STRUCTURAL CALCULATION
|
|
- Avis Morrison
- 6 years ago
- Views:
Transcription
1 STRUCTURAL CALCULATION Project: Report: BATLab, Geneva Curtan wall System mscellaneous checks Report-No.: M FE rev1 Lndner Fassaden GmbH Swtzerland Offce In der Schappe CH 4144 ARLESHEIM Swtzerland Tel: +41 (0) Fax: +41 (0) Sgnature: 17. October 2012 Larry Castañeda BSc.C.E., MSc. Structural Engneerng FE Structural desgn Page 1 of 37 M FE1502-0rev1.doc
2 Document revson: Revson Date Modfcaton 0 17 August 2012 Issue for Approval 1 17 October Spacng of glass screen T-mullon s set to 1.05m (max) - Corner mullon added for blnd gude ral fxng Contents 1 References Document references Drawng references Software used Desgn parameters Buldng materals Loads Deflecton lmts General groupng: Lev General groupng: Lev Glazed element Outer-nner profle shear connector Spandrel glazng Press L-Mullon Glass DL holder Top fxng: DL+WL Tor and bottom fxng: WL only Spandrel panel Horzontal metal panel: 3mm / EN AW-5005 H Horzontal panel claddng types A.301, A.401, A.551 & A Horzontal panel claddng types A.552 & A Vertcal ral channel: mm / EN AW-5754 H Corner elements Corner Levels 0 & Blnds Levels 0 & Screw channel test FE Structural desgn Page 2 of 37 M FE1502-0rev1.doc
3 1 References 1.1 Document references Norms and standards [1] SIA 260:2003, Bass of Structural Desgn. [2] SIA 261:2003, Actons on structures. [3] EN :2007, Eurocode 9 Desgn of alumnum structures Part 1-1: General structural rules. [4] EN :2007, Eurocode 9 Desgn of alumnum structures Part 1-4: Cold-formed structural sheetng. [5] EN 13830:2003, Curtan Wallng Product Standard [6] EN 14024:2004, Metal profles wth thermal barrer Mechancal performance Requrements, proof and tests for assessment. [7] GBD Lab GmbH. Proflsystem Luxemburg Belastungsversuche Schraubkanal Project specfc documents [8] Lndner. M FE1501-0, Curtan wall System profles. [9] Emmer Pfennnger Partner AG. Soumsson de facade et de protecton solare. 13 October Drawng references [10] Lndner FA rev--, Coupe de prncpe Facade prncpale laboratores [11] Lndner FA rev--, Coupe vertcal de prncpe Facade prncpale [12] Lndner FA rev--, Coupe horz. de prncpe Facade prncpale au travers du verre vson 1.3 Software used [13] SCIA Engneer 2008, an analyss, desgn and detalng of structures wth lnear, non-lnear, FEM and 2 nd order calculaton capabltes, s used n the structural calculatons. FE Structural desgn Page 3 of 37 M FE1502-0rev1.doc
4 2 Desgn parameters 2.1 Buldng materals Mnmum propertes of materals used. Member Grade Modulus of elastcty E [N/mm 2 ] Alumnum: γ M0,M1 = 1.0; γ M2 = 1.25 Yeld or 0.2% proof strength, f o [N/mm 2 ] Tensle strength f u [N/mm 2 ] Extruded sectons EN AW-6060 T Sheets EN AW-5005 H Welded sheets EN AW-5754 H Stanless steel: γ M0,M1 = 1.0; γ M2 = 1.25 Sheets and plates Bolts and screws A2-70 or C Loads Dead load, DL The self-weght of the element and glazng s consdered n the analyss wth an ncremental factor of Wnd load, WL In accordance wth specfcaton [9], the followng wnd loads are consdered: Typcal calddng w p,k = kn/m 2 Net pressure w s,k = kn/m 2 Net sucton Ranscreen panels Wnd loads to the ranscreen panels are determned consderng pressure on walls for mult-skn acc. to EN Cl for o and excludng the ±0.20 kn/m 2 nternal pressure. w p,k = 2/3 ( ) = kn/m 2 Net pressure on outer skn w s,k = mn{1/3 ( ); 0.6} = kn/m 2 Net sucton on outer skn w o,k = 1/3 ( ) = kn/m 2 Net corner local sucton on outer skn External blnds w o,k = kn/m 2 Net corner local sucton on outer skn Imposed/lve load, IL In accordance wth specfcaton [9], the followng mposed loads are consdered: Barrer loadngs Horzontal lne load, q k = 0.80 kn/m - appled 1.20 m above fnshed floor Mantenance load Pont load, Q k = 0.50 kn - appled on a square of 100mm sdes FE Structural desgn Page 4 of 37 M FE1502-0rev1.doc
5 2.3 Deflecton lmts Deflecton lmts for the desgn of system framng members and components: Deflecton mode Allowable deflecton, δ allow [mm] Reference Framng members Normal H/200 or 15 mm Performance requrement [9] In-plane L/500 or 3mm EN Framng support Inward/outward under wnd load ± L/150 SIA 233 Cl Claddng panel Inward under wnd pressure + L/40 Outward under wnd sucton - L/70 DIBt Zulassung Nr. Z FE Structural desgn Page 5 of 37 M FE1502-0rev1.doc
6 2.4 General groupng: Lev 0-1 A.552, A.701 & A.702 A.301, A.401 & A General groupng: Lev 1-9 A.552 & A.702 A.552, A.701 & A.702 A.301, A.401 & A.551 FE Structural desgn Page 6 of 37 M FE1502-0rev1.doc
7 3 Glazed element 3.1 Outer-nner profle shear connector Vertcal Secton Detals t = 4mm for Claddng types A.301, A.401 & A.551 t = 6mm for Claddng types A.552, A.701 & A.702 Claddng types A.301, A.401 & A.551 Claddng types A.552, A.701 & A mm 50mm / w/ 2 EN ISO Ø4.8mm RIVETS mm 50mm / w/ 3 EN ISO Ø4.8mm RIVETS FE Structural desgn Page 7 of 37 M FE1502-0rev1.doc
