Design of stay vanes and spiral casing

Slides:



Advertisements
Similar presentations
Pressure, Drag and Lift for Uniform Flow Over a Cylinder a 2 = 1.
Advertisements

Flow Disturbance of Flow due to Bends and Obstacles, etc. Time Transients and Spatial Distribution of Fluid Force on Structure Surface FLAVOR-3D: 3-D Fluid.
Elementary Mechanics of Fluids
Design of Pelton turbines
Francis turbines Examples Losses in Francis turbines NPSH
External Flows.
The Ultimate Importance of Invariant Property : Rothalpy
First Law of Thermodynamics-The Energy Equation (4) Work transfer can also occur at the control surface when a force associated with fluid normal stress.
Cascade theory The theory in this lecture comes from: Fluid Mechanics of Turbomachinery by George F. Wislicenus Dover Publications, INC
Force due to a jet hitting an inclined plane
Fluid Dynamics.
THE WASHINGTON MONUMENT (1884) The purpose of this study is to show how this structure supports its own weight and wind load, by calculating its efficiency.
CIEG 305 DERIVATION OF THE ENERGY EQUATION 1 st Law of Thermodynamics Change in energy per time Rate at which heat is added to system Rate at which work.
MECH 221 FLUID MECHANICS (Fall 06/07) Chapter 10: OPEN CHANNEL FLOWS
Forces Acting on a Control Volume Body forces: Act through the entire body of the control volume: gravity, electric, and magnetic forces. Surface forces:
Design of Components of Francis Turbine
1 Short Summary of the Mechanics of Wind Turbine Korn Saran-Yasoontorn Department of Civil Engineering University of Texas at Austin 8/7/02.
Centrifugal pumps. Impellers Multistage impellers.
CHAPTER 7 ENERGY PRINCIPLE
CHAPTER 6 MOMENTUM PRINCIPLE Dr. Ercan Kahya Engineering Fluid Mechanics 8/E by Crowe, Elger, and Roberson Copyright © 2005 by John Wiley & Sons, Inc.
Application of the Momentum Equation
PHAROS UNIVERSITY ME 259 FLUID MECHANICS FOR ELECTRICAL STUDENTS Basic Equations for a Control Volume.
Unit: IV-Fluid Dynamic
Flow inside turbomachines
1 Energy Conversion. 2 Specific energy The specific energy of a hydro power plant is the quantity of potential and kinetic energy which 1 kilogram of.
Design Analysis of Parts of Francis Turbine
Wednesday, Nov. 19, 2003PHYS , Fall 2003 Dr. Jaehoon Yu 1 PHYS 1443 – Section 003 Lecture #21 Wednesday, Nov. 19, 2003 Dr. Mystery Lecturer 1.Fluid.
Dr. Jason Roney Mechanical and Aerospace Engineering
PHAROS UNIVERSITY ME 253 FLUID MECHANICS II
Design of stay vanes and spiral casing Revelstoke, CANADA.
Energy and Rotalpy Where: E 1 =Energy at the inlet of the turbine[J/kg] E 2 =Energy at the inlet of the turbine[J/kg] I 1 =Rotalpy at the inlet of the.
Monday April 26, PHYS , Spring 2004 Dr. Andrew Brandt PHYS 1443 – Section 501 Lecture #24 Monday, April 26, 2004 Dr. Andrew Brandt 1.Fluid.
Potential Flow and Computational Fluid Dynamics Numerical Analysis C8.3 Saleh David Ramezani BIEN 301 February 14, 2007.
Guide vanes in Francis turbines. El Cajon, HONDURAS.
NORWEGIAN HYDROPOWER CENTRE SEDIMENT EROSION IN HYDRAULIC TURBINES Biraj Singh Thapa, PhD Candidate (August 2013) Department of Energy and Process Engineering.
Momentum Equation and its Applications
Draft Tube Flow.
Bernoulli and Flow Continuity.  U-Tube Manometer  Used to measure pressure of a fluid  Principles involved: ◦ The pressure is the same in equal elevations.
IMPACT OF JETS PREPARED BY KIRIT S DAYMA ( )
Heat and Flow Technology I.
Heat and Flow Technology I.
Chapter 6: Momentum Analysis of Flow Systems
Centrifugal pumps.
EXAMPLE Water flows uniformly in a 2m wide rectangular channel at a depth of 45cm. The channel slope is and n= Find the flow rate in cumecs.
Pelton Wheel is an example of such turbine.
Continuity Equation.
Pimpri Chinchwad polytechnics
Dynamics of Uniform Circular Motion Rotational Kinematics
PHYS 1443 – Section 003 Lecture #21
Betz Theory for A Blade Element
Fluid Flow and Bernoulli’s Equation
The Bernoulli Equation
CE 3305 Engineering FLUID MECHANICS
Oscillations Readings: Chapter 14.
Invention of Geometries to Generate Lift
CTC 450 Bernoulli’s Equation EGL/HGL.
Control volume approach (검사체적 방법)
Guide vanes in Francis turbines
Motion in Two Dimensions
FLUIDS IN MOTION The equations that follow are applied when a moving fluid exhibits streamline flow. Streamline flow assumes that as each particle in the.
Draft Tube Flow.
Fluvial Hydraulics CH-3
Gas/Steam Medium.
Chunk 5 Application of Newton’s Laws
Kaplan turbine.
Friction 2 Rolling Objects Practice Problems LabRat Scientific © 2018.
We assume here Ideal Fluids
Hydraulic Turbines Presented By: Vinod Dahiya
Section 8, Lecture 1, Supplemental Effect of Pressure Gradients on Boundary layer • Not in Anderson.
Example 3.E - Graf Assume a channel with uniform flow at a depth of 5.03 m. Channel is rectangular with a width of 9 m and average velocity of 12 m/s.
Presentation transcript:

