Nozzles & Jets for Pelton Wheels A Special Device to implement Pure Momentum based Energy Exchange……. P M V Subbarao Professor Mechanical Engineering.

Slides:



Advertisements
Similar presentations
Baffling in SHELL-AND-TUBE HEAT EXCHANGERS
Advertisements

OFF DESIGN PERFORMANCE PREDICTION OF STEAM TURBINES
Design of Pelton turbines
Design Analysis of Parts of Pelton Wheel Turbine
Impulse Turbine / Pelton Turbine
FUNDAMENTALS OF FLUID MECHANICS
PELTON TURBINE Pelton Turbine is a Tangential Flow Impulse Turbine.
MASS, MOMENTUM , AND ENERGY EQUATIONS
Monroe L. Weber-Shirk S chool of Civil and Environmental Engineering Closed Conduit Flow CEE 332.
Gravity Water Supply Design
California State University, Chico
Pertemuan CLOSED CONDUIT FLOW 2
Reynolds Experiment Laminar Turbulent Reynolds Number
CEE 331 Fluid Mechanics April 17, 2017
CEE 331 Fluid Mechanics April 17, 2017
Forces Acting on a Control Volume Body forces: Act through the entire body of the control volume: gravity, electric, and magnetic forces. Surface forces:
Closing Remarks on Pelton Wheel
Options for High Head Hydro Sites Design of Strong and Compact Muscles for High Specific Energy ……. P M V Subbarao Professor Mechanical Engineering Department.
Development of Turbine Cascades
Micro Turbines : Turbo-expanders New Solutions for Distributed Green & Waste Resources….. P M V Subbarao Professor Mechanical Engineering Department.
Boundary Layer Correction of Viscous Flow Through 2 D Turbine Cascades
Design of Components of Francis Turbine
Assessment of Engine Breathing Capacity P M V Subbarao Professor Mechanical Engineering Department Measure of Filling & Emptying Effectiveness….
Test 1A Same material Voluntary Outside regular class.
The Thrust Generator P M V Subbarao Professor Mechanical Engineering Department Another Passive Device…… An Obvious Concept for Generation of Motive Power.
Matching of Bucket to Jet in Pelton Wheels Satisfying the Concerns of Pelton……. P M V Subbarao Professor Mechanical Engineering Department.
CE 230-Engineering Fluid Mechanics
Fluid mechanics 3.1 – key points
C & CD Nozzles for Jet Propulsion
Pipe Sizing Basics Prof. Dr. Mahmoud Fouad Major & Minor Losses
PHAROS UNIVERSITY ME 259 FLUID MECHANICS FOR ELECTRICAL STUDENTS Basic Equations for a Control Volume.
Stagnation Properties P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Capacity of A Resource…..
Monroe L. Weber-Shirk S chool of Civil and Environmental Engineering Closed Conduit Flow CEE 332.
Design Analysis of Parts of Francis Turbine
Analysis of Axial & Centrifugal Compressors To be Selected as per Specific Speed of Applications…. P M V Subbarao Professor Mechanical Engineering Department.
Reynolds Transport Theorem We need to relate time derivative of a property of a system to rate of change of that property within a certain region (C.V.)
Gas dynamics of Real Combustion in Turbo Combustor P M V Subbarao Professor Mechanical Engineering Department Make Sure that design is Acceptable to Gas.
Design of Supersonic Intake / Nozzle P M V Subbarao Associate Professor Mechanical Engineering Department I I T Delhi Meeting the Cruising Conditions…
An Exclusive Conservation Equation for Ideal Turbo-machines P M V Subbarao Professor Mechanical Engineering Department Invention of New Property for CVs.
Jets & Buckets for Pelton Wheels Means to Complete the Second Law of Power Retrieval……. P M V Subbarao Professor Mechanical Engineering Department.
Engineering Relations from Second Law P M V Subbarao Professor Mechanical Engineering Department An Equation to Regulate Manufacturing Processes …..
Performance Analysis of Multi Stage Axial Flow Compressors

