added to the system, = rate of work done by the system

16.2 Line Integrals. location should be approximately 0 01 V(2 1) = 0 01 h4 3i = h i, so the particle should be approximately at the

MASS, MOMENTUM, AND ENERGY EQUATIONS

mywbut.com Hydraulic Turbines

CHAPTER 1 Basic Considerations

PROPERTIES OF FLUIDS

Fluid Mechanics Answer Key of Objective & Conventional Questions

Contents. 2 Basic Components Aerofoils Force Generation Performance Parameters xvii

Institute of Aeronautical Engineering

M E 320 Professor John M. Cimbala Lecture 24

ACCOUNTING FOR FRICTION IN THE BERNOULLI EQUATION FOR FLOW THROUGH PIPES

IJREAS Volume 2, Issue 2 (February 2012) ISSN:

CHAPTER TWO CENTRIFUGAL PUMPS 2.1 Energy Transfer In Turbo Machines

Chapter 7. Introduction to Fluid Machinery

WATER DISTRIBUTION NETWORKS

ME3560 Tentative Schedule Spring 2019

Lecture 3: Electrical Power and Energy

HYDRAULIC TURBINES. Hydraulics and Hydraulic Machines

ME3560 Tentative Schedule Fall 2018

Northern Lesson 2 Gear Pump Terminology. Gear Pump 101. Lesson 2: Gear Pump Terminology. When your reputation depends on it!

Attempt ALL QUESTIONS IN SECTION A and ANY TWO QUESTIONS IN SECTION B Linear graph paper will be provided.

Chapter 4. Turbomachinery. 4.1 Introduction. 4.2 Pumps

BASIC EQUATION. Rotational speed = = ABC 60

Introduction to Fluid Machines, and Compressible Flow Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur

ME 316: Thermofluids Laboratory

Chapter 2 SOLUTION 100 = km = h. = h. ft s

4 Mechanics of Fluids (I)

Only if handing in. Name: Student No.: Page 2 of 7

!! +! 2!! +!"!! =!! +! 2!! +!"!! +!!"!"!"

ME 201 Thermodynamics

CLASS Fourth Units (Second part)

FE Exam Fluids Review October 23, Important Concepts

Unit 8 Problem Solutions

9. Pumps (compressors & turbines) Partly based on Chapter 10 of the De Nevers textbook.

Two mark questions and answers UNIT I BASIC CONCEPT AND FIRST LAW SVCET

CENTRIFUGAL PUMP SELECTION, SIZING, AND INTERPRETATION OF PERFORMANCE CURVES

TECHNICAL INFORMATION Bulletin

OPEN CHANNELS (OPEN CHANNEL FLOW AND HYDRAULIC MACHINERY)

In the next lecture...

Chapter (6) Energy Equation and Its Applications

98-Mar-BS FLUID MACHINERY

2 cos sin 2 2. cos sin 2 cos 1 sin 2. .But = ( ),and = + = ( ) ( ) ( ) 2. [by the equality of mixed partials] = ± ( ) ( ).

9.1. Click here for answers. Click here for solutions. PARAMETRIC CURVES

Download Solution Manual for Thermodynamics for Engineers 1st Edition by Kroos and Potter

NOT FOR SALE 6 APPLICATIONS OF INTEGRATION. 6.1 Areas Between Curves. Cengage Learning. All Rights Reserved. ( ) = 4 ln 1 = 45.

HYDRAULICS AND HYDRAULIC MACHINES LABORATORY

CVE 372 HYDROMECHANICS EXERCISE PROBLEMS

CALIFORNIA POLYTECHNIC STATE UNIVERSITY Mechanical Engineering Department ME 347, Fluid Mechanics II, Winter 2018

Objectives. Conservation of mass principle: Mass Equation The Bernoulli equation Conservation of energy principle: Energy equation

AEROSPACE ENGINEERING DEPARTMENT. Second Year - Second Term ( ) Fluid Mechanics & Gas Dynamics

ENGINEERING FLUID MECHANICS. CHAPTER 1 Properties of Fluids

SKM DRILLING ENGINEERING. Chapter 3 - Drilling Hydraulics

NATIONAL EXAMINATIONS. May MEC-AG-1 FLUID MACHINERY. Three hours duration. Notes to Candidates

CHAPTER 2 Fluid Statics

nozzle which is fitted to a pipe through which the liquid is flowing under pressure.

