Module 4 Reaction Turbines: Kaplan Turbine. Module 4 Reaction Turbines: Kaplan Turbine....
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Transcript of Module 4 Reaction Turbines: Kaplan Turbine. Module 4 Reaction Turbines: Kaplan Turbine....
Module 4
Reaction Turbines: Kaplan Turbine.
Introduction.
Radial : At entrance to runner blade, velocity has primarily radial component.
Eg: Old Francis turbines.
Mixed : At entrance to runner blade, velocity has a radial as well as axial component.
Eg: Modern Francis Turbines
Axial: At entrance to runner blade, velocity has primarily an axial component.
Eg: Kaplan and propeller turbines.
Classification of Reaction Turbines: Radial, Mixed and Axial
RadialAxial
Kaplan Turbine Schematic
Spiral casing
Guide Vane
Kaplan Runner
Draft tube
Hub
Kaplan Turbine - Photo
Kaplan Runner
Hub
Kaplan Turbine – Horizontal Installation
Kaplan Runner
Hub
Kaplan Turbine Versus Propeller turbine
Propeller turbine
Kaplan turbine: Propeller turbine with variable pitch (adjustable) propeller blades
The Kaplan turbine has runner blades that can be adjusted to run at maximum efficiency for various head (H) and flow (Q) conditions. Propeller turbines have fixed blades
Kaplan Turbine Schematic
Generator
Guide Vane
Kaplan Runner
Draft tube
Runner hub
Reaction Turbine Schematic
Francis Turbine Kaplan Turbine
Path of a water particle
1 2
Kaplan turbine - Points to remember
1. Peripheral velocites at inlet and exit, and equal.
; Since inlet and exit of a particle of water is60
at the same radius or equivalently the same diamete
u u
DNu
1 2
2 2 31
1
r D,
2.Flow velocities are assumed same at inlet and exit.
3. Flow through the turbine is Q= m /s4
where is the runner outer diameter, is the runner hub diameter
and is the flow v
o h f
o h
f
u u
D D V
D D
V
elocity at inlet.
Kaplan Turbine Runner
Path of a water particle
oDhD
Kaplan Turbine – Problem p1
2u
2fV2r
2rV
1u 1wV
1rV 1fV1V
1a 1r
3 2
3
Step 1 : Find flow rate through turbine
Shaft Power 11772 kW0.84
Water Horse Power1000
11772 kW
1000 kg/m 9.81 m/s 20 m
1000
71.428 m /s
o gQH
Q
Q
2V
A Kaplan turbine working under a head of 20 m develops 11772 kW shaft power. Outer
and hub diameters of the runner are 3.5 m and 1.75 m. Guide blade angle at extreme edge
of runner is 35 . Hydraulic an d overall efficiencies are respectively 88% and 84 % . If
velocity of whirl is 0 at outlet determine 1) Runner vane angles at inlet and exit at extreme
edge of runner 2) Speed of turbine.
Kaplan Turbine – Problem p2
2u
2fV2r
u2rV
1u 1wV
1rV 1fV1V
u
1a 1r
1
3 2 21
3
12 22 2
Step 2 : Find flow velocity at inlet
71.428 m /s4
71.428 m /s
3.5 m 1.75 m4 4
9.9 m/s
f
o h f
f
o h
V
Q D D V
QV
D D
Guide blade angle Angle made by fluid
absolute velocity to runner peripheral
velocity
A Kaplan turbine working under a head of 20 m develops 11772 kW shaft power. Outer
and hub diameters of the runner are 3.5 m and 1.75 m. Guide blade angle at extreme edge
of runner is 35 . Hydraulic an d overall efficiencies are respectively 88% and 84 % . If
velocity of whirl is 0 at outlet determine 1) Runner vane angles at inlet and exit at extreme
edge of runner 2) Speed of turbine.