Steps in Development of 2 D Turbine Cascades P M V Subbarao Professor Mechanical Engineering Department A Classical Method Recommended by Schlichting.……
Viscous Flow in Pipes: Overview
Flow of Compressible Fluids. Definition A compressible flow is a flow in which the fluid density ρ varies significantly within the flowfield. Therefore,
G.H. Patel College of Engineering and Technology
Gas Dynamics of Flow through Valves Method to Estimate the Flow Capacity of Valve Passage…. P M V Subbarao Professor Mechanical Engineering Department.
Chapter 10: Flows, Pumps, and Piping Design
Nishkarsh Srivastava ( )
Theory of Turbine Cascades P M V Subbarao Professor Mechanical Engineering Department Its Group Performance, What Matters.……
Mathematics to Innovate Blade Profile P M V Subbarao Professor Mechanical Engineering Department Also a Fluid Device, Which abridged the Globe into Global.
First Law of Thermodynamics applied to Flow processes
Internal Incompressible
Fluid Mechanics and Machinery Hydraulic Turbines
The Multistage Impulse Turbines
The Bernoulli Equation
Design of Passive (Adiabatic) Control Volumes
PELTON WHEEL AND FRANCIS TURBINE
KINEMATICS 1. A nozzle is so shaped that the velocity of flow along the centre line changes linearly from 1.5 m/s to 15 m/s in a distance of m. Determine.
Multi-Staging in Impulse Turbines
Chapter 4. Analysis of Flows in Pipes
Reaction Turbines.
Analysis of Multi Stage Steam Turbines
Solar Energy Based Energy Systems - II
Estimation of Profile Losses
Control volume approach (검사체적 방법)
Chapter 5. Pipe System Learning Outcomes:
20. Pipe Flow 2 CH EN 374: Fluid Mechanics.
Hydraulic Turbines Presented By: Vinod Dahiya
Presentation transcript:

Nozzles & Jets for Pelton Wheels A Special Device to implement Pure Momentum based Energy Exchange……. P M V Subbarao Professor Mechanical Engineering Department

Key Parts of Pelton Turbine

Design Of Intake for High Release of Power p atm H

Multi Jet Distributors for Pelton Wheels

Discharge Distribution And Flow Energy Losses In the Distributor Q/Q BEP

CFD Analysis of Free Jets & Flows In Air A Consultancy Project Sponsored By BHEL, Bhopal

The set of governing equations solved were primarily the continuity and the momentum equations. These basic equations in Cartesian coordinate system for incompressible flows are given below, Governing Differential Equations

Arrangement of Jets

CAD Model of Distributor

Pelton Wheel Flow Distributor

Static Pressure Distribution

Distribution of Velocity Magnitude

Exit Velocities The area averaged values for the various critical sections are listed below, Inlet:20.77 ms-1 Outlet 1: ms-1 Outlet 2:18.13 ms-1 Outlet 3:17.05 ms-1 Outlet 4:16.91 ms-1 Outlet 5:15.22 ms-1 Outlet 6: 9.75 ms-1

Feedback It is evident from the area averaged values of velocity and the mass fluxes at the outlet that the flow distribution is not exactly uniform. The flow at outlets 2, 3, 4, 5 is almost equal, however, flow at outlet -1 is high and outlet -2 is low. The uniformity of flow distribution may be restored by employing variable openings using the spears provided inside the injection nozzle along with possible alterations in the rate of curvature of distributor especially in the region of outlet-6.

Closing Remarks : Multi Jet Pelton Wheel Higher rotational speed Smaller runner Simple flow control possible Redundancy Can cope with a large range of flows But Needs complex manifold May make control/governing complex

A Complex Engineering Micro Alternate To Simple Gigantic Natural System

Flow Control using Spear & Nozzle System

Free Surface Expansion Shape for Maximum Power

Simplification of Nozzle Shape   d0d0 d jet,VC The nozzle and spear are perfectly streamlined to reduce friction losses and achieve perfect circular jets.

Geometrical Relations for Nozzle The values of α varies between 20 to 30° whereas β varies from 30 to 45°.

Industrial Correlations for Jet Area variation with stroke Optimal value of Outlet jet area, a o s is the displacement of spear

Discharge through a Spear Nozzle if a o is the jet area at nozzle outlet section and knowing that this is dependable on the stroke s of the needle tip, the water velocity for this section is: Then, the corresponding flow rate is:

Discharge Control using Spear Nozzle

Linear Rate of Change Discharge w.r.t Stroke

Geometrical Relations for Nozzle dOdO 2d O – 2.4d O 5d O – 9d O 0.8d O – 0.9d O 1.2d O – 1.4d O 1.1d O – 1.3d O

Performance Analysis of Nozzle-Spear Valve Ideal Nozzle-spear Valve: Along flow direction Real Nozzle-spear Valve:

Pipe MaterialAbsolute Roughness, e micron (unless noted) drawn brass1.5 drawn copper1.5 commercial steel45 wrought iron45 asphalted cast iron120 galvanized iron150 cast iron260 wood stave0.2 to 0.9 mm concrete0.3 to 3 mm riveted steel0.9 to 9 mm

Numerical Computation of Total Pressure Variation

Jet carrying a discharge of Q to deliver a power P To generate a discharge of Q, we need a least jet diameter of Acceptable Performance of Nozzle

Diameter of the Jet at the outlet, d o It is important to find out the VC and outlet jet diameters/areas The Diameter of Jet before Reaching Bucket