Rate of Flow Quantity of fluid passing through any section (area) per unit time

PUMP PERFORMANCE MEASUREMENTS Jacques Chaurette p. eng. April 2003

1) Specific Gravity It is the ratio of specific weight of fluid to the specific weight of water.

Centrifugal Pumps. Problem 1. This is a small project having three parts: Parts (a), (b), and (c).

Attempt ALL QUESTIONS IN SECTION A and ANY TWO QUESTIONS IN SECTION B Linear graph paper will be provided.

P U M P S. The quality standard for hydraulic efficiency and suction lift. PERIPHERAL PUMPS TEP/ TSP - SERIES 50Hz

THERMODYNAMICS, FLUID AND PLANT PROCESSES. The tutorials are drawn from other subjects so the solutions are identified by the appropriate tutorial.

1 st Law Analysis of Control Volume (open system) Chapter 6

Fluid Dynamics Midterm Exam #2 November 10, 2008, 7:00-8:40 pm in CE 110

Therefore, the control volume in this case can be treated as a solid body, with a net force or thrust of. bm # V

Pressure and Flow Characteristics

Fachgesprach 12. HVAC Pumps. For Project Managers

Mechanical Engineering Programme of Study

To investigate the performance of the Pelton Wheel turbine with different range of flow rates and rotational speeds.

BASIC EQUATION. Rotational speed. u = linear velocity in m/s r = radius in m ω = angular velocity in rad/s D = diameter in m N = rotation per minute

Following are the results of four drained direct shear tests on an overconsolidated clay: Diameter of specimen 50 mm Height of specimen 25 mm

Signature: (Note that unsigned exams will be given a score of zero.)

Transcription:

CAER urbomachinery Chapter / urbomachinery 800 / 0 8 8 rad /s, u r 8 8 0 0 m /s, u r 8 8 0 0 8 m /s, rbv, but V u since, n n 0 0 0 0 0 0 m / s V V 0 0 m /s, rb 0 0 0 Vn u 0 8 6 77 m /s, tan tan 0 n t V t 0 ( 90 under ideal conditions) r V rv t t 000 0 0( 0 6 77 0) 6 N m W 88 6 980 W, t / 980 /( 980 0 0 ) 7 m ft gal / sec 0 67 ft / sec, 000 09 rad /sec, 7 8 gal 0 0 67 Vn 6 ft /sec, r b 0 u r 09 / ft/sec, u g u V t ( n cot ) ( 6 cot 60 ) ft W t 6 0 8 0 67 7 ft - lb /sec, or W 7/ 0 horsepower 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part

Chapter / urbomachinery 6 Compute loss in suction pipe: h f L K L ga 0 0 0 0 0 9 0 8 8 m 0 9 8 0 Water at 0 C: 979 N/m, p 0 a v Substitute known data into NS relation, solving for z: z p atm p v h L NS 0 0 0 8 m 979 8 N N 970 00 0 8 0 6 m / s, from Fig 9, m and W 9 kw 00 7 6 m, 970 00 W W 9 7 kw 970 0 / 600 C 0 00 06 0 ( in m /h) g 98 C 0 00 6 0 ( in m) abulate C and C using selected values of and from Fig 6: (m /h) C 0 (m) C 0 0 0 6 0 0 00 06 0 9 0 6 00 7 9 0 6 0 00 8 08 he dimensionless curve shown in Fig is for the 0-mm impeller Since the impellers are not the same (0 mm versus 0 mm), dynamic similitude does not exist and thus, the curves are not the same 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part