8 3.1.1 Check compresson part: EN AW-6060 T6 f o = 140 N/mm 2 N c,rd = /1.1 = 8.02 kn N cr = /(2.0 67) 2 = 5.42 kn λ = (63 140/5420) = 1.28 Ø = 0.5[1+0.35( ) ] = 1.47 χ = 1/[1.47+( )] = 0.46 N b,rd = = 3.69 kn Claddng types A.301, A401 & A.551 (b 1 + b 2 )/2 = ( )/2 = 0.86 m N Ed = /2 = 1.67 kn 0.40 < 1.00 Claddng types A.552, A.701 & A.702 (b 1 + b 2 )/2 = ( )/2 = 1.87 m N Ed = /2 = 3.64 kn 0.99 < Check angle: t 50mm / Claddng types A.301, A401 & A.551 t = 4.0 mm M Rd = /4 210/1.0 = 42.0 kn mm M Ed = = 41.8 kn mm 0.99 < 1.00 Claddng types A.552, A.701 & A.702 t = 6.0 mm M Rd = /4 210/1.0 = kn mm M Ed = = 91.0 kn mm 0.88 < Check rvets: EN ISO Ø4.8mm From techncal data, F t,rd = 2.80/1.33 = 2.10 kn < - governng for tenson! F v,rd = 2.02/1.33 = 1.52 kn Accordng to EN , F p,rd = /1.25 = 3.32 kn F b,rd = 1.5 ( ) 170/1.25 = 1.26 kn < - governng for shear! Claddng types A.301, A401 & A.551 F t,ed = /20/2 = 1.25 kn 0.60 < 1.00 F v,ed = 1.46/2 = 0.73 kn 0.58 < 1.00 Claddng types A.552, A.701 & A.702 F t,ed = /20/3 = 1.82 kn 0.87 < 1.00 F v,ed = 3.64/3 = 1.21 kn 0.96 < 1.00 FE Structural desgn Page 8 of 37 M FE1502-0rev1.doc
9 4 Spandrel glazng ADDITIONAL INTERMEDIATE L-MULLION WITH WL RESTRAINT/FIXING b 1 + b 2 + b S = 1.05 m (max) 4.1 Press L-Mullon RAIL CHANNEL: U mm / EN AW-5754 H14 A = 2.31 cm Iy = 3.58 cm4 Iz = 1.61 cm4 Wy = 1.24 cm3 DIN 933 M10 100mm / A2-70 W/ DOUBLE NUT OR LOCTITE SG500-8mm 6mm (SYMMETRICAL) T mm / EN AW-6060 T6 FE Structural desgn Page 9 of 37 M FE1502-0rev1.doc
10 4.1.1 Check T mm / EN AW-6060 T6 q w = = 0.88 N/mm Stress M Rd = /1.1 = kn mm M Ed = /8 = kn mm 0.60 < 1.00 Deflecton δ zul = 760/200 = 3.8 mm δ max = /( ) = 1.52 mm 0.40 < Structural sealant: SG500 σ des = 0.14 N/mm 2 Desgn short term tensle stress h c = = 6.0 mm Effectve bte σ = 0.88/(2 6) = 0.07 N/mm < Glass DL holder b DL,max = ( )/2 = 2.81 m F z,d = = 0.85 kn T mm EN AW-6060 T6 Check mm 40mm / EN AW-6060 T6 N Rd = /1.1 = kn M Rd = /4 140/1.1 = kn mm M Ed = 0.85 (11.4-3/2) = 8.42 kn mm 0.85/ /11.45 = 0.79 < mm 40mm EN AW-6060 T6 Check 2 DIN 7982 ST4.2 13mm / A2-70 or F t,rd = /1.25 = 3.06 kn F o,rd = 0.95 ( ) 170/1.25 = 0.79 kn <- governs n tenson! F v,rd = /1.25 = 2.08 kn F b,rd = (3/2) 170/1.25 = 1.28 kn <- governs n shear! Desgn forces, F t,ed = /10/2 = 0.48 kn 0.61 < 1.00 F v,ed = 0.85/2 = 0.42 kn 0.33 < = 0.94 < DIN 7982 ST4.2 13mm / FE Structural desgn Page 10 of 37 M FE1502-0rev1.doc
11 4.3 Top fxng: DL+WL b DL max = ( )/2 = 2.81 m F z,d = 1.35( )0.9 = 0.87 kn F y,d = [ /2 0.9(0.9/2-0.1) ]/0.76 = 0.33 kn F d = ( ) = 0.93 kn T mm EN AW-6060 T Check T mm / EN AW-6060 T6 Lp shear V y,rd = 0.8/ /1.1 = 1.23 kn 0.63 < 1.00 V z,rd = 0.8/ /1.1 = 4.06 kn 0.21 < 1.00 Local bendng of flanges b eff = = 75.0 mm M Rd = /4 140/1.1 = kn mm M Ed = /2 (40-8)/2 = kn mm 0.52 < 1.00 DIN 933 M10 100mm A Check bolt: DIN 933 M10 100mm / A2-70 Bearng of bolt on ral channel, α b = 14.8/(3 12) = 0.41 F b,rd = /1.25 = 3.54 kn F v,ed = 1.03(62+5)/75 = 0.92 kn 0.26 < 1.00 Bendng of bolt, M Rd = /1.0 = kn mm M Ed = 1.03(13+5)(62-5)/75 = kn mm 0.39 < Tor and bottom fxng: WL only F y,d = (0.9/2-0.04)/0.76 = 0.64 kn Check T mm / EN AW-6060 T6 Lp shear V y,rd = 0.8/ /1.1 = 1.76 kn < 2F y,d Hgh shear! f o,v = 1-(2 0.93/1.76-1) 2 = 0.99 M Rd = /4 140/1.1 = 9.45 kn mm Consderng tolerance and thermal movements of 2mm, M Ed = 0.64 (5+2) = 4.49 kn mm 0.47 < 1.00 T mm EN AW-6060 T6 Local bendng of flanges b eff = 4 22 = 88.0 mm M Rd = /4 140/1.1 = kn mm M Ed = 0.64/2 (40-8)/2 = 5.12 kn mm 0.20 < 1.00 DIN 933 M10 100mm A2-70 FE Structural desgn Page 11 of 37 M FE1502-0rev1.doc
12 4.4.2 Check bolt: DIN 933 M10 100mm / A2-70 Bearng of bolt on ral channel, α b = 14.8/(3 12) = 0.41 F b,rd = /1.25 = 3.54 kn F v,ed = 0.93(62+5)/75 = 0.83 kn 0.23 < 1.00 Bendng of bolt, M Rd = /1.0 = kn mm M Ed = 0.93(13+5)(62-5)/75 = kn mm 0.35 < 1.00 FE Structural desgn Page 12 of 37 M FE1502-0rev1.doc
13 5 Spandrel panel 5.1 Horzontal metal panel: 3mm / EN AW-5005 H14 Claddng types A.301, A.401, A.551 & A.701 b 1 + b 2 + b 1 F 2 F 2 F 2 F 2 370, 625 F 1 F 3 F 3 F 1 Claddng types A F 2 F 2 F 2 F 2 F 2 370, 625 F 3 F 3 F 1 F 1 F 3 Claddng types A.702 ADDITIONAL INTERMEDIATE FIXINGS F 2 F 2 F 2 F 2 F 2 370, 625 F 1 F 3 F 3 F 3 F 1 FE Structural desgn Page 13 of 37 M FE1502-0rev1.doc
14 ADDITIONAL INTERMEDIATE FIXINGS 5.2 Horzontal panel claddng types A.301, A.401, A.551 & A Structural model Loads LC1: Wnd pressure LC2: Wnd sucton LC3: Imposed load 1 q L = 0.5/( ) = 50.0 kn/m 2 mposed load FE Structural desgn Page 14 of 37 M FE1502-0rev1.doc
15 v LC4: Imposed load 2 v Non-lnear load combnatons Stress check f o = N/mm 2 Desgn resstance, σ general,rd = 120/1.1 = N/mm 2 General stress resstance From analyss results, σ max = 81.9 N/mm < 1.00 Stresses: NC201 FE Structural desgn Page 15 of 37 M FE1502-0rev1.doc
16 Project: BATLab, Geneva Stresses: NC202 Stresses: NC203 v Stresses: NC204 FE Structural desgn Page 16 of 37 M FE1502-0rev1.doc
17 5.2.4 Deflecton check Servceablty lmt, δ zul,edge = 1955/175 = mm δ zul,local = 625/40 = mm δ zul,total = = mm From structural analyss, due to dead and wnd load NC101 & NC102, δ edge = 4.43 mm 0.40 < 1.00 δ local = ( )/2 = 7.38 mm 0.47 < 1.00 δ max = mm 0.40 < 1.00 From structural analyss, due to dead and mposed load NC103 & NC104, δ edge = 4.47 mm 0.40 < 1.00 δ local = ( )/2 = mm 0.66 < 1.00 δ max = mm 0.53 < 1.00 Deflecton: NC101 Deflecton: NC102 FE Structural desgn Page 17 of 37 M FE1502-0rev1.doc
18 Project: BATLab, Geneva Deflecton: NC103 v Deflecton: NC104 FE Structural desgn Page 18 of 37 M FE1502-0rev1.doc
19 5.2.5 Reacton forces Reacton forces: NC201 Reacton forces: NC202 FE Structural desgn Page 19 of 37 M FE1502-0rev1.doc
