substation design example
TRANSCRIPT
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-: Design Example :-
Design a Single Phase Bus Support for a Substation inNagpur, given the following information,
Height of Bus Centerline above foundation = 5.5 m
Schedule 40 aluminum bus = 100 mm (mass = 5.51 kg/m)
Maximum Short Circuit force = 550 N/m
Short Circuit reduction factor = 0.66
Bus Support Spacing = 6.0 m
Insulator Height (hi) = 2.0 m
Insulator Diameter (Di) = 0.28 m
Insulator Weight (Wi) = 140 kg
Basic Wind Speed (Vb) = 33 m/sec (Zone = 1) Reliability level = 2 (Return period of design loads 150 yrs)
Terrain Category = 2
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LATTICE STRUCTURE DETAILS:-
Main Leg = ISA65x65x6 @ 5.8kg/mBracing,
Inclined = ISA45x45x5 @ 3.4kg/m
Plan = ISA45x45x5 @ 3.4kg/m
Part of Structure = 04
Each Part Length = 850 mm
Inclined Length = 931 mm
Back to Back of Str. = 380 mm
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Short-Circuit Loading:-
Fsc = 6.0 m x 0.66 x 550 N/m Fsc = 2178 N
Mom @ Base = 5.5 m x 2178 N
Mom @ Base = 11979 N.m
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Wind Loading :- IS 802 (Part 1 / Sec 1) :1995,
Basic wind speed Vb = 33 m/sec
Metrological Reference wind speed VR is, VR = Vb / K0 , where K0 = 1.375 (cl. 8.2 pg 3)
VR = 33 / 1.375 = 24 m/sec
Design wind speed Vd = VR x K1 x K2, Where K1 = Risk Coeff. (cl. 8.3.1)
K1 = 1.08 (Table 2)
Where K2 = Terrain roughness coeff. (cl.8.3.2)
K2 = 1.00 (Table 3)
Design wind speed Vd = 24 x 1.08 x 1.0 = 25.92 m/sec
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Wind Loading :-Design wind pressure Pd = 0.6 Vd2 (cl. 8.4)
Pd = 0.6 x 25.92 x 25.92 = 403.11 N/sq.m
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Wind load on Conductor Fwc (cl 9.2)
Fwc = Pd x Cdc x L x d x Gc,
Where,
Cdc = Drag coeff, taken as 1.0 for conductor
L = wind span, being sum of half the span on either side of
supporting point in meters
d = diameter of cable / tube
Gc = gust response factor (Table 7) = 1.83
Fwc = 403.11 x 1.0 x 6 x 0.1 x 1.83
Fwc = 442.615 N (737.7 N/sq.m)
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Wind Loading :-
Wind load on Insulator Strings (Fwi) :- (cl 9.3)
Fwi = Cdi x Pd x Ai x Gi
Where,
Cdi = drag coeff to be taken as 1.2
Ai = 50 % of the area of insulator string projected ona plane which is parallel to the longitudinal axis of
the string
Gi = Gust response factor (Table 6) = 1.92 Fwi = 1.2 x 403.11 x 0.5 x 2 x 0.28 x 1.92
Fwi = 260.1 N (928.8 N/sq.m)
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Wind on structure Fwt = Pd x Cdt x Ae x Gt
Where,
Cdt = Drag coeff for panel under considerationagainst which the wind is blowing . Values of Cdtfor different solidity ratios are given in Table 5.
Solidity ratio () is equal to the effective area of
a frame normal to the wind direction divided bythe area enclosed by the boundary of the framenormal to the wind direction.
Solidity ratio () = Aeff / Agross
Ae = Total net surface area of the legs, bracing,cross arms and secondary members of thepanel projected normal to the face in m2
Gt = Gust response factor, Table 6
Wind Loading :-
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Solidity Ratio () = Ae / Ag
= 0.678 / 1.292 = 0.525
Drag Coeff Cdt = 2.0 (Table 5)
Gt = 1.92 (Table 6)Fwt = 403.11 x 2 x 0.678 x 1.92
Fwt = 1049.50 N (1547.92 N/sq.m)
0.678Total Net Surface Area Ae =
0.0680.0450.3843,5,7 & 9
1.292Gross Surface Area Ag = 3.4 m x 0.38 m
0.1680.0450.93142,4,6 & 8
0.4420.0653.421
Area
(sq.m)
Width
(m)
Length
(m)
NosMember
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Wind load summary :-
5363.001752.22Totals
1784.151.71049.5Wind on Structure (Fwt)
1144.444.4260.1Wind on Insulator (Fwi)
2434.415.5442.62Wind on Bus (Fwc)
Moment @
Base (N.m)
Lever
Arm (m)
Force
(N)
Description
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Earthquake Loading:-
IS 1893 (Part 1) : 2002
Design Horizontal Acceleration Coeff (Ah),
Ah = Z I / 2R * Sa/g
Z = Zone factor = Zone II = 0.10 (Table 2)I = Importance factor = 1.5 (Table 6)
R = Response reduction factor = 4 (Table 7)
Sa/g = Avg. response acceleration coeff for rock or soil
sites as given by fig 2 & Table 3 based onappropriate natural periods and damping of thestructure.
Fundamental Natural Period Ta = 0.085 h0.75
Ta = 0.085 x 3.40.75 = 0.213 secSa/g = 2.5
Hence, Ah = 0.10 x 1.5 x 2.5 / 2 x 4 = 0.047
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Earthquake Loading:-IS 1893 (Part 1) : 2002
Design Seismic Base Shear VB = Ah W
W = Seismic weight of the structure
508.92162.78Totals
141.081.7180kg x 9.81 x 0.047 =
82.99
EQ on Structure
284.024.4140kg x 9.81 x 0.047 =
64.55
EQ on Insulator
83.825.56m x 5.51 kg/m x 9.81
x 0.047 = 15.24
EQ on Bus
Moment @
Base (N.m)
L.A
(m)
Force (N)Description
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Results:-
SCF + WL :-
Force = 2178 + 1752.22 = 3930.22 N
Moment @ Base = 11979 + 5363 = 17342 N
SCF + EQ :-
Force = 2178 + 162.78 = 2340.78 N
Moment @ Base = 11979 + 508.92 = 12487.92 N
The combined loading of wind and short-circuit forcesproduce the greatest forces and moment at the base
design for this condition.Therefore seismic forces are not critical for thisstructure.
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Forces in the Member:-
Moment at the base causes tension andcompression in the chord angles.
C = Tensile or Compressive force
C = 17342 N.m / [ 2(0.380 2 x 0.0181)]
C = 25221.1 N per leg
P = Applied loadP + C = [140 x 9.81 + 6 x 54] / 4 + 25221.1
P + C = 25645.45 N per leg
Forces in bracing member shall be 25 % of the legmember.
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Thank you..