Chapter / urbomachinery 800 0 Compute the specific speed: 0 / / 0, ( g ) ( 9 8 ) hence use a mixed flow pump As an alternate, since is close to unity, a radial flow pump could be employed Fig : At 0 7 (best eff), C 0 08, (a) C 0 08, C 0 00, C 0 0 W NS 70 78 rad /s, 0 0 09 78 / 7 ft, 0 08 78 7 7 8 ft, 0 0 78 7 NS 7 ft, W 0 00 9 78 7 6 0 ft - lb /sec, or W 6 0 / 0 horsepower 6 600 6 8 rad /s, 7 / 60 0 78 m / s, 0 ( g ) 6 8 0 78 ( 9 8 9 ) / / 0 7, Use a radial flow pump 8,,, or, 9, and 9 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part

Chapter / urbomachinery 0 Assume a pump speed N = 000 rpm, or 000 09 rad /s 0 W /( ) 00 0 /( 880 0 66) m, f 09 0 66 ( g ) ( 9 8 ) / / 6 he specific speed suggests a mixed-flow pump owever, if N = 000 rpm, a radial-flow pump may be appropriate Consider both possibilities Mixed flow: from Fig, at best, : Use C 0 07, C 0 8, C 0 067 C W g and C Combining and solving for and, / C g / C and C 0 66 / 08 9 8 / 0 067 0 m, 066 08 0 8 rad/s, 880 900 kg/m, g 98 or N 8 0 / 67 rpm W C 0 07 900 8 0 0 W, or kw W Radial flow: from Fig, at best, : C 0 07, C 0 06, C 0 W 0 66 / 0 06 9 8 / 0 0 878 m, 066 006 0878 9 rad/s, or 9 0 N 6 rpm W 0 007 900 9 0 878 6 0 W, or 6 kw ence, a mixed-flow pump is preferred 6 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part

Chapter / urbomachinery he intersection of the system demand curve with the head-discharge curve yields 7 m / min, 6 m, W 7 kw N 0 rpm, 7 m / min, 6 m, W 7 kw, N 00 rpm, N 00 7 m /min, N 0 N N 6 00 9 96 m, 0 W W N 7 00 06 N kw 0 Efficiency will remain approximately the same 7 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part

Chapter / urbomachinery 6 Compute system demand: f L K V g 00 0 00 m, 0 98 VA 0 0 m, 00 / 0 rad/s 0 9, Axial pump is appropriate / / ( g ) (980) 8 (a) he intersection of the pump curve with the demand curve yields 6 m and 80 m / h From Fig 6, 6 kw and NS 8 m W 0 Use energy eqn to establish system demand: f e 0 0008 ln 0 7 ln 0 7 0 07, z f L ga 0 07 80 60 ( / ) 60 0 89 00 From Fig 6, at best, ft / sec, and ft 9 8 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part

Chapter / urbomachinery Assume three pumps in series, so that 6 ft hen the demand head is 60 0 89 6 ft ence three pumps in series are appropriate he required power is W or W 0 / 0 06 hp / 6 086 6/ 07 0 ft - lb, sec (a) For water at 80C, pv = 6 0 a, and = 9 kg/m Write the energy equation from the inlet (section i) to the location of cavitation in the pump: pi Vi pv NS, g NS p p V i v i ( 8 6 ) 0 g 9 6 67 m 9 8 (b) NS = 67 m, N = 00 rpm, N = 000 rpm, / = NS NS N N 67 000 8 m 00 Given: 7 L 00 m, 0 0 m, z z z m, V m /s, 6 0 m / s, 9 kg /m, p 86 0 a, p 0 0 a Compute the pump head: 00 Re 0 7 60 v a -09 09 f ln 7Re ln 7 (0 ) 00 fl V 00 00 z 0 m g 00 98 9 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part

Chapter / urbomachinery (a) Choose a radial-flow pump Use Fig to select the size and speed: C 0, C 0 06, 0 7, 0 0 0 0089 m, C C g 0 0089 C 0 06 0 090 0 0 0089 0 090 m 0 06 9 8 0 (b) Available net positive suction head: (c) NS p p a g v 0 90 rad /s, or N 90 680 rpm 0 0 86 0 z 9 9 8 9 m 6 0 / 0 6 rad /s, cot (r b / cot ) cot ( 0 8 6/ 0 cot 7 ) 6 Vt u V r n cot cot r b 0 6 cot 7 8 7 m /s, 0 8 Vt u V r n cot cot rb 0 6 cot 00 9 m /s, 0 8 ( rv t rv t ) 000 0( 8 7 9 ) 80 7 N m 7 W 6 80 7 0 8 W, or 7 MW Under ideal conditions, and W W f, hence W / 7 0 8 /( 980 0) m 60 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part