20 5.2.6 Check fxng type F1 F y,d = 0.18 kn F z,d = 0.29 Kn Check angle: mm 50mm / EN AW-6060 T6 beff = 4 8 = 32.0 mm M Rd = /4 140/1.1 = 4.07 kn mm From structural analyss, M Ed = /19 8 = 3.07 kn mm 0.75 < 1.00 Check self-tappng screw: 1 DIN ST / A2-70 or F t,rd = /1.25 = 4.14 kn F o,rd = 0.95 ( ) 240/1.25 = 4.47 kn F p,rd = (9.5/22) /1.25 = 0.61 kn <- governs n tenson! F v,rd = /1.25 = 2.81 kn F b,rd = /1.25 = 1.96 kn <- governs n shear! From structural analyss, F t,ed = /19 = 0.41 kn 0.68 < 1.00 F v,ed = F z,d = 0.18 kn 0.09 < = 0.77 < ISO Ø4.0 L / AlMg2.5 3mm / EN AW 5005 H14 Check blnd rvets: 4 ISO Ø4.0 L / AlMg2.5 From techncal data, F t,rd = 1.55/1.25 = 1.24 kn <- governs! F v,rd = 1.00/1.25 = 0.80 kn <- governs! Accordng to EN , F p,rd = /1.25 = 3.53 kn F b,rd = /1.25 = 1.96 kn From structural analyss, F t,ed = /30 = 0.05 kn 0.04 < 1.00 F v,ed = 0.29/ /30 = 0.26 kn 0.33 < / = 0.36 < 1.00 DIN 7981 ST4.8 13/ mm 50mm EN AW-6060 T6 EN AW-5754 H14 FE Structural desgn Page 20 of 37 M FE1502-0rev1.doc
21 5.2.7 Check fxng type F2 F y,d = 0.51 kn 3mm / EN AW 5005 H14 Check angle: mm 35mm / EN AW-6060 T6 beff = 4 (10-3) = 28.0 mm M Rd = /4 140/1.1 = 8.02 kn mm From structural analyss, M Ed = 0.51 (10-3) = 3.57 kn mm 0.44 < 1.00 Check self-tappng screw: 1 DIN ST / A2-70 or F t,rd = /1.25 = 4.14 kn F p,rd = (9.5/22) = 0.80 kn <- governs n tenson! From structural analyss, F t,ed = F y,d = 0.51 kn 0.64 < Check fxng type F3 F y,d = 0.57 kn Check self-tappng screw: 1 DIN ST / A2-70 or F t,rd = /1.25 = 4.14 kn F o,rd = 0.95 ( ) 170/1.25 = 0.68 kn <- governs! From structural analyss, F t,ed = F y,d = 0.57 kn 0.84 < 1.00 DIN 7981 ST4.8 13/ mm 50mm EN AW-6060 T6 DIN ST4.8 13/ w/ S.St. SLEEVE THROUGH VERTICAL SLOT MULLION PROFILE EN AW-6060 T6 FE Structural desgn Page 21 of 37 M FE1502-0rev1.doc
22 5.3 Horzontal panel claddng types A.552 & A Structural model Loads LC1: Wnd pressure LC2: Wnd sucton LC3: Imposed load 1 q L = 0.5/( ) = 50.0 kn/m 2 mposed load FE Structural desgn Page 22 of 37 M FE1502-0rev1.doc
23 v LC4: Imposed load 2 v Non-lnear load combnatons Stress check f o = N/mm 2 Desgn resstance, σ general,rd = 120/1.1 = N/mm 2 General stress resstance From analyss results, due to dead and wnd load NC201 & NC202, σ max = 83.0 N/mm < 1.00 From analyss results, due to dead and wnd load NC203 & NC204, σ max = 68.3 N/mm < 1.00 Stresses: NC201 FE Structural desgn Page 23 of 37 M FE1502-0rev1.doc
24 Project: BATLab, Geneva Stresses: NC202 Stresses: NC203 v Stresses: NC Deflecton check Servceablty lmt, δ zul,edge = 1770/200 = 8.85 mm δ zul,local = 625/40 = mm δ zul,total = = mm From structural analyss, due to dead and wnd load NC101 & NC102, δ edge = 3.28 mm 0.37 < 1.00 δ local = 9.61-( )/2 = 7.06 mm 0.45 < 1.00 δ max = 9.61 mm 0.39 < 1.00 FE Structural desgn Page 24 of 37 M FE1502-0rev1.doc
25 From structural analyss, due to dead and mposed load NC103 & NC104, δ edge = 3.56 mm 0.40 < 1.00 δ local = ( )/2 = mm 0.65 < 1.00 δ max = mm 0.54 < 1.00 Deflecton: NC101 Deflecton: NC102 Deflecton: NC103 FE Structural desgn Page 25 of 37 M FE1502-0rev1.doc
26 v Project: BATLab, Geneva Deflecton: NC Reacton forces Reacton forces: NC201 Reacton forces: NC202 FE Structural desgn Page 26 of 37 M FE1502-0rev1.doc
27 5.3.6 Check fxng type F1 F y,d = 0.27 kn F z,d = 0.25 Kn Check angle: mm 50mm / EN AW-6060 T6 beff = 4 8 = 32.0 mm M Rd = /4 140/1.1 = 4.07 kn mm From structural analyss, M Ed = /19 8 = 3.07 kn mm 0.75 < 1.00 Check self-tappng screw: 1 DIN ST / A2-70 or F t,rd = /1.25 = 4.14 kn F o,rd = 0.95 ( ) 240/1.25 = 4.47 kn F p,rd = (9.5/22) /1.25 = 0.61 kn <- governs n tenson! F v,rd = /1.25 = 2.81 kn F b,rd = /1.25 = 1.96 kn <- governs n shear! From structural analyss, F t,ed = /19 = 0.38 kn 0.63 < 1.00 F v,ed = F z,d = 0.25 kn 0.13 < = 0.76 < ISO Ø4.0 L / AlMg2.5 3mm / EN AW 5005 H14 Check blnd rvets: 4 ISO Ø4.0 L / AlMg2.5 From techncal data, F t,rd = 1.55/1.25 = 1.24 kn <- governs! F v,rd = 1.00/1.25 = 0.80 kn <- governs! Accordng to EN , F p,rd = /1.25 = 3.53 kn F b,rd = /1.25 = 1.96 kn From structural analyss, F t,ed = /30 = 0.07 kn 0.06 < 1.00 F v,ed = 0.27/ /30 = 0.30 kn 0.38 < / = 0.58 < 1.00 DIN 7981 ST4.8 13/ mm 50mm EN AW-6060 T6 EN AW-5754 H14 FE Structural desgn Page 27 of 37 M FE1502-0rev1.doc
28 5.3.7 Check fxng type F2 F y,d = 0.49 kn 3mm / EN AW 5005 H14 Check angle: mm 35mm / EN AW-6060 T6 beff = 4 (10-3) = 28.0 mm M Rd = /4 140/1.1 = 8.02 kn mm From structural analyss, M Ed = 0.49 (10-3) = 3.43 kn mm 0.43 < 1.00 Check self-tappng screw: 1 DIN ST / A2-70 or F t,rd = /1.25 = 4.14 kn F p,rd = (9.5/22) = 0.80 kn <- governs n tenson! From structural analyss, F t,ed = F y,d = 0.49 kn 0.61 < Check fxng type F3 F y,d = 0.56 kn Check self-tappng screw: 1 DIN ST / A2-70 or F t,rd = /1.25 = 4.14 kn F o,rd = 0.95 ( ) 170/1.25 = 0.68 kn <- governs! From structural analyss, F t,ed = F y,d = 0.56 kn 0.82 < 1.00 DIN 7981 ST4.8 13/ mm 50mm EN AW-6060 T6 DIN ST4.8 13/ w/ S.St. SLEEVE THROUGH VERTICAL SLOT MULLION PROFILE EN AW-6060 T6 FE Structural desgn Page 28 of 37 M FE1502-0rev1.doc
29 5.4 Vertcal ral channel: mm / EN AW-5754 H14 The ral channel supports the spandrel glass va press angles and the horzontal metal panel. The most onerous condton s checked usng the loads and dmenson of claddng type A Structural model 5mm / EN AW-5754 H14 3mm / EN AW-5754 H14 5mm / EN AW-5754 H Loads Consderng claddng type A.702, P D1 = /2 = 0.67 kn 10mm lam. glass P D2 = /2 = 0.21 kn 3mm alu. sheet P W1 = /8 = 0.23 kn wnd load on glass P W2 = /4 = 0.09 kn wnd load on vertcal metal panel P W2 = /4 = 0.14 kn wnd load on upper fxng of horzontal metal panel M W = = 1.4 kn mm moment due to eccentrcty of P W2 P W3 = /4 = 0.19 kn wnd load on lower fxng of horzontal metal panel q L = 0.50 kn mposed load FE Structural desgn Page 29 of 37 M FE1502-0rev1.doc
