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Francis turbines
•
•
•
•

Examples
Losses in Francis turbines
NPSH
Main dimensions
Traditional runner

X blade runner
SVARTISEN

P = 350 MW
H = 543 m
Q* = 71,5 m3/S
D0 = 4,86 m
D1 = 4,31m
D2 = 2,35 m
B0 = 0,28 m
n = 333 rpm
La Grande, Canada

P = 169 MW
H = 72 m
Q = 265 m3/s
D0 = 6,68 m
D1e = 5,71m
D1i = 2,35 m
B0 = 1,4 m
n = 112,5 rpm
Outlet
draft tube

Outlet
runner

Inlet
runner

Outlet
guide vane

Inlet
guide vane
Hydraulic efficiency
ηh =

c1u ⋅ u1 − c2u ⋅ u 2
=
g ⋅ Hn

1

2
2


 
c1
c3
 g ⋅ h1 + + z1  −  g ⋅ h 3 + + z 3  − losses

 

2
2

 

2
2


 
c1
c3
 g ⋅ h 1 + + z1  −  g ⋅ h 3 + + z 3 

 

2
2

 

Losses in Francis Turbines

Hydraulic Efficiency [%]

Draft tube

Output Energy

Head [m]
Hydraulic Efficiency [%]

Losses in Francis Turbines

Output Energy

Output [%]
Friction losses between runner
and covers

Friction losses
Gap losses

Gap losses
Friction losses

Friction losses in
the spiral casing
and stay vanes
Guide vane losses

Gap losses
Runner losses
Draft tube losses
Relative path

Absolute path without
the runner installed

Absolute path with the runner installed
Velocity triangles
Net Positive Suction Head, NPSH
2
2
2
c3
c3
c2
h2 +
+ z 2 = hb + h3 +
+ z3 + ζ ⋅
2⋅g
2⋅g
2⋅g
2
c3
− H s = h3 +
+ z3 − z 2
2⋅g

c2
h 2 + 2 + z2
2⋅g
c2
h2 + 2
2⋅g

2
c3
= h b − Hs + z2 + ζ ⋅
2⋅g

J
= h b − Hs + J
1

'
h 2 = hb + h 2
NPSH
h2

2
 c2


= hb − H s − 
 2 ⋅ g − J  > hva



NPSH

NPSH = h b − h 2 − H s

NB:
HS has a negative
value in this figure.
NPSH required
NPSH R

< h b − h va − H s
2
m2

= NPSH A

2
2

c
u
NPSH R = a ⋅
+b⋅
2⋅ g
2⋅ g

Turbines
Pumps
a 1.05 < a < 1.15 1.6 < a < 2.0
b 0.05 < b < 0.15 0.2 < b < 0.25
Main dimensions
• Dimensions of the outlet
• Speed
• Dimensions of the inlet

D1

D2
Dimensions of the outlet
We assume cu2= 0 and choose β2 and u2 from NPSHR:
2
c
u
a ⋅ ( u 2 ⋅ tan β 2 ) + b ⋅ u 2
NPSH R = a ⋅
+b⋅
=
2⋅ g
2⋅ g
2⋅ g
2
m2

13o <
35 <
1,05 <
0,05 <

β2
u2
a
b

<
<
<
<

2
2

2

22o
(Lowest value for highest head)
43 m/s (Highest value for highest head)
1,15
0,15
Diameter at the outlet
c m 2 = u 2 tan β 2
Connection between cm2and choose D2 :

D2
Q = π ⋅ 2 ⋅ cm2
4

⇒ cm2

Q⋅4
=
π ⋅ D2
2

D1

4⋅Q
⇒ D2 =
π ⋅ cm 2
D2
Speed
Connection between n and choose u2 :

π ⋅ D2 ⋅ n
u2 =
60

u 2 ⋅ 60
⇒ n=
π ⋅ D2
Correction of the speed
The speed of the generator is given from the
number of poles and the net frequency

3000
n=
zp

for

f = 50Hz
Example
Given data:
Flow rate
Head

Q = 71.5 m3/s
H = 543 m

We choose:
a = 1,10
b = 0,10
β2 = 22o
u2 = 40 m/s

(

)