Chapter / urbomachinery 8 N 0 rpm, W 00 kw, ft, W 9kW, ft From the similarity rules, W W N N N N and Substitute second eqn into the first to eliminate ( N / N ), and solve for : / / / / 9 0 W 076 ft, W 00 N N / / 0 0 99 0 76 rpm 0 Write energy eqn from upper reservoir (loc ) to surge tank (loc ) and solve for : ga f L z z ( ) / 9 8 ( / ) 0 8 0 0 000 / ( 60 68 ) 0 0 m / s Apply energy eqn from loc to lower reservoir (loc ) and determine : z z f L K v ga 0 0 00 0 0 68 9 0 8 m 9 8 0 8 W 980 0 0 0 9 89 0 W, or 89 kw From Fig, use a Francis turbine A representative value of the specific speed is (Fig 0): / / ( g ) ( 9 8 ) ( W / / ) ( 67 0 / 000) or N 06 0 / 90 rpm / 06 rad/s, 6 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part

Chapter / urbomachinery 00 / 0 0 9 rad /s, and from Fig at best efficiency ( = 08), 0, cv = 09 V cv g 0 9 9 80 6 m /s, 6 W 0 78 m /s 980 0 08 his is the discharge from all of the jets etermine the wheel radius r : r g 0 9 80 0 9 0 97 m, ence, the diameter of the wheel is r 0 97 9 m Compute diameter of one jet: j r / 8 9 / 8 0 m, or mm Let N j no of jets hen each jet has a discharge of / N j and an area / N V j j Solving for N j : N j 78 V 6 0 j, ( W Use three jets / ) / ( g ) / 0 9( 0 / 000) / ( 9 80) 6 / 0 0 7, 0 / 6, 60 ft / sec (one unit), W 7,00 0 6 ft 6 60 08 Write energy eqn from upper reservoir (loc ) to lake (loc ): z f L K z, ga 00 0 000,60 0 6 660, 6 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part

Chapter / urbomachinery which reduces to 8 6 7 99 0 89 0 6 0 Solving, 8 ft W 7, 000 0 76 6,000 kw, 6 008 0 m From Fig, a Francis or pump/turbine unit is indicated 6 (a) Let be the total head and the discharge delivered to the turbine; then 09 09 0 898 m and W 6 0 0 0 m / s 980 89 8 0 8 Write energy eqn from reservoir to turbine outlet: f L K ga, 0 0 000 0 89 8 9 8 ( / ), 9 67 06 which reduces to 0 Solving = m (b) Compute jet velocity: V cv g 0 98 9 8 89 8 7 9 m /s he flow through one nozzle is /, and the jet area is j / ence j / V / 79 0 06 m, 0 06 j 0 6 m 6 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part

Chapter / urbomachinery 8 ( 9 8 7) W 000 0 / 0 / 99 0 6 W (one unit) otal power developed is 9 0 6 W ence, required number of units is 9/ 99 8 Use two turbines 0 (a) fl z z ga 000 0 9 89 8 m, 098 (0780 ) W 980 0 8 08 6 0 W, or 6 kw (b) Compute the specific speed of the turbine: N 00 6 rad/s, 0 0 W 6 / 6 6 0 /000 / / g 988 ence, from Fig 0, a Francis turbine is appropriate (c) From Fig, the turbine with = 06 is chosen: C = 0, C = 0, and = 09 C C g C 0 7 rad /s, or N 7 680 rpm ; W 980 0 8 0 9 6 0 0 0 0 0 0 0 0 9 m, or approximately 00 m ; 0 9 8 8 Calculate a new specific speed based on the final design data: W, or 6 kw 7 60 /000 / 096 (988) an acceptable value according to Fig 0 6 0 Cengage Learning All Rights Reserved May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part