30 LC1: Dead Load LC2: Wnd load, pressure LC3: Imposed load Non-lnear Load combnatons Stress check f o = N/mm 2 ρ o,haz = 0.53 σ zul = 190/1.1 = N/mm 2 σ zul,haz = /1.1 = N/mm 2 From structural analyss, σ max = 84.2 N/mm < 1.00 σ max,haz = 76.6 N/mm < 1.00 FE Structural desgn Page 30 of 37 M FE1502-0rev1.doc
31 Project: BATLab, Geneva Stresses: NC201 Stresses: NC202 FE Structural desgn Page 31 of 37 M FE1502-0rev1.doc
32 5.4.4 Deflecton check Servceablty lmt, δ zul = 1386/200 = 6.93 mm From structural analyss, δ max = 2.98 mm 0.43 < 1.00 Deflecton: NC101 Deflecton: NC102 FE Structural desgn Page 32 of 37 M FE1502-0rev1.doc
33 5.4.5 Bottom fxng angle Check angle: mm 60mm / EN AW-6060 T6 N Rd = /1.1 = kn M Rd = /4 140/1.1 = kn mm From structural analyss, N Ed = = 0.73 kn 0.02 < 1.00 M Ed = 0.70(60-4/2) (20-4/2) = kn mm 0.86 < = 0.88 < mm 60mm EN AW-6060 T6 Check self-drllng crews: 2 DIN 7504 K-ST / A2-70 or F t,rd = /1.25 = 4.14 kn F o,rd = /1.25 = 2.12 kn <- governs! From structural analyss, F t,ed = 0.70 kn 0.33 < 1.00 Check blnd rvets: 4 ISO Ø4.8 L / AlMg2.5 From techncal data, F t,rd = 2.22/1.25 = 1.78 kn <- governs! F v,rd = 1.40/1.25 = 1.12 kn <- governs! Accordng to EN , F p,rd = /1.25 = 3.15 kn F b,rd = /1.25 = 1.76 kn From structural analyss, F t,ed = ( )/25/2 = 0.85 kn 0.48 < 1.00 F v,ed = ( )/4 = 0.18 kn 0.16 < DIN 7504-K ST4.8 22/ w/ S.St. SLEEVE THROUGH VERTICAL SLOT 4 ISO Ø4.8 L / AlMg2.5 FE Structural desgn Page 33 of 37 M FE1502-0rev1.doc
34 6 Corner elements 6.1 Corner Levels 0 & SSG Check Materal: SG-500 σ des = 0.14 N/mm 2 τ des = N/mm 2 Structural bte Consder 2mm tolerance and neckng of slcone, b = m τ = /2 = 1.41 N/mm h c 1.41/ = mm Sealant thckness ε des = 12.5 % s = [ ]1948 = 2.28 mm 5mm / EN AW-5754 H14 e 2.28/ ( ) = 4.42 mm mm / EN AW-6060 T6 Provde: Structural sealant SG mm 6mm 2 DIN 7982 ST4.8 L / Corner mullon: mm / EN AW-6060 T6 f o = 140 N/mm 2 N c,rd = /1.1 = kn N cr = /( ) 2 = kn λ = ( /3415) = 3.53 Ø = 0.5[1+0.35( ) ] = 7.28 χ = 1/[7.28+( )] = 0.07 N b,rd = = 2.71 kn Compresson force on the mullon, D 1 = 0.15( )/ = 1.04 kn Transom profle and metal sheet + blnds D 2 = ( )/2 = 0.23 kn Insulaton N Ed = 1.35 ( ) = 1.71 kn 0.63 < Fxng screws: 2 DIN 7982 ST4.8 L / A2-70 or Bearng on welded end plate 5mm/EN AW-5754 H14 f u,haz = = N/mm 2 α b = 8.6/(3 4.8) = 0.60 F b,rd = (5-3.6/2) 150.1/1.25 = 1.66 kn F v,ed = 1.5( / /2)/2 = 1.41 kn 0.85 < 1.00 FE Structural desgn Page 34 of 37 M FE1502-0rev1.doc
35 6.2 Blnds Levels 0 & 1 SHS60 5 / EN AW-6060 T6 M5 L / 350mm O.C. MAX. 4 M6 L / A2-70 w/ BLIND NUT RIVET / ALU. BENT PL 60 5MM / EN AW-6060 T6 8 Ø4.8 / A2 STAINLESS STEEL RIVETS Blnd ral Ral M Ed = / /8 = kn mm δ allow = 350/150 = 2.33 mm Alu. profle M Rd = /1.1 = kn mm 0.57 < 1.00 δ max = / /( ) = 0.88 mm 0.38 < 1.00 Fxng screws F v,ed = / = 1.39 kn F t,ed = /7.1 = 3.85 kn FE Structural desgn Page 35 of 37 M FE1502-0rev1.doc
36 M5 L / 350 mm O.C. F v,rd = /1.25 = 3.97 kn F b,rd = ( /2) 170/1.25 = 2.50 kn 0.56 < 1.00 F t,rd = /1.25 = 5.00 kn F p,rd = ( /2) 170/1.25 = 5.02 kn d τ = ( ) 30.8 = 4.95 mm F o,rd = /1.25= 3.91 kn 0.98 < Corner mullon Box secton M Ed = / /8 = kn mm δ allow =2025/90 = 22.5 mm SHS 60 5 / EN AW-6060 T6 M Rd = /1.1 = kn mm 0.57 < 1.00 δ max = / /( ) = mm 0.66 < 1.00 Screw fxng to bracket H Ed = /2 (2.025/2+0.15) = 4.61 kn F v,ed = /21/2 = 4.61 kn F t,ed = /21/2 = 2.30 kn Max. shear and max. tenson does not occur at the same tme 4 M6 / A2-70 F v,rd = /1.25 = 5.63 kn 0.82 < 1.00 F b,rd = (5-3.0/2) 170/1.25 = 6.12 kn F t,rd = /1.25 = 7.10 kn 0.32 < 1.00 F p,rd = (5-3.0/2) 170/1.25 = 7.38 kn Rvets fxng to element transom F v,ed = /33/4 = 1.54 kn F t,ed = /33/4 = 0.38 kn 8 Ø4.8mm / A2 stanless steel F v,rd = 4.40/1.25 = 3.52 kn F b,rd = /1.25 = 1.96 kn 0.78 < 1.00 F t,rd = 6.10/1.25 = 4.88 kn F p,rd = /1.25 = 0.47 kn 0.81 < 1.00 FE Structural desgn Page 36 of 37 M FE1502-0rev1.doc
37 7 Screw channel test FE Structural desgn Page 37 of 37 M FE1502-0rev1.doc
Module 11 Design of Joints for Special Loading. Version 2 ME, IIT Kharagpur
Module 11 Desgn o Jonts or Specal Loadng Verson ME, IIT Kharagpur Lesson 1 Desgn o Eccentrcally Loaded Bolted/Rveted Jonts Verson ME, IIT Kharagpur Instructonal Objectves: At the end o ths lesson, the
More informationAPOLLO SCAFFOLDING SERVICES LTD SPIGOT CONNECTION TO EUROCODES DESIGN CHECK CALCULATIONS
Alan White Design APOLLO SCAFFOLDING SERVICES LTD SPIGOT CONNECTION TO EUROCODES DESIGN CHECK CALCULATIONS Alan N White B.Sc., M.Eng., C.Eng., M.I.C.E., M.I.H.T. JUL 2013 Somerset House 11 Somerset Place
More informationPlease review the following statement: I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.
Please revew the followng statement: I certfy that I have not gven unauthorzed ad nor have I receved ad n the completon of ths exam. Sgnature: Instructor s Name and Secton: (Crcle Your Secton) Sectons:
More informationCOMPOSITE BEAM WITH WEAK SHEAR CONNECTION SUBJECTED TO THERMAL LOAD
COMPOSITE BEAM WITH WEAK SHEAR CONNECTION SUBJECTED TO THERMAL LOAD Ákos Jósef Lengyel, István Ecsed Assstant Lecturer, Professor of Mechancs, Insttute of Appled Mechancs, Unversty of Mskolc, Mskolc-Egyetemváros,
More informationORIGIN 1. PTC_CE_BSD_3.2_us_mp.mcdx. Mathcad Enabled Content 2011 Knovel Corp.