Kaplan Turbine – Problem p2
2u
2fV2r
u2rV
1u 1wV
1rV 1fV1V
u
1a 1r
Guide blade angle Angle made by fluid
absolute velocity to runner peripheral
velocity
A Kaplan turbine working under a head of 20 m develops 11772 kW shaft power. Outer
and hub diameters of the runner are 3.5 m and 1.75 m. Guide blade angle at extreme edge
of runner is 35 . Hydraulic an d overall efficiencies are respectively 88% and 84 % . If
velocity of whirl is 0 at outlet determine 1) Runner vane angles at inlet and exit at extreme
edge of runner 2) Speed of turbine.
1
11
1
11
Step 3 : Find whirl velocity at inlet
from inlet velocity triangle.
tan tan 35
9.9 m/s14.14 m/s
tan 35 tan 35
w
fa
w
fw
V
V
V
VV
Kaplan Turbine – Problem p2
2u
2fV2r
u2rV
1u 1wV
1rV 1fV1V
u
1a 1r
Guide blade angle Angle made by fluid
absolute velocity to runner peripheral
velocity
A Kaplan turbine working under a head of 20 m develops 11772 kW shaft power. Outer
and hub diameters of the runner are 3.5 m and 1.75 m. Guide blade angle at extreme edge
of runner is 35 . Hydraulic an d overall efficiencies are respectively 88% and 84 % . If
velocity of whirl is 0 at outlet determine 1) Runner vane angles at inlet and exit at extreme
edge of runner 2) Speed of turbine.
1
11 12
1
Step 4 : Find peripheral vel at inlet
14.14 m/s0.88
9.81 m/s 20 m
12.21 m/s
wh
u
uV u
gH
u
1 1 2Runner PowerHydraulic Efficiency =
Water power
w wm V u V
0
2
1 1 2w w
u
QH
Q V u V
0
21 1w
u V u
gQH gH
Kaplan Turbine – Problem p3
2u
2fV2r
u2rV
1u 1wV
1rV 1fV1V
u
1a 1r
1
11
1 1
1
Step 5 : Runner vane angle at inlet
9.9 m/stan
14.14 m/s 12.21 m/s
78.97
r
fr
w
r
V
V u
A Kaplan turbine working under a head of 20 m develops 11772 kW shaft power. Outer
and hub diameters of the runner are 3.5 m and 1.75 m. Guide blade angle at extreme edge
of runner is 35 . Hydraulic an d overall efficiencies are respectively 88% and 84 % . If
velocity of whirl is 0 at outlet determine 1) Runner vane angles at inlet and exit at extreme
edge of runner 2) Speed of turbine.
Kaplan Turbine – Problem p4
2u
2fV2r
u2rV
1u 1wV
1rV 1fV1V
u
1a 1r
2
1 2 1 2
2 12
2 1
1
Step 6 : Find vane angle at outlet
For Kaplan turbine and
9.9 m/stan
12.21 m/s
39.035
r
f f
f fr
r
u u V V
V V
u u
A Kaplan turbine working under a head of 20 m develops 11772 kW shaft power. Outer
and hub diameters of the runner are 3.5 m and 1.75 m. Guide blade angle at extreme edge
of runner is 35 . Hydraulic an d overall efficiencies are respectively 88% and 84 % . If
velocity of whirl is 0 at outlet determine 1) Runner vane angles at inlet and exit at extreme
edge of runner 2) Speed of turbine.
Kaplan Turbine – Problem p4
2u
2fV2r
u2rV
1u 1wV
1rV 1fV1V
u
1a 1r
1
Step 7 : Find Speed Of Turbine N
3.5 m12.21 m/s =
60 6066.63 rpm
NDNu
N
A Kaplan turbine working under a head of 20 m develops 11772 kW shaft power. Outer
and hub diameters of the runner are 3.5 m and 1.75 m. Guide blade angle at extreme edge
of runner is 35 . Hydraulic an d overall efficiencies are respectively 88% and 84 % . If
velocity of whirl is 0 at outlet determine 1) Runner vane angles at inlet and exit at extreme
edge of runner 2) Speed of turbine.
The End