ASME PTB Example E E4.3.5 BPVC VIII

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1 Table of contents Table of contents... 1 Comparison Overview * Internal Design Pressure... 3 Example E Cylindrical Shell... 3 E LV Calculation * Example E Conical Shell... 6 E LV Calculation * Example E Spherical Shell... 9 E LV Calculation * Example E Torispherical Head E LV Calculation * Example E Elliptical Head E LV Calculation * Appendix : Material documentation Layout Input values: or Calculated values: or Critical values: or Estimated values: or Lauterbach Verfahrenstechnik GmbH 1 27-Feb-2014

2 Comparison Overview * Equation form Comments Results for examples E4.3.1 to 5 acc. ASME and Lauterbach Verfahrenstechnik GmbH The LV program uses formulas for thick shells acc.asme VIII Div.1 UG27/32 and App.1. Equations Value Conversion factor mm2in = MPa2psi = 'Results Ex. E4.3.1 LV and ASME Required thickness t acc. LV t1 = mm2in*#6(1) Required thickness tc ASME tc1asme = Difference in % Diff1 = (t1-tc1asme)/tc1asme* 'Results Ex. E4.3.2 LV and ASME Required thickness acc. LV t2 = mm2in*#15(7) Required thickness ASME tc2asme = Difference in % Diff2 = (t2-tc2asme)/tc2asme* 'Results Ex. E4.3.3 LV and ASME Required thickness t acc. LV t3 = mm2in*#25(8) Required thickness tc ASME tc3asme = Difference in % Diff3 = (t3-tc3asme)/tc3asme* 'Results Ex. E4.3.4 LV and ASME Allowable Pressure P acc. LV P4 = MPa2psi*#16(5) Allowable Pressure P ASME P4Asme = Difference in % Diff4 = (P4-P4Asme)/P4Asme* 'Results Ex. E4.3.5 LV and ASME Allowable Pressure P acc. LV P5 = MPa2psi*#16(9) Allowable Pressure P ASME P5Asme = Difference in % Diff5 = (P5-P5Asme)/P5Asme* 'Maximum difference between LV and ASME Dmax = Max( Diff1 ; Diff2 ; Diff3 ; Diff4 ; Diff5 ) * Form for equations Lauterbach Verfahrenstechnik GmbH 2 27-Feb-2014

3 4.3 Internal Design Pressure Example E Cylindrical Shell Determine the required thickness for a cylindrical shell considering the following design conditions. All Category A and B joints are Type 1 butt welds and have been 100% radiographically examined. Vessel Data: Material = SA-516, Grade 70, Normalized Design Conditions = 356 psig@300 F Inside Diameter = 90.0 in Corrosion Allowance = in Allowable Stress = psi Weld Joint Efficiency = 1.0 Determine the inside radius and adjust for corrosion allowance. Lauterbach Verfahrenstechnik GmbH 3 27-Feb-2014

4 E LV Calculation * Cylindrical shells Design pressure PD 356 psi = pd 356 psi Hydrostatic head DP 0 psi = Dp 0 psi Calculation pressure P0 356 psi = p0 356 psi Calulation temperature T0 300 F Outside diameter D0 98 in Design wall thickness te 4 in Wall thickness allowance c in Allowance (corrosion) c2 0 in Weld joint efficiency E 1 - Material: K02700-SA Class:-Size: Allowable stress S psi Results Outside radius R0 49 in Effective thickness t in Required thickness t(r0) t(r) thin shell acc. UG in in thick shell (not applicable) in in Minimum t = Min[t(R);t(R0)] t mm with allowances t+c1+c in Allowable excess pressure P 1633 psi Allowable excess pressure without hydr. head MAWP 1633 psi Remark: For calculation of openings according to UG-37: Required thickness t(e=1) mm Allowable unreinforced opening diameter da for welded, brazed, and flued connections acc. UG 36(c)3: da 89 mm for t 10 mm or: da 3 1/2 in for t 3/8 in da 60 mm for t > 10 mm or: da 2 3/8 in for t > 3/8 in For a vessel thickness > 2*t(E=1) the reinforcement of the vessel alone is sufficient for unreinforced openings, unless additional conditions acc. to UG-37 apply. * Thickness of shells under internal pressure ASME BPVC VIII UG-27 & APPENDIX-1, 2013 Edition Lauterbach Verfahrenstechnik GmbH 4 27-Feb-2014

