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Design of Tower

The document outlines the design specifications for tower members, including details on materials, dimensions, and load calculations under various conditions. It includes multiple annexures with data on tensile strength, safety conditions, and graphical representations of the tower structure. Additionally, it provides calculations for different components such as bracings and arms, ensuring structural integrity and safety standards are met.

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0% found this document useful (0 votes)
45 views16 pages

Design of Tower

The document outlines the design specifications for tower members, including details on materials, dimensions, and load calculations under various conditions. It includes multiple annexures with data on tensile strength, safety conditions, and graphical representations of the tower structure. Additionally, it provides calculations for different components such as bracings and arms, ensuring structural integrity and safety standards are met.

Uploaded by

RushiL PateL
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF or read online on Scribd
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Design af Tower Members un ANNEXURE. 2 EARTHWIRE i. ] Stranding | Weight per | Overall Total ‘Ultimate tensile strength (kg) No, metre | Diameter] Sectional 700] 1100 1670 tka) (mm) | Area(mm® |_Nimm® | Nimm? | Nimm* 1 0.429 945 34.552 3629 | 5913 5297 2 0.523 10.50 67.248 4se7 | 7177 | 10243 3 ses 10.98 73.6468 4904 | 7348 | 11201 4 0.680 12.00 87.965 sees | e374 | 13379 8 1.163, 1575 | 148089 | 10041 | 15778 - 6 1436 so | te2801 | 12396 | 19479 - 7. 1.570 1830 | 199897 | 13555 - - 8 1.875 20.00 | 238761 | 16191 - - a 0.458 1140 141 ‘8000 - - ‘Strands Modulus of Elasticity “E” | Co-efficient of linear expansion “a” per 0° C 1 1.989 x 10° kgiom? 1.50110" 7 4.933x10 41.50 x10 19 1.893x10° 11.0010" OPTICAL FIBRE 1.52.10" 13.40x 10" cr Manual on Transmission Linas ANNEXURE-$ ‘Sheet No. 1 0f2 DESIGN LOADS (FOR SUSPENSION TOWER) RELIABILITY CONDITION (NORMAL CONDITION) (32°C & FULL WIND) ale xg 5 69 ws a 156 al aN alt ag an 1136 z 2 al as ay, eS leven a 9 no ow 1391 TOWER SECURITY CONOITION (B.W. CONDITION) (32°C & NO WIND) mm ar 7m v = 4 we im, wo w Kae SR [aK x, i my _ o A La Fld SL ist sso1a77insnsn (GW. BROKEN) COND, BROKEN) Design of Tower Member 13 ANNEXURE-3 SheetNo. 20f2 DESIGN LOADS SAFETY CONDITION (NORMAL CONDITION) (32°C & Full Wind) 5 i a a v2 al al a 12 Ue eee ASSH:6 SAFETY CONDITION (B.W. CONDITION) (32°C & NO WIND) elie : HIE 2 Nw ae 2 aS aps ge als “ AS Ee - sa ee ASSH:7 ASH: 8/9/10/8A/9A/10A (GW. STRINGING! (COND, STRINGING) Marna! on Tranzmiszion Linez a4 ANNEXURE-4 Sheet No.1 of 2 VSM AVA GRAPHICAL DIAGRAM METHOD 2M yok / Al LE \ { (SSE em ny serene Ost OOSE 802 ‘Sipe GazEZ © VD eoqo seme) jOWBTON [010] Key WZ Decign of Tower Members us ANNEXURE-¢ ‘Sheet No. 2of 2 Mioce cross = Ane mm aso cc a ete sess MULTIPLYING FACTORS 47.20 Mona on Trenzmizcion Lines BOTTOM PLAN OF BOTTOM X-ARM / [ / N\ \ EO BOS yO Vi \ y b {ALL DIENSIONS AREAL Decign af Tower Member: ut ANNEXURE- 5 SheetNo. 20f8 DESIGN OF TOWER DESIGN OF LEG MEMBER PART2 ASMA (NCI GW = 2404705) x 4566 = 1785 To = (@s0+2«175q)x 8936 = «= aT MC = (880 +2 x 1756) x 4.036 = 47726 Mo = @8683 ™ _ 60583, ‘STRESS= 2xWxCos® "2x2. 114x0-999 - ‘18261 Vertealload=Max= 219 +6x 929 — = we + (73 +6 x 356) —_— = (553) ‘Self weight of Tower = 160004 00. ‘Compression e109 “Tension 15308 L75x75x6 (L = 864/0.999 = 865) L 865 59.25 Ult. compressive strength = 2265 x 8.66 = Tri 46 19615 (on Gross Area) Safety margin over limit load (SM) S.M. = 1098 Ultimate Tensile strength = 2549 x 6.56 = 16721 SM. =1.08 (OnNet Area) 12 mm dia, Bolt-6 Nos. (Single Shear) timate Shearing strength = = 21450 Ultimate Bearing strength = 19181 SM. 12 mm dia. Bolts 6 No. (Double Shear) Ultimate shearing strenath 42900 Note: Allloads in kg and al ever arms in Metres. 