Clck to Vew Mathcad Document 2011 Knovel Corp. Buldng Structural Desgn. homas P. Magner, P.E. 2011 Parametrc echnology Corp. Chapter 3: Renforced Concrete Slabs and Beams 3.2 Renforced Concrete Beams -
More informationIncrease Decrease Remain the Same (Circle one) (2 pts)
ME 270 Sample Fnal Eam PROBLEM 1 (25 ponts) Prob. 1 questons are all or nothng. PROBLEM 1A. (5 ponts) FIND: A 2000 N crate (D) s suspended usng ropes AB and AC and s n statc equlbrum. If θ = 53.13, determne
More informationDUE: WEDS FEB 21ST 2018
HOMEWORK # 1: FINITE DIFFERENCES IN ONE DIMENSION DUE: WEDS FEB 21ST 2018 1. Theory Beam bendng s a classcal engneerng analyss. The tradtonal soluton technque makes smplfyng assumptons such as a constant
More informationFUZZY FINITE ELEMENT METHOD
FUZZY FINITE ELEMENT METHOD RELIABILITY TRUCTURE ANALYI UING PROBABILITY 3.. Maxmum Normal tress Internal force s the shear force, V has a magntude equal to the load P and bendng moment, M. Bendng moments
More informationStrength Requirements for Fore Deck Fittings and Equipment
(Nov 2002) (Rev.1 March 2003) (Corr.1 July 2003) (Rev.2 Nov 2003) (Rev.3 July 2004) (Rev.4 Nov 2004) (Rev.5 May 2010) Strength Requrements for Fore Deck Fttngs and Equpment 1. General 1.1 Ths UR S 27 provdes
More informationTHE EFFECT OF BEAM TO COLUMN CONNECTION IN ARC PORTAL FRAME
THE EFFECT OF BEAM TO COLUMN CONNECTON N ARC PORTAL FRAME Asko Keronen Rakenteden Mekankka, Vol. 26 No 2 1993, ss. 35-5 SUMMARY A full scale rc (renforced concrete) portal frame has been bult n order to
More informationME 307 Machine Design I. Chapter 8: Screws, Fasteners and the Design of Nonpermanent Joints
Dr.. zz Bazoune Chapter 8: Screws, Fasteners and the Desgn of Nonpermanent Jonts Dr.. zz Bazoune Chapter 8: Screws, Fasteners and the Desgn of Nonpermanent Jonts CH-8 LEC 35 Slde 2 Dr.. zz Bazoune Chapter
More informationI have not received unauthorized aid in the completion of this exam.
ME 270 Sprng 2013 Fnal Examnaton Please read and respond to the followng statement, I have not receved unauthorzed ad n the completon of ths exam. Agree Dsagree Sgnature INSTRUCTIONS Begn each problem
More informationPlease review the following statement: I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.
ME 270 Sprng 2014 Fnal Exam NME (Last, Frst): Please revew the followng statement: I certfy that I have not gven unauthorzed ad nor have I receved ad n the completon of ths exam. Sgnature: INSTRUCTIONS
More information9.2 Seismic Loads Using ASCE Standard 7-93
CHAPER 9: Wnd and Sesmc Loads on Buldngs 9.2 Sesmc Loads Usng ASCE Standard 7-93 Descrpton A major porton of the Unted States s beleved to be subject to sesmc actvty suffcent to cause sgnfcant structural
More informationSAMPLE PROJECT IN THE MIDDLE EAST DOCUMENT NO. STR-CALC UNITISED CURTAIN WALL 117 ENGINEER PROJECT. Pages REVISION TITLE
PROJECT ENGINEER DOCUMENT NO. STR-CALC-548 0 REVISION TITLE Pages UNITISED CURTAIN WALL 117 UNITISED CURTAIN WALL 2 of 117 Table of Contents 1 Summary 3 2 Basic Data 4 2.1 Standards and References 4 2.2
More informationApplication nr. 7 (Connections) Strength of bolted connections to EN (Eurocode 3, Part 1.8)
Application nr. 7 (Connections) Strength of bolted connections to EN 1993-1-8 (Eurocode 3, Part 1.8) PART 1: Bolted shear connection (Category A bearing type, to EN1993-1-8) Structural element Tension
More informationMECHANICS OF MATERIALS
Fourth Edton CHTER MECHNICS OF MTERIS Ferdnand. Beer E. Russell Johnston, Jr. John T. DeWolf ecture Notes: J. Walt Oler Texas Tech Unversty Stress and Stran xal oadng Contents Stress & Stran: xal oadng
More informationPlease review the following statement: I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.
ME 270 Summer 2014 Fnal Exam NAME (Last, Frst): Please revew the followng statement: I certfy that I have not gven unauthorzed ad nor have I receved ad n the completon of ths exam. Sgnature: INSTRUCTIONS
More informationMade by SMH Date Aug Checked by NRB Date Dec Revised by MEB Date April 2006
Job No. OSM 4 Sheet 1 of 8 Rev B Telephone: (0144) 45 Fax: (0144) 944 Made b SMH Date Aug 001 Checked b NRB Date Dec 001 Revised b MEB Date April 00 DESIGN EXAMPLE 9 - BEAM WITH UNRESTRAINED COMPRESSION
More informationStructural Dynamics and Earthquake Engineering
Structural Dynamcs and Earthuake Engneerng Course 9 Sesmc-resstant desgn of structures (1) Sesmc acton Methods of elastc analyss Course notes are avalable for download at http://www.ct.upt.ro/users/aurelstratan/
More informationLAB 4: Modulus of elasticity
LAB 4: Modulus of elastcty 1. Preparaton: modulus of elastcty (chapter15, p.79) Hook s law graphcal determnaton of modulus of elastcty (p.8) determnaton of modulus of elastcty n tenson and flexural stress
More informationThermal expansion of wood and timber-concrete composite members under ISO-fire exposure
Thermal expanson of wood and tmber-concrete composte members under ISO-fre exposure ANDREA FRANGI and MARIO FONTANA Insttute of Structural Engneerng, ETH Zurch, Swtzerland Summary Ths paper dscusses the
More informationA Mechanics-Based Approach for Determining Deflections of Stacked Multi-Storey Wood-Based Shear Walls
A Mechancs-Based Approach for Determnng Deflectons of Stacked Mult-Storey Wood-Based Shear Walls FPINNOVATIONS Acknowledgements Ths publcaton was developed by FPInnovatons and the Canadan Wood Councl based
More informationAPPENDIX F A DISPLACEMENT-BASED BEAM ELEMENT WITH SHEAR DEFORMATIONS. Never use a Cubic Function Approximation for a Non-Prismatic Beam
APPENDIX F A DISPACEMENT-BASED BEAM EEMENT WITH SHEAR DEFORMATIONS Never use a Cubc Functon Approxmaton for a Non-Prsmatc Beam F. INTRODUCTION { XE "Shearng Deformatons" }In ths appendx a unque development
More informationPlease review the following statement: I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.
Please revew the followng statement: I certfy that I have not gven unauthorzed ad nor have I receved ad n the completon of ths exam. Sgnature: Instructor s Name and Secton: (Crcle Your Secton) Sectons:
More informationPlan: Fuselages can. multideck
Lecture 22(18). TRENGTH ANALY OF FUELAGE Plan: 1. tructurally - power fuselage schemes. 2. trength analyss of fuselages cross-sectons. 3. emmonocoque fuselage cross-secton calculaton. Calculaton from external
More informationSTATIC ANALYSIS OF TWO-LAYERED PIEZOELECTRIC BEAMS WITH IMPERFECT SHEAR CONNECTION
STATIC ANALYSIS OF TWO-LERED PIEZOELECTRIC BEAMS WITH IMPERFECT SHEAR CONNECTION Ákos József Lengyel István Ecsed Assstant Lecturer Emertus Professor Insttute of Appled Mechancs Unversty of Mskolc Mskolc-Egyetemváros
More informationConnection and Tension Member Design
ACH 631 Note Set 17.1 F2015abn Connecton and Tenson Member Desgn Notaton: A = area (net = wth holes, bearng = n contact, etc...) A e = effectve net area fond from the prodct of the net area A n by the
More informationMade by PTY/AAT Date Jan 2006
Job No. VALCOSS Sheet of 9 Rev A P.O. Box 000, FI-0044 VTT Tel. +358 0 7 Fax +358 0 7 700 Design Example 3 Stainless steel lattice girder made Made by PTY/AAT Date Jan 006 RFCS Checked by MAP Date Feb
More informationPlease review the following statement: I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.
