fluid system 09-reaction turbine-francis and...
TRANSCRIPT
Dr. Ir. Harinaldi, M.EngMechanical Engineering Department
Faculty of Engineering University of Indonesia
Reaction tuRbines
Radial Flow Radial Flow –– Francis TurbineFrancis Turbine
Construction of Francis TurbineConstruction of Francis Turbine
Velocity TriangleVelocity TriangleEuler Equation:
g
CUCUmgWE xx 2211
Flow velocities:
111 2 br
QCr
222 2 br
QCr
heightrunnerb
Axial Flow Axial Flow –– Kaplan TurbineKaplan Turbine
Construction of Kaplan TurbineConstruction of Kaplan Turbine
Velocity TriangleVelocity TriangleEuler Equation:
g
CCUmgWE xx 21
For zero whirl at exit:gUCE x1
1
11
cot 180cot
a
oax
CUCUC
g
UCUE a 12 cot
arr CCC 21
22114
dDQCCC arr
Flow velocities:
diameterhubdtipbladetodiameterD
)(diameter mean at evaluate is mDUNote:
2dDDm 60NDU m
InstallationInstallation
Net Head Across TurbineNet Head Across Turbine Net head (H) is the different in the
total head between the inlet flange and the tail water level
Net head (H) is not equal to Gross head (H1)
Total head across turbine
gVZgVgpH
ZgaugepZZgVVgppH22
0 ; )( 0 ; 22
302
00
33302
32
030
gVhHH fp 2231
Relation: net head and gross head
Energy given to the runner
rgd hhhHmgWE
energy kinetic residual2
runnerin loss head frictionaldraft tubein loss head frictional
vanesguidein loss head frictional
pipelinein loss head frictional
23
gVhhhh
r
d
g
fp
Losses and EfficiencyLosses and EfficiencyEnergy balance through the turbine
slcrm PPPPPP Ps = shaft power output Pc = casing and draft tube lossPm= mechanical loss Pl = leakage lossPr = runner loss P = water power available
Runner Loss
rrr hgQP qQQr
runner through rate flowrQleakage rate flowq
runnerin loss head frictionalrh
Leakage Loss
rl gqHP runner theacross head totalrH
Casing and draft tube Loss
cc gQhP draft tube and casingin loss headch
Energy balance becomes: srcrrm PqHQhQhgPgQH
Losses and EfficiencyLosses and EfficiencyOverall Efficiency
gQHPs
o
flangeinlet at availablepower fluidpoweroutput shaft
gQH
PP msH
flangeinlet at availablepower fluidrunnerby receivedpower
Hydraulic efficiency
For maximum efficiency
gQHCU x
H 11
Characteristics CurvesCharacteristics Curves
Characteristics CurvesCharacteristics Curves
Comparison of hydraulic turbine efficiencies
Draft TubeDraft Tube Bring the water pressure back to the pressure of the tailrace Remove the kinetic energy still existing at the runner outlet
adsa
da
a
d
pphgVVHgpgphgVVZygpgp
ygpgpZhZgVgpZgVgp
22
32
22
23
2222
33
32
3322
22
2
2
; 0 22
Energy Equation between runner outlet and tailrace
Efficiency of draft tube
gV
hgVV
d
d
2
2
draft tube of entranceat headvelocity head pressurein gain net
22
23
22
Cavitation in TurbineCavitation in Turbine
ExampleExampleA Francis turbine has an inlet diameter of 1.4 m and rotates at 430 rpm. Water enters the runner without shocks with a flow velocity of 9.5 m/s and leaves the runner without whirl with an absolute velocity of 7 m/s. The difference between the sum of the static and potential heads at entrance to the runner and at the exit from the runner is 62 m. If the turbine develops 12 250 kW and has a flow rate of 12 m3/s of water when the net head is 115 m, find(a) The absolute velocity at entry to the runner and angle of inlet guide vane(b) Runner blade entry angle(c) Head loss in runnerSolution:Given: D1= 1.4 m; N = 430 rpm; Cr1= 9.5 m/s; C2 = 7 m/s; P = 12250 kW; H = 115 m; Q = 12 m3/s ; Cx2 = 0(a) Inlet velocity and inlet guide vane angle
m/s 5.31604304.16011 NDURunner tip speed
Power given to runner
m/s 4.325.311210
10.122503
3
11
112211
QUPC
CQUg
CUCUgQP
x
xxx
ExampleExample
m/s 8.334.325.9 2221
211 xr CCC
(b) Runner blade entry angle
Absolute inlet velocity
Inlet guide vane angle
o
x
r
CC 3.16
4.325.9arctanarctan
1
11
o
x
r
UCC 6.84
5.314.325.9arctanarctan
11
11
(c) Head loss in runner
Head loss in runner = total head across runner – head transferred to runner
Total head across runner = 21
22
2121
2ZZ
gCC
gpp
Head transferred to runner = gCU x11
ExampleExample
m 622121
ZZg
pp
However,
gCUZZ
gCC
gpph x
r11
21
22
2121
2
Head loss in runner
Thus,
m 69.13
81.94.325.31
81.9278.3362
262
22
1122
21
gCU
gCCh x
r