Design of stay vanes and spiral casing Revelstoke, CANADA

Guri-2, VENEZUELA

Aguila, ARGENTINA

Sauchelle-Huebra, SPAIN

Sauchelle-Huebra, SPAIN

Three Gorges Turbine, GE Hydro

The spiral casing will distribute the water equally around the stay vanes In order to achieve a uniform flow in to the runner, the flow has to be uniform in to the stay vanes.

Flow in a curved channel Streamline

The pressure normal to the streamline can be derived as:

Newton 2. Law gives: m 1

The Bernoulli equation gives: Derivation of the Bernoulli equation gives: 2

Equation 1 and 2 combined gives: Free Vortex

Inlet angle to the stay vanes cm ai cu

Plate turbine

Find the meridonial velocity from continuity: B

Find the tangential velocity: R0 R By

Example C L4 Flow Rate Q = 1,0 m3/s Velocity C = 10 m/s Height By = 0,2 m Radius R0 = 0,8 m Find: L1, L2, L3 and L4 L1 q L3 R0 R L2 By

Example C L4 Flow Rate Q = 1,0 m3/s Velocity C = 10 m/s Height By = 0,2 m Radius R0 = 0,8 m L1 q L3 R0 R L2 By

Example C L4 Flow Rate Q = 1,0 m3/s Velocity C = 10 m/s Height By = 0,2 m Radius R0 = 0,8 m We assume Cu to be constant along R0. At q=90o, Q is reduced by 25% L1 q L3 R0 R L2 By

Example C L4 Flow Rate Q = 0,75 m3/s Velocity Cu = 12,9 m/s Height By = 0,2 m Radius R0 = 0,8 m L1 q L3 R0 R L2 By

Example C L4 Flow Rate Q = 0,75 m3/s Velocity Cu = 12,9 m/s Height By = 0,2 m Radius R0 = 0,8 m L1 q L3 R0 R L2 L2 = 0,35 m L3 = 0,22 m L4 = 0,10 m By

Find the meridonial velocity from continuity: B k1 is a factor that reduce the inlet area due to the stay vanes

Find the tangential velocity:

Spiral casing design procedure We know the flow rate, Q. Choose a velocity at the upstream section of the spiral casing, C Calculate the cross section at the inlet of the spiral casing: Calculate the velocity Cu at the radius Ro by using the equation:

Spiral casing design procedure Move 20o downstream the spiral casing and calculate the flow rate: Calculate the new spiral casing radius, r by iteration with the equation:

Outlet angle from the stay vanes cm a cu

Weight of the spiral casing

Stay Vanes

Number of stay vanes

Design of the stay vanes The stay vanes have the main purpose of keeping the spiral casing together Dimensions have to be given due to the stresses in the stay vane The vanes are designed so that the flow is not disturbed by them

Flow induced pressure oscillation Where f = frequency [Hz] B = relative frequency to the Von Karman oscillation c = velocity of the water [m/s] t = thickness of the stay vane [m]

Where A = relative amplitude to the Von Karman oscillation B = relative frequency to the Von Karman oscillation