4s Manual on Transmission Lines ANNEXURES ‘Sheet No.3 of 8 82 gw DESIGN OF BRACINGS 1 | | E.Fb FOR TRANS. FACE BRACINGS gh ft | i ‘ASSM-I (NO) Ay Gwe (240+ 705) x 1.520 = 1496 4 jo | 10. TC = (6506.2 1756) «1.750 284 | MO= (880 + 2 « 1756) x 1.950 2 | EF = 17264 ‘Eb FOR LONG. FACE BRACINGS | +} so [ne ! ASSM - 4 (MC BROKEN) 3 | MG = 1465 x 1.950 = 2857 j Torsion (MC) = 1465 x 4.20 6153 | i. Io AL! aso [at DESIGN OF TRANS. FACE BRACINGS ‘<° b= 1.379 1.075 4xWx Cos a= 4x2.118x = 659 +379 =p 36 stress = —EFO_ _ 17284 Logo 2 aW.tosa 650 . (Compression & Tension) 4 ke 164 260 145 x45 x4 L STS. 18051 Tmin ~ “0.7 Utimate compressive strength = 901 x 3.47 = 3126 Utimate tensile strength = 2549x2218 = S654 12. mm dia. Bolt 2 Nos. (Single Shear) Utimate Shearing strength = 7146 SM. =1.86 Utimate Bearing strength = 4888 Design of Tower Memberc 9 ANNEXURE-5 ‘Sheet No. 4 of 8 DESIGN OF LONG. FACE BRACING ‘6’ L=1379 4.W.Cosa=659 ZFb 9010 ‘STRESS = T= 1368 4.W.Cosa 6.59 Las x45 4. L__ 1379 cb. 1373 458.54 min” O87 \Utimate Compressive strength = 901 x3.47 = 3126 SM.=228 \Utimate Tensile strength = 2549 x 2218 = 5664 SM=414 12mm dia. Bolts 2 Nos. (Single Shear) ‘Utimate Shearing Strength = 7150 \Utimate Bearing Strength = 4262 SM.=311 180 Maa on Tranzmizcion Linez ANNEXURES: ‘Sheet No. 5 of 8 DESIGN OF BOTTOM X.ARM 2080 a 8 | # 3] 3 a . 2158 Stas A200 — —} Design of Lower Member Leng = 1078+ 3.125 = 3.90 STRESS IN MEMBER ASSM-10 (BC Broken) cr = S88, 2x3:125 sy = 1887x880 sess 2xoese * st = 1000390 1504 2150 ‘Compression = 5107 Tension = - L60x6Ox5 (3300/2 = 1650) Utimate Compressive Strength = 1793 x 6.75 = 10308 SM, =201 Unimate Tensile Strength = 2549 x 4.00 = 10196 SM. =~ 12 mm dia. Bolts 3 Nos. (Single shear) Utimate Shearing Strength = 10719 Utimate Bearing Strength = 9165 SM. =179 Design of Tower Members 61 ANNEXURE-S ‘Sheet No. 6of 8 DESIGN OF UPPER MEMBER length =V0.864°+ 1.057 + 3.143* = 3.426 STRESS IN MEMBER (ASSM -6) 2520 «3.426 SV =—Sypgep 74996 (Tension) LAS x45 x4 L 226 Tmed * 137 250 Ultimate Tensile strength = 2549 x 2218 = $654 12. mm dia. Bolts 3 Nos. (Single shear) Ultimate Shearing strength = 10718 Ultimate Bearing strength = 7332 SM. = 1.13 SM. = 146 DESIGN OF TRANS. BELT STRESS IN MEMBER (ASSM-10 BC Broken) 10251 st 2213 4 sys = = +3058 a = =2727 152 Marna on Trancmizcion Linez ANNEXURE-5 ‘Sheet No. 7 of 8 TRANSVERSE BELT (CONTINUED) LeSx 8526 to. 28 me rin 128 Ultimate Compressive strength = 691 x 7.44 =5141 Ultimate Tensile strength = 2543 5.317 = 13553 FOS.=- 12 mm dia. bolts 2 Nos. (Single shear) Ubimate Shearing strength = = 7146 Ultimate Bearing strength = 7382 FOS.=152 Design of LONG. BELT ‘STRESS IN MEMBER (ASSM-6) sT 102%2.150 = £18 4x3.125 sv zemm2iso =. - 1568 4x 0.864 sloo= = - SL Compression = - Tension = 1586 LAS x45 4 L 215 AL 8 ea Tmin 087 Uhimate Tensile Strength = 2549 x 2.218 = 5654 SM. =356 ‘12 mm dia. Bolts 2 Nos (Single shear) Ultimate Shearing strength = 7450 Uliimate Bearing strength = 4262 SM. = 268 Design of Tower Members 1g ANINEXURE-S ‘Sheet No. 8 of 8 DESIGN OF PLAN BRACING Length of Bracing = /2 150 > 2.150 040 STRESS IN MEMBER (ASSM-S - B.C. Broken) (1465 x42) (1465) oo e JE = 494 (Compression & Tension) 412.150 4 15 x45 04 he] LE = 47 min Tmn ~ O87 Utimate Compressive strength = 660x347 =2290 SM.= 4.63 Ultimate Tensile strength = 2549 x 2.218, =5644 SM. = 1144 12. mm dia. Bolt 1 No, (Single shear) Uttimate Shearing strength = 3573 Utimate Bearing strength = 2131 SM.=431 Numbers COMPUTER AIDED ANALYSIS Four Fi Te Line diagram showing Four Faces of Tower with Node ae lege 3/ |e 4 ORES 8 a N 8 156 MEMBER NUMBERS & NODE NUMBERS FOR SD-ANALYSIS. Manual on Trancmizzion Linas BOTTOM PLAN OF TOP CROSS ARH BOTTOM PLAN OF MIDDLE CROSS ARM ANNEXURE-6 ‘Sheet No. 2: BOTTOM PLAN OF BOTTOM CROSS ARM of 3 ISOMETRIC VIEW

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