 2

1,1⋅ 40 ⋅ tan 22 + 0,1 ⋅ 40 2
NPSH R =
= 22,8 m
2⋅g
Find D2 from:
4⋅Q
4⋅Q
D2 =
=
π ⋅ cm 2
π ⋅ u2 ⋅ tan β 2

4 ⋅ 71,5
D2 =
= 2.37 m

π ⋅ 40 ⋅ tan 22
Find speed from:

u2 ⋅ 60 40 ⋅ 60
n=
=
= 322 rpm
π ⋅ D2 π ⋅ 2.37
Correct the speed with synchronic speed:
3000
zp =
= 9.3
n
3000
choose z p = 9 ⇒ n K =
= 333 rpm
9
We keep the velocity triangle at the outlet:
u2

u2K

β2
c2
c2K

w2
cm 2 cmK
tan β 2 =
=
u2 u2 K

4⋅Q
4⋅Q
π ⋅ D22 K
π ⋅ D22
=
=
π
π
⋅ n ⋅ D2
⋅ nK ⋅ D2 K
60
60

⇓
3
3
nK ⋅ D2 K = n ⋅ D2

⇓
D2 K

3
n ⋅ D2
322
=3
= 2.373 ⋅ 3
= 2.35m
nK
333
Dimensions of the inlet
u 1 ⋅ c u1 − u 2 ⋅ c u 2
ηh =
= 2 ⋅ ( u 1 ⋅ c u1 − u 2 ⋅ c u 2 )
g⋅H
At best efficiency point, cu2= 0

u 1 ⋅ c u1
ηh ≈ 0,96 =
= 2 ⋅ u 1 ⋅ c u1
g⋅H

ηh
0,96
c u1 =
=
2 ⋅ u1 2 ⋅ u1
Diameter at the inlet
We choose:

0,7 < u1 < 0,75

D1 n ⋅ 2 ⋅ π D1
u1 = ω ⋅
=
⋅
2
60
2
⇓
u1 ⋅ 60
D1 =
n⋅π

D1

D2
Height of the inlet
Continuity gives:

c m1 ⋅ A1 = c m 2 ⋅ A 2
We choose:

cm2 = 1,1 · cm1

1.1 ⋅ π ⋅ D
B1 ⋅ D1 ⋅ π =
4

2
2

B1 = B0
Inlet angle
cu1
cm1
c1

c m1
tan β 1 =
u1 − c u1

u1
β1
w1
Example continues
Given data:
Flow rate
Head

Q = 71.5 m3/s
H = 543 m

We choose:
ηh = 0,96
u1 = 0,728
cu2 = 0

η h = 2 ⋅ u 1 ⋅ c u1

ηh
0.96
⇒ c u1 =
=
= 0,66
2 ⋅ u1 2 ⋅ 0,728
Diameter at the inlet
u1 = u1 ⋅ 2 ⋅ g ⋅ h = 0,728 ⋅ 2 ⋅ 9,81⋅ 543 = 75,15 m s

u1 ⋅ 60 75,15 ⋅ 60
D1 =
=
= 4,31 m
n ⋅π
333 ⋅ π

D1
Height of the inlet
1,1⋅ π ⋅ D
1,1⋅ 2.35
B1 =
=
= 0,35 m
4 ⋅ D1 ⋅ π
4 ⋅ 4,31
2
2

B1

2
Inlet angle
cu1
cm1
c1

u1
β1
w1

cm 2 sin β 2 ⋅ u2 sin 22 ⋅ 40,9 m s
cm1 =
=
=
= 13,9 m s
1,1
1,1
1,1
c m1 =

c m1
13,9
=
= 0,135
2⋅g ⋅h
2 ⋅ 9,81 ⋅ 543

 c m1 
0,135


 = arctan
β1 = arctan
 = 62.9
u −c 
 0,728 − 0,659 
 1 u1 
SVARTISEN

P = 350 MW
H = 543 m
Q* = 71,5 m3/S
D0 = 4,86 m
D1 = 4,31m
D2 = 2,35 m
B0 = 0,28 m
n = 333 rpm

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Francis turbine

  • 1. Francis turbines • • • • Examples Losses in Francis turbines NPSH Main dimensions
  • 2.
  • 3.
  • 5. SVARTISEN P = 350 MW H = 543 m Q* = 71,5 m3/S D0 = 4,86 m D1 = 4,31m D2 = 2,35 m B0 = 0,28 m n = 333 rpm
  • 6. La Grande, Canada P = 169 MW H = 72 m Q = 265 m3/s D0 = 6,68 m D1e = 5,71m D1i = 2,35 m B0 = 1,4 m n = 112,5 rpm
  • 7.
  • 9. Hydraulic efficiency ηh = c1u ⋅ u1 − c2u ⋅ u 2 = g ⋅ Hn 1 2 2     c1 c3  g ⋅ h1 + + z1  −  g ⋅ h 3 + + z 3  − losses     2 2     2 2     c1 c3  g ⋅ h 1 + + z1  −  g ⋅ h 3 + + z 3      2 2    
  • 10. Losses in Francis Turbines Hydraulic Efficiency [%] Draft tube Output Energy Head [m]
  • 11. Hydraulic Efficiency [%] Losses in Francis Turbines Output Energy Output [%]
  • 12. Friction losses between runner and covers Friction losses
  • 14. Friction losses Friction losses in the spiral casing and stay vanes Guide vane losses Gap losses Runner losses Draft tube losses
  • 15.
  • 16. Relative path Absolute path without the runner installed Absolute path with the runner installed
  • 18. Net Positive Suction Head, NPSH 2 2 2 c3 c3 c2 h2 + + z 2 = hb + h3 + + z3 + ζ ⋅ 2⋅g 2⋅g 2⋅g 2 c3 − H s = h3 + + z3 − z 2 2⋅g c2 h 2 + 2 + z2 2⋅g c2 h2 + 2 2⋅g 2 c3 = h b − Hs + z2 + ζ ⋅ 2⋅g J = h b − Hs + J 1 ' h 2 = hb + h 2
  • 19. NPSH h2 2  c2   = hb − H s −   2 ⋅ g − J  > hva   NPSH NPSH = h b − h 2 − H s NB: HS has a negative value in this figure.
  • 20. NPSH required NPSH R < h b − h va − H s 2 m2 = NPSH A 2 2 c u NPSH R = a ⋅ +b⋅ 2⋅ g 2⋅ g Turbines Pumps a 1.05 < a < 1.15 1.6 < a < 2.0 b 0.05 < b < 0.15 0.2 < b < 0.25
  • 21. Main dimensions • Dimensions of the outlet • Speed • Dimensions of the inlet D1 D2
  • 22. Dimensions of the outlet We assume cu2= 0 and choose β2 and u2 from NPSHR: 2 c u a ⋅ ( u 2 ⋅ tan β 2 ) + b ⋅ u 2 NPSH R = a ⋅ +b⋅ = 2⋅ g 2⋅ g 2⋅ g 2 m2 13o < 35 < 1,05 < 0,05 < β2 u2 a b < < < < 2 2 2 22o (Lowest value for highest head) 43 m/s (Highest value for highest head) 1,15 0,15
  • 23. Diameter at the outlet c m 2 = u 2 tan β 2 Connection between cm2and choose D2 : D2 Q = π ⋅ 2 ⋅ cm2 4 ⇒ cm2 Q⋅4 = π ⋅ D2 2 D1 4⋅Q ⇒ D2 = π ⋅ cm 2 D2
  • 24. Speed Connection between n and choose u2 : π ⋅ D2 ⋅ n u2 = 60 u 2 ⋅ 60 ⇒ n= π ⋅ D2
  • 25. Correction of the speed The speed of the generator is given from the number of poles and the net frequency 3000 n= zp for f = 50Hz
  • 26. Example Given data: Flow rate Head Q = 71.5 m3/s H = 543 m We choose: a = 1,10 b = 0,10 β2 = 22o u2 = 40 m/s ( )  2 1,1⋅ 40 ⋅ tan 22 + 0,1 ⋅ 40 2 NPSH R = = 22,8 m 2⋅g
  • 27. Find D2 from: 4⋅Q 4⋅Q D2 = = π ⋅ cm 2 π ⋅ u2 ⋅ tan β 2 4 ⋅ 71,5 D2 = = 2.37 m  π ⋅ 40 ⋅ tan 22
  • 28. Find speed from: u2 ⋅ 60 40 ⋅ 60 n= = = 322 rpm π ⋅ D2 π ⋅ 2.37
  • 29. Correct the speed with synchronic speed: 3000 zp = = 9.3 n 3000 choose z p = 9 ⇒ n K = = 333 rpm 9
  • 30. We keep the velocity triangle at the outlet: u2 u2K β2 c2 c2K w2 cm 2 cmK tan β 2 = = u2 u2 K 4⋅Q 4⋅Q π ⋅ D22 K π ⋅ D22 = = π π ⋅ n ⋅ D2 ⋅ nK ⋅ D2 K 60 60 ⇓ 3 3 nK ⋅ D2 K = n ⋅ D2 ⇓ D2 K 3 n ⋅ D2 322 =3 = 2.373 ⋅ 3 = 2.35m nK 333
  • 31. Dimensions of the inlet u 1 ⋅ c u1 − u 2 ⋅ c u 2 ηh = = 2 ⋅ ( u 1 ⋅ c u1 − u 2 ⋅ c u 2 ) g⋅H At best efficiency point, cu2= 0 u 1 ⋅ c u1 ηh ≈ 0,96 = = 2 ⋅ u 1 ⋅ c u1 g⋅H ηh 0,96 c u1 = = 2 ⋅ u1 2 ⋅ u1
  • 32. Diameter at the inlet We choose: 0,7 < u1 < 0,75 D1 n ⋅ 2 ⋅ π D1 u1 = ω ⋅ = ⋅ 2 60 2 ⇓ u1 ⋅ 60 D1 = n⋅π D1 D2
  • 33. Height of the inlet Continuity gives: c m1 ⋅ A1 = c m 2 ⋅ A 2 We choose: cm2 = 1,1 · cm1 1.1 ⋅ π ⋅ D B1 ⋅ D1 ⋅ π = 4 2 2 B1 = B0
  • 34. Inlet angle cu1 cm1 c1 c m1 tan β 1 = u1 − c u1 u1 β1 w1
  • 35. Example continues Given data: Flow rate Head Q = 71.5 m3/s H = 543 m We choose: ηh = 0,96 u1 = 0,728 cu2 = 0 η h = 2 ⋅ u 1 ⋅ c u1 ηh 0.96 ⇒ c u1 = = = 0,66 2 ⋅ u1 2 ⋅ 0,728
  • 36. Diameter at the inlet u1 = u1 ⋅ 2 ⋅ g ⋅ h = 0,728 ⋅ 2 ⋅ 9,81⋅ 543 = 75,15 m s u1 ⋅ 60 75,15 ⋅ 60 D1 = = = 4,31 m n ⋅π 333 ⋅ π D1
  • 37. Height of the inlet 1,1⋅ π ⋅ D 1,1⋅ 2.35 B1 = = = 0,35 m 4 ⋅ D1 ⋅ π 4 ⋅ 4,31 2 2 B1 2
  • 38. Inlet angle cu1 cm1 c1 u1 β1 w1 cm 2 sin β 2 ⋅ u2 sin 22 ⋅ 40,9 m s cm1 = = = = 13,9 m s 1,1 1,1 1,1 c m1 = c m1 13,9 = = 0,135 2⋅g ⋅h 2 ⋅ 9,81 ⋅ 543  c m1  0,135    = arctan β1 = arctan  = 62.9 u −c   0,728 − 0,659   1 u1 
  • 39. SVARTISEN P = 350 MW H = 543 m Q* = 71,5 m3/S D0 = 4,86 m D1 = 4,31m D2 = 2,35 m B0 = 0,28 m n = 333 rpm