ME 270 Fall 2013 Fnal Exam NME (Last, Frst): Please revew the followng statement: I certfy that I have not gven unauthorzed ad nor have I receved ad n the completon of ths exam. Sgnature: INSTRUCTIONS
More informationStructural Steelwork Eurocodes Development of A Trans-national Approach
Structural Steelwork Eurocodes Development of A Trans-national Approach Course: Eurocode Module 7 : Worked Examples Lecture 0 : Simple braced frame Contents: 1. Simple Braced Frame 1.1 Characteristic Loads
More informationI certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.
ME 270 Fall 2012 Fnal Exam Please revew the followng statement: I certfy that I have not gven unauthorzed ad nor have I receved ad n the completon of ths exam. Sgnature: INSTRUCTIONS Begn each problem
More informationSecond Order Analysis
Second Order Analyss In the prevous classes we looked at a method that determnes the load correspondng to a state of bfurcaton equlbrum of a perfect frame by egenvalye analyss The system was assumed to
More informationStructural Steelwork Eurocodes Development of A Trans-national Approach
Structural Steelwork Eurocodes Development of A Trans-national Approach Course: Eurocode 3 Module 7 : Worked Examples Lecture 20 : Simple braced frame Contents: 1. Simple Braced Frame 1.1 Characteristic
More informationJob No. Sheet 1 of 7 Rev A. Made by ER/EM Date Feb Checked by HB Date March 2006
Job No. Sheet of 7 Rev A Design Example Design of a lipped channel in a Made by ER/EM Date Feb 006 Checked by HB Date March 006 DESIGN EXAMPLE DESIGN OF A LIPPED CHANNEL IN AN EXPOSED FLOOR Design a simply
More informationGENERAL GEOMETRY LEFT SIDE BEAM RIGHT SIDE BS :2000/AC:2009. Ratio 0.17
Autodesk Robot Structural Analysis Professional 2015 Design of fixed beam-to-beam connection BS 5950-1:2000/AC:2009 Ratio 0.17 GENERAL Connection no.: 2 Connection name: Beam-Beam Structure node: 40 Structure
More informationNEW. HALFEN Adjustable Cantilever A REVOLUTION IN TUNNEL PIPE SUPPORT
NEW HAFEN Adjustable Cantilever A REVOUTION IN TUNNE PIPE SUPPORT HAFEN Adjustable Cantilever The advantages at a glance The HAFEN Adjustable Cantilever combines the established high load bearing of the
More informationSAMPLE PROJECT IN THE MIDDLE EAST DOCUMENT NO. STR-CALC POINT-FIXED GLASS - STEELWORKS 18 ENGINEER PROJECT. Pages REVISION TITLE
PROJECT ENGINEER DOCUMENT NO. STR-CLC-325 0 REVISION TITLE Pages POINT-FIXED GLSS - STEELWORKS 18 POINT-FIXED GLSS SECONDRY STEELWORKS 2 of 18 Table of contents 1 Basic Data... 3 1.1 References... 3 1.2
More informationExample 4: Design of a Rigid Column Bracket (Bolted)
Worked Example 4: Design of a Rigid Column Bracket (Bolted) Example 4: Design of a Rigid Column Bracket (Bolted) Page : 1 Example 4: Design of a Rigid Column Bracket (Bolted) Determine the size of the
More informationStructural Calculations for Juliet balconies using BALCONY 2 System (Aerofoil) handrail. Our ref: JULB2NB Date of issue: March 2017
Juliet balconies using BALCONY 2 System (Aerofoil) handrail PAGE 1 (ref: JULB2NB280317) Structural Calculations for Juliet balconies using BALCONY 2 System (Aerofoil) handrail Our ref: JULB2NB280317 Date
More informationUNIVERSITY OF BOLTON RAK ACADEMIC CENTRE BENG(HONS) MECHANICAL ENGINEERING SEMESTER TWO EXAMINATION 2017/2018 FINITE ELEMENT AND DIFFERENCE SOLUTIONS
OCD0 UNIVERSITY OF BOLTON RAK ACADEMIC CENTRE BENG(HONS) MECHANICAL ENGINEERING SEMESTER TWO EXAMINATION 07/08 FINITE ELEMENT AND DIFFERENCE SOLUTIONS MODULE NO. AME6006 Date: Wednesda 0 Ma 08 Tme: 0:00
More informationLifetime prediction of EP and NBR rubber seal by thermos-viscoelastic model
ECCMR, Prague, Czech Republc; September 3 th, 2015 Lfetme predcton of EP and NBR rubber seal by thermos-vscoelastc model Kotaro KOBAYASHI, Takahro ISOZAKI, Akhro MATSUDA Unversty of Tsukuba, Japan Yoshnobu
More informationChapter 12 Equilibrium & Elasticity
Chapter 12 Equlbrum & Elastcty If there s a net force, an object wll experence a lnear acceleraton. (perod, end of story!) If there s a net torque, an object wll experence an angular acceleraton. (perod,
More informationDESIGN OPTIMIZATION OF CFRP RECTANGULAR BOX SUBJECTED TO ARBITRARY LOADINGS
Munch, Germany, 26-30 th June 2016 1 DESIGN OPTIMIZATION OF CFRP RECTANGULAR BOX SUBJECTED TO ARBITRARY LOADINGS Q.T. Guo 1*, Z.Y. L 1, T. Ohor 1 and J. Takahash 1 1 Department of Systems Innovaton, School
More informationProject Name Structural Calculation for Feature Pressing
Project Name Structural Calculation for Feature Pressing Presented to: Client Logo Revision Generated by Date Reviewed by Date Comment 0 1 2 3 Table of Contents 1.0 Introduction & Loadings... 3 1.1 Introduction
More informationTHE EFFECT OF TORSIONAL RIGIDITY BETWEEN ELEMENTS ON FREE VIBRATIONS OF A TELESCOPIC HYDRAULIC CYLINDER SUBJECTED TO EULER S LOAD
Journal of Appled Mathematcs and Computatonal Mechancs 7, 6(3), 7- www.amcm.pcz.pl p-issn 99-9965 DOI:.75/jamcm.7.3. e-issn 353-588 THE EFFECT OF TORSIONAL RIGIDITY BETWEEN ELEMENTS ON FREE VIBRATIONS
More informationAn influence line shows how the force in a particular member changes as a concentrated load is moved along the structure.