5 Equations: P0 = 0.1*p0 = = 0.1 * R0 = D0 / 2 = 1245 = 2489 / 2 t+c1+c2 = 23.8 = R = R0 - t0 = = 1146 = corroded inside radius 1) Thin shell: For P0 = 356 psi 0.385*S*E = 7700 psi and te = (R0-te) / 2 = ( )/2 = acc. UG-27 Eq.(1) with the inside radius R: P0*R * 1146 t(r) = = = S*E - 0.6*P * * S*E*t * 1 * P(R) = = = R + 0.6*t * or with the outside radius R0 acc. App.1-1 Eq.(1): P0*R * 1245 t(r0) = = = 22 S*E + 0.4*P * * S*E*t * 1 * P(R0) = = = R0-0.4*t * ) Thick shell: For P0 = 356 psi > 0.385*S*E = 7700 psi or te = > (R0-te) / 2 = ( )/2 = with the inside radius R acc. App.1-2: t(r) = R * ( Exp(P0/(S*E)) - 1 ) = 1146 * ( Exp( / ( * 1 ) - 1 ) P(R) = S*E*Log((R+t0)/R) = * 1 * Log(( )/ 1146 )) or with the outside radius R0 acc. App.1-2: t(r0) = R0 * ( 1 - Exp(-P0/(S*E)) ) = 1245 * ( 1 - exp( / ( * 1 ) ) P(R0) = S*E*Log(R0/(R0-t0)) = * 1 * Log( 1245 / ( )) Log(x) = Ln(x) Lauterbach Verfahrenstechnik GmbH 5 27-Feb-2014

6 4.3.2 Example E Conical Shell Determine the required thickness for a conical shell considering the following design conditions. All Category A and B joints are Type 1 butt welds and have been 100% radiographically examined. Vessel Data: Material = SA - 516, Grade 70, Normalized Design Conditions = 356 F Inside Diameter (Large End) = in Inside Diameter (Small End) = 90.0 in Length of Conical Section = 78.0 in Corrosion Allowance = in Allowable Stress = psi Weld Joint Efficiency = 1.0 Adjust for corrosion allowance and determine the cone angle. Lauterbach Verfahrenstechnik GmbH 6 27-Feb-2014

7 E LV Calculation * Conical sections with or without knuckle acc. to UG-32(g) Design pressure PD 356 psi = pd 356 psi Hydrostatic head DP 0 psi = Dp 0 psi Calculation pressure P0 356 psi = p0 356 psi Calculation temperature T0 300 F Final wall thickness te in Wall thickness allowance c1 0 in Allowance (corrosion) c in Effective thickness witout allowances t in Half-apex angle ( 30 without knuckle) α Outside diameter at the large end D in Inside diameter at the large end D in Outside diameter at the small end Dk 94 in Cone length L in Weld joint efficiency factor E 1 - Material: K02700-SA Class:-Size: Allowable stress S psi Calculation: Required thickness t in inc. allowances (te= in t+) t in Allowable excess pressure incl. hydrost. head P psi without hydrostatic head MAWP psi Remark: Geometrical conditions: valid Strength condition: Wall thickness acceptable For calculation of openings according to UG-37(a) in nomenclature for tr: Design diameter according to UG-37(a):tr(b) D1 in Required thickness t(e=1) in * Dished heads and cones under internal pressure ASME VIII UG-32 and APPENDIX-1 BPVC 2013 Edition Lauterbach Verfahrenstechnik GmbH 7 27-Feb-2014

8 Equations according to UG-32(g): cos( α ) = cos( ) = D = D0-2 * t0 / cos( α ) = 3812 = * / P0*D t =, 2*cos( α )*(S*E - 0.6*P0) t = = * * ( * * ) 2*S*E*t0*cos( α ) P =, D + 1.2*t0*cos( α ) P = = 2 * * 1 * * * * Rem.: App.1-5(d) or (e) indicates if a reinforcement ring is required. