Upload
riya-jane
View
217
Download
0
Tags:
Embed Size (px)
Citation preview
Matching of Buckets & Wheel
Optimal number of Muscles for this Artificial Beat…….
P M V SubbaraoProfessor
Mechanical Engineering Department
The Bucket of A Pelton Wheel
• A Pelton Wheel is a work generating animal (An Elephant).
• Basic diet is Hydro Potential energy (calorific Value).
• Intake System efficiently converts Potential Energy into Kinetic Energy (ATP).
• Bucket convert kinetic energy into shaft energy (The Muacles)
• How to select the size and number of Muscles Required by a Specific Pelton Turbine.
Geometry of Wheel, Bucket & Jet Interactions
Rpelton
dj,O, Vj,O
Rwheel
A
A’B B’
Number of buckets
• The number of buckets for a given runner must be determined so that no water particle is lost.
• Minimize the risks of detrimental interactions between the out flowing water particles and the adjacent buckets.
• The runner pitch is determined by the paths of; – the bucket tip (diameter Dpelton), – the Wheel diameter (DWheel).
• and the relative paths of the water particles stemming from the upper (A-A’)and lower (B-B’) generators of the jet.
• The bucket pitch must be selected so that no particle stemming from the lower generator of the jet can escape the runner without encountering any bucket.
Bucket Duty Cycle
Reference Position
Zones of Bucket Duty Cycle
• i) Approach of the tip to the jet (θj < −40◦).
• ii) Initial feeding process : (θj = −40◦...−10◦).
• iii) Entire separation of the jet (θj = −10◦...0◦)
• iv) Last stage of inflow (θj = 0◦...15◦)
• v) Last stage of outflow (θj = 15◦...50◦).
• vi) Series of droplets (θj = −50◦...∞).
Minimum Number of Buckets
1B 1C
Rwheel
Rpelton
Dj,O, Vj,O
1A
1D
Best location of Jet :The axis of the jet falls on Pitch Circle
Minimum Number of Buckets
1B 1C1E
RwheelR
Pelton
dj,O, Vj,O
Minimum Number of Buckets
RW
heelRPelton
dO, Vj,O
lj
tj : Time taken bye the jet to travel lj
tb: Time taken by first bucket to travel
RWRP
dO, Vj,O
lj
sinpeltonj Dl
wheel
wheel
R
U
• tj = lj/Vjet,O
• tb =
For better working tj < tb
Oj
j
V
l
,
wheel
wheel
Oj
pelton
U
R
V
D
,
sin
Ojwheel
peltonwheel
VR
DU
,
sin
The minimum allowable value of
sin12sin ,
,
wheelvO
wheelu
wheel
pelton
Oj
wheel
Rk
k
R
D
V
U
RWRP
dO, Vj,O
lj
pelton
Ojetwheel
R
dR
2cos
,
wheel
Ojetwheel
R
dR
2cos
,
wheel
wheel
Ojet
D
D
d
2
1
1
cos
,
wheel
VCjetvturbine
us D
dK
KN wheel ,
14
260
wheel
wheel
Ojet
D
D
d
2
1
1
cos
,
Maximum allowable angle between two successive buckets
2
Minimum number of buckets 360
z
Dr Taygun has suggested an empirical relation for z
155.0,
VCjet
wheel
d
Dz
Bucket Power Distribution
P(j)
1
2
34
5
Total
Bucket Energy Distribution
Ej,k
gHm
E
water
kk
h
Non-Orthogonal Jet Bucket Interactions : Entry
Vjet Vrel,jet
Ublade
Vjet
Vrel,jetUblade
Vjet
Vrel,jet
Non-Orthogonal Jet Bucket Interactions : Exit
Vjet
Vrel,jet
Ublade
VjetVrel,jet
Ublade
Vjet Vrel,jet
Ublade
VjetVrel,jet
Ublade
Absolute and Relative Paths of Jet : Orthogonal Interactions
e
Vjet
Ublade
Ublade
Vrel,jet,exit
e
Vjet,exit
U
Vri
Vre
UVri
Vai
Inlet Velocity Triangle
U
VreVae
Exit Velocity Triangle
Vai
Orthogonal Interactions
U
VriVai
Vre
Vae
iie e
Vai: Inlet Absolute VelocityVri: Inlet Relative VelocityVre: Exit Relative VelocityVae:Exit Absolute Velocity
i: Inlet Nozzle Angle.i: Inlet Blade Angle.e: Exit Blade Angle.i: Exit Nozzle Angle.
Actual Velocity Triangles: Pelton Bucket
1cos2max, ed k riereb VVUmP
cos
Influence of the Casing
Casing with Rectangular dome.
Casing with cylindrical dome.
Splash Water Distribution
Evaluation of Casing Perfromance
ANALYSIS OF THE LOSSES
• The losses in a Pelton turbine may be split up into the following losses:
• Losses in the jet because of friction, high turbulence, jet-divergence and gravitation.
• Losses in the runner because of friction in the buckets, entrance losses.
• Losses in the casing because of ventilation and splash water falling into the runner and/or the jet.
• Mechanical losses in the generator, bearings,...
Closing Remarks on Pelton Wheel
• The first scientifically developed concept and also patented product.
• The only one option for high heads (> 600 m)
• Best suited for low flow rates with moderate heads (240m -- 600m).
• A better choice for moderate heads with medium flow rates.
• Easy to construct and develop, as it works at constant (atmospheric) pressure.
• Low rpm at moderate or marginal heads is a major disadvantage.