CE 331, Fall 2010 Influence Les for Trusses 1 / 7 An fluence le shows how the force a partcular member changes as a concentrated load s moved along the structure. For eample, say we are desgng the seven
More informationMaximum Stress Estimation Model for Multi-Span Waler Beams with Deflections at the Supports Using Average Strains
Sensors 05, 5, 778-774; do:0.3390/s5040778 Artcle OPEN ACCESS sensors ISSN 44-80 www.mdp.com/journal/sensors Maxmum Stress Estmaton Model for Mult-Span Waler Beams wth Deflectons at the Supports Usng Average
More informationKSH Bevel gear high speed screw jack
KSH evel gear hgh speed screw jack Product descrpton evel gear hgh speed screw jack KSH1 to KSH3 The bevel gear hgh speed screw jack type KSH s a modular desgn n 3 szes. Each sze s avalable wth two ratos;
More informationJob No. Sheet 1 of 6 Rev B. Made by IR Date Oct Checked by FH/NB Date Oct Revised by MEB Date April 2006
Job No. Sheet 1 of 6 Rev B, Route de Limours Tel : (0)1 0 85 5 00 Fax : (0)1 0 5 75 8 Revised by MEB Date April 006 DESIGN EXAMPLE 6 BOLTED JOINT A 0 0 angle loaded in tension is to be connected to a gusset
More informationChaper 2: Stress in beams
Chaper : Stress n eams FLEURE Beams suject to enng wll fle COPRESSON TENSON On the lower surface the eam s stretche lengthwse. Ths sujects t to tensle stress. N.A. N.A. s the neutral as On the upper surface
More informationTorsion Stiffness of Thin-walled Steel Beams with Web Holes
Torson Stffness of Thn-walled Steel Beams wth Web Holes MARTN HORÁČEK, JNDŘCH MELCHER Department of Metal and Tmber Structures Brno Unversty of Technology, Faculty of Cvl Engneerng Veveří 331/95, 62 Brno
More informationChapter 3. Estimation of Earthquake Load Effects
Chapter 3. Estmaton of Earthquake Load Effects 3.1 Introducton Sesmc acton on chmneys forms an addtonal source of natural loads on the chmney. Sesmc acton or the earthquake s a short and strong upheaval
More informationEurocode 3 for Dummies The Opportunities and Traps
Eurocode 3 for Dummies The Opportunities and Traps a brief guide on element design to EC3 Tim McCarthy Email tim.mccarthy@umist.ac.uk Slides available on the web http://www2.umist.ac.uk/construction/staff/
More informationIndeterminate pin-jointed frames (trusses)
Indetermnate pn-jonted frames (trusses) Calculaton of member forces usng force method I. Statcal determnacy. The degree of freedom of any truss can be derved as: w= k d a =, where k s the number of all
More informationAutodesk Robot Structural Analysis Professional 2014 Design of fixed beam-to-column connection EN :2005/AC:2009
Autodesk Robot Structural Analysis Professional 2014 Design of fixed beam-to-column connection EN 1993-1-8:2005/AC:2009 Ratio 0,44 GENERAL Connection no.: 24 Connection name: Ligação 2 Structure node:
More informationDr. Ing. J. H. (Jo) Walling Consultant Cables Standards Machinery
The common mode crcut resstance unbalance (CMCU) calculaton based on mn. / max. conductor resstance values and par to par resstance unbalance measurements ncludng loop resstance evsed and extended verson
More informationGEOSYNTHETICS ENGINEERING: IN THEORY AND PRACTICE
GEOSYNTHETICS ENGINEERING: IN THEORY AND PRACTICE Prof. J. N. Mandal Department of cvl engneerng, IIT Bombay, Powa, Mumba 400076, Inda. Tel.022-25767328 emal: cejnm@cvl.tb.ac.n Module - 9 LECTURE - 48
More informationSTEEL BUILDINGS IN EUROPE. Multi-Storey Steel Buildings Part 10: Technical Software Specification for Composite Beams
STEEL BUILDINGS IN EUROPE Multi-Storey Steel Buildings Part 10: Technical Software Specification for Composite Beams Multi-Storey Steel Buildings Part 10: Technical Software Specification for Composite
More informationSTUDY ON SEISMIC BEHAVIOR OF RC COMPOSITE CORE WALLS WITH CONCEALED STEEL TRUSS SUBJECTED TO COMBINED ACTION
STUDY ON SEISMIC BEHAVIOR OF RC COMPOSITE CORE WALLS WITH CONCEALED STEEL TRUSS SUBJECTED TO COMBINED ACTION CAO Wanln 1, CHANG Wehua 2, ZHANG Janwe 1 1 College of archtecture and Cvl Engneerng, Bejng
More informationMade by SMH Date Aug Checked by NRB Date Nov Revised by MEB Date April 2006
Job o. OS 466 Sheet of 8 Rev B Silwood Par, Ascot, Bers SL5 7Q Telephone: (0344) 63345 Fax: (0344) 6944 CALCULATIO SHEET Design Example 0 Axiall loaded column in fire ade b SH Date Aug 00 Checed b RB Date
More informationTurbulence classification of load data by the frequency and severity of wind gusts. Oscar Moñux, DEWI GmbH Kevin Bleibler, DEWI GmbH
Turbulence classfcaton of load data by the frequency and severty of wnd gusts Introducton Oscar Moñux, DEWI GmbH Kevn Blebler, DEWI GmbH Durng the wnd turbne developng process, one of the most mportant
More informationASSOCIATION POUR LA CERTIFICATION DES MATERIAUX ISOLANTS
Revson ndex Date of mplementaton C 15/03/017 Techncal Specfcaton E ASSOCIATIO POUR LA CERTIFICATIO DES MATERIAUX ISOLATS 4, avenue du Recteur-Poncaré, 7578 Pars Cedex 16 Tel. 33.(0)1.64.68.84.97 Fax. 33.(0)1.64.68.83.45
More informationChapter Eight. Review and Summary. Two methods in solid mechanics ---- vectorial methods and energy methods or variational methods
Chapter Eght Energy Method 8. Introducton 8. Stran energy expressons 8.3 Prncpal of statonary potental energy; several degrees of freedom ------ Castglano s frst theorem ---- Examples 8.4 Prncpal of statonary
More informationCLT - Cross Laminated Timber Fire protection.
CLT - Cross Lamnated Tmber Fre protecton www.clt.nfo www.storaenso.com C O N T E N T S Verson 01/2014 AG It should be noted that ths fact sheet on fre protecton s merely ntended to support the user. Stora
More informationBASE PLATE CONNECTIONS
SKILLS Project BASE PLATE CONNECTIONS LEARNING OUTCOMES Design process for pinned and fixed column base joints Base-plate resistance Anchor bolt resistance Concrete resistance Weld resistance Application
More informationPreliminary Design of Moment-Resisting Frames
Prelmnary Desgn of Moment-Resstng Frames Preprnt Aamer Haque Abstract A smple method s developed for prelmnary desgn of moment-resstng frames. Preprnt submtted to Elsever August 27, 2017 1. Introducton
More informationDesign of Steel Structures Prof. S.R.Satish Kumar and Prof. A.R.Santha Kumar
5.10 Examples 5.10.1 Analysis of effective section under compression To illustrate the evaluation of reduced section properties of a section under axial compression. Section: 00 x 80 x 5 x 4.0 mm Using
More informationFastener Modeling for Joining Composite Parts
AM-VPD09-006 Fastener Modelng for Jonng Composte Parts Alexander Rutman, Assocate Techncal Fellow, Sprt AeroSystems Chrs Boshers, Stress ngneer, Sprt AeroSystems John Parady, Prncpal Applcaton ngneer,
More informationMODELLING OF ELASTO-STATICS OF POWER LINES BY NEW COMPOSITE BEAM FINITE ELEMENT Bratislava
ODING OF ASTO-STATICS OF POW INS BY NW COPOSIT BA FINIT NT urín Justín 1 rabovský Jura 1 Gogola oman 1 utš Vladmír 1 Paulech Jura 1 1 Insttute of Automotve echatroncs FI STU n Bratslava Ilkovčova 3 812
More informationHALFEN HIT INSULATED CONNECTION
NEW! HALFEN HIT symmetrcal, nsulated connectons for cantlevered balcones! HALFEN HIT INSULATED CONNECTION HIT.-E CONCRETE NEW! the complete product range for balcony solutons wth European Techncal Approval
More informationand Reinforced Soil Structures
Geosynthetcs t and Renforced Sol Structures K. Rajagopal, Professor Department of Cvl Engneerng IIT Madras, Chenna e-mal: gopalkr@tm.ac.n Embankment or Wall? Any slope steeper than 70 s desgned as a retanng
More informationDesign of a Steel I-section for Bending, Shear and Axial Force
Benchmark Example No. 20 Design of a Steel I-section for Bending, Shear and Axial Force SOFiSTiK 2018 VERiFiCATiON MANUAL DCE-EN20: Design of a Steel I-section for Bending, Shear and Axial Force VERiFiCATiON
More informationSCREWS, FASTENERS AND NON PERMANENT JOINTS 2 MOW Department of Mechanical and Aeronautical Engineering
SCREWS, ASTENERS AND NON PERMANENT JOINTS 2 MOW 227 2014 Yeldng take place n the frst thread wth cold work strengthenng Never re-use nuts n structural connectons because ther thread gets daaged Washers
More informationANALYSIS OF TIMOSHENKO BEAM RESTING ON NONLINEAR COMPRESSIONAL AND FRICTIONAL WINKLER FOUNDATION
VOL. 6, NO., NOVEMBER ISSN 89-668 6- Asan Research Publshng Network (ARPN). All rghts reserved. ANALYSIS OF TIMOSHENKO BEAM RESTING ON NONLINEAR COMPRESSIONAL AND FRICTIONAL WINKLER FOUNDATION Adel A.
More informationSIMPLIFIED APPROACH TO THE NON-LINEAR BEHAVIOR OF RC MEMBERS
SIMPLIFIED APPROACH TO THE NON-LINEAR BEHAVIOR OF RC MEMBERS Shahd NASIR 1, Supratc GUPTA 2 And Hdetaka UMEHARA 3 SUMMARY In ths paper, a smplfed one-dmensonal analytcal tool based on fnte dfference technque
More informationLab 2e Thermal System Response and Effective Heat Transfer Coefficient
58:080 Expermental Engneerng 1 OBJECTIVE Lab 2e Thermal System Response and Effectve Heat Transfer Coeffcent Warnng: though the experment has educatonal objectves (to learn about bolng heat transfer, etc.),
More informationCE 4780 Hurricane Engineering II. Section on Flooding Protection: Earth Retaining Structures and Slope Stability. Table of Content
CE 4780 Hurrcane Engneerng II Secton on Floodng Protecton: Earth Retanng Structures and Slope Stablty Dante Fratta Fall 2002 Table of Content Introducton Shear Strength of Sols Seepage Analyss Methods
More informationPRATICAL STATIC CALCULATION METHOD FOR ESTIMATING ELASTO-PLASTIC DYNAMIC RESPONSES OF SPACE FRAMES
th World Congress on Computatonal Mechancs (WCCM XI) 5th European Conference on Computatonal Mechancs (ECCM V) 6th European Conference on Computatonal lud ynamcs (EC VI) E. Oñate, J. Olver and A. Huerta
More informationExperiment 1 Mass, volume and density
Experment 1 Mass, volume and densty Purpose 1. Famlarze wth basc measurement tools such as verner calper, mcrometer, and laboratory balance. 2. Learn how to use the concepts of sgnfcant fgures, expermental
More informationFrame element resists external loads or disturbances by developing internal axial forces, shear forces, and bending moments.
CE7 Structural Analyss II PAAR FRAE EEET y 5 x E, A, I, Each node can translate and rotate n plane. The fnal dsplaced shape has ndependent generalzed dsplacements (.e. translatons and rotatons) noled.
More informationEVALUATION OF THE VISCO-ELASTIC PROPERTIES IN ASPHALT RUBBER AND CONVENTIONAL MIXES
EVALUATION OF THE VISCO-ELASTIC PROPERTIES IN ASPHALT RUBBER AND CONVENTIONAL MIXES Manuel J. C. Mnhoto Polytechnc Insttute of Bragança, Bragança, Portugal E-mal: mnhoto@pb.pt Paulo A. A. Perera and Jorge
More informationDesign of AAC wall panel according to EN 12602
Design of wall panel according to EN 160 Example 3: Wall panel with wind load 1.1 Issue Design of a wall panel at an industrial building Materials with a compressive strength 3,5, density class 500, welded
More informationBasic concept of reactive flows. Basic concept of reactive flows Combustion Mixing and reaction in high viscous fluid Application of Chaos
Introducton to Toshhsa Ueda School of Scence for Open and Envronmental Systems Keo Unversty, Japan Combuston Mxng and reacton n hgh vscous flud Applcaton of Chaos Keo Unversty 1 Keo Unversty 2 What s reactve
More informationEURAMET.M.D-S2 Final Report Final report
Fnal report on ERAMET blateral comparson on volume of mass standards Project number: 1356 (ERAMET.M.D-S2) Volume of mass standards of 10g, 20 g, 200 g, 1 kg Zoltan Zelenka 1 ; Stuart Davdson 2 ; Cslla
More informationBalcony balustrades using the SG12 laminated glass system: PAGE 1 (SG12FF010717) Structural Calculations for SG12 System balustrades using 21.5mm laminated toughened glass without the need for a handrail
More informationAdvanced Analysis of Steel Structures
Advanced Analysis of Steel Structures Master Thesis Written by: Maria Gulbrandsen & Rasmus Petersen Appendix Report Group B-204d M.Sc.Structural and Civil Engineering Aalborg University 4 th Semester Spring
More informationPhysics 141. Lecture 14. Frank L. H. Wolfs Department of Physics and Astronomy, University of Rochester, Lecture 14, Page 1
Physcs 141. Lecture 14. Frank L. H. Wolfs Department of Physcs and Astronomy, Unversty of Rochester, Lecture 14, Page 1 Physcs 141. Lecture 14. Course Informaton: Lab report # 3. Exam # 2. Mult-Partcle
More informationInterconnect Modeling
Interconnect Modelng Modelng of Interconnects Interconnect R, C and computaton Interconnect models umped RC model Dstrbuted crcut models Hgher-order waveform n dstrbuted RC trees Accuracy and fdelty Prepared
More informationFor sunshades using the Zee blades wind loads are reduced by 10 psf.
C.R. Laurence Co., Inc. 2503 East Vernon Los Angeles, CA 90058 24 July 2009 SUBJ: CR LAURENCE UNIVERSAL SUN SHADES The CRL Universal Aluminum Sun Shades were evaluated in accordance with the 2006 International
More information2. (a) Explain different types of wing structures. (b) Explain the advantages and disadvantages of different materials used for aircraft
Code No: 07A62102 R07 Set No. 2 III B.Tech II Semester Regular/Supplementary Examinations,May 2010 Aerospace Vehicle Structures -II Aeronautical Engineering Time: 3 hours Max Marks: 80 Answer any FIVE
More informationBRACING MEMBERS SUMMARY. OBJECTIVES. REFERENCES.
BRACING MEMBERS SUMMARY. Introduce the bracing member design concepts. Identify column bracing members requirements in terms of strength and stiffness. The assumptions and limitations of lateral bracing
More informationCHAPTER 9 CONCLUSIONS
78 CHAPTER 9 CONCLUSIONS uctlty and structural ntegrty are essentally requred for structures subjected to suddenly appled dynamc loads such as shock loads. Renforced Concrete (RC), the most wdely used
More informationFinite Element Modelling of truss/cable structures
Pet Schreurs Endhoven Unversty of echnology Department of Mechancal Engneerng Materals echnology November 3, 214 Fnte Element Modellng of truss/cable structures 1 Fnte Element Analyss of prestressed structures
More informationSchöck Isokorb Type S22 and S16
Schöck Isokorb Type S22 and S16 Figure 1. Schöck Isokorb Type S22 The Schöck Isokorb Type S22 and S16 is used to transmit axial and shear forces in a steel connection. The combination of multiple modules
More informationThe Dissolution and Transport of Radionuclides from Used Nuclear Fuel in an Underground Repository
Presented at the COMSOL Conference 2010 Boston The Dssoluton and Transport of adonucldes from Used Nuclear Fuel n an Underground epostory Y A N N I C K B E A U E G A D 1 M A K G O B I E N 2 F A N K G A
More informationStructural Steelwork Eurocodes Development of A Trans-national Approach
Structural Steelwork Eurocodes Development of A Trans-national Approach Course: Eurocode Module 7 : Worked Examples Lecture 22 : Design of an unbraced sway frame with rigid joints Summary: NOTE This example
More informationSteel Structures Design and Drawing Lecture Notes
Steel Structures Design and Drawing Lecture Notes INTRODUCTION When the need for a new structure arises, an individual or agency has to arrange the funds required for its construction. The individual or
More informationPlease initial the statement below to show that you have read it
EN0: Structural nalyss Exam I Wednesday, March 2, 2005 Dvson of Engneerng rown Unversty NME: General Instructons No collaboraton of any nd s permtted on ths examnaton. You may consult your own wrtten lecture
More informationIn this section is given an overview of the common elasticity models.
Secton 4.1 4.1 Elastc Solds In ths secton s gven an overvew of the common elastcty models. 4.1.1 The Lnear Elastc Sold The classcal Lnear Elastc model, or Hooean model, has the followng lnear relatonshp
More information