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Nozzles

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

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Title: Nozzles


1
Nozzles Jets for Pelton Wheels
P M V Subbarao Professor Mechanical Engineering
Department
A Special Device to implement Pure Momentum based
Energy Exchange.
2
Key Parts of Pelton Turbine
3
Design Of Intake for High Release of Power
4
Multi Jet Distributors for Pelton Wheels
5
Discharge Distribution And Flow Energy Losses In
the Distributor
Q/QBEP
6
  • CFD Analysis of Free Jets Flows In Air

A Consultancy Project Sponsored By BHEL,
Bhopal 2008 -- 2009
7
Governing Differential Equations
  • 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,

8
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9
Arrangement of Jets
10
CAD Model of Distributor
11
Pelton Wheel Flow Distributor
12
Static Pressure Distribution
13
Distribution of Velocity Magnitude
14
Exit Velocities
The area averaged values for the various critical
sections are listed below, Inlet 20.77
ms-1 Outlet 1 25.37 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
15
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.

16
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

17
A Complex Engineering Micro Alternate To Simple
Gigantic Natural System
18
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19
Flow Control using Spear Nozzle System
20
Free Surface Expansion Shape for Maximum Power
21
Simplification of Nozzle Shape
The nozzle and spear are perfectly streamlined to
reduce friction losses and achieve perfect
circular jets.
22
Geometrical Relations for Nozzle
The values of a varies between 20 to 30 whereas
ß varies from 30 to 45.
23
Industrial Correlations for Jet Area variation
with stroke
Optimal value of Outlet jet area, ao
s is the displacement of spear
24
Discharge through a Spear Nozzle
if ao 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
25
Discharge Control using Spear Nozzle
26
Linear Rate of Change Discharge w.r.t Stroke
27
Geometrical Relations for Nozzle
2dO 2.4dO
dO
5dO 9dO
28
Performance Analysis of Nozzle-Spear Valve
Ideal Nozzle-spear Valve
Along flow direction
Real Nozzle-spear Valve
29
Pipe Material Absolute Roughness, e
Pipe Material micron(unless noted)
drawn brass 1.5
drawn copper 1.5
commercial steel 45
wrought iron 45
asphalted cast iron 120
galvanized iron 150
cast iron 260
wood stave 0.2 to 0.9 mm
concrete 0.3 to 3 mm
riveted steel 0.9 to 9 mm
30
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31
Numerical Computation of Total Pressure Variation
32
Acceptable Performance of Nozzle
Jet carrying a discharge of Q to deliver a power P
To generate a discharge of Q, we need a least jet
diameter of
33
The Diameter of Jet before Reaching Bucket
Diameter of the Jet at the outlet, do
It is important to find out the VC and outlet jet
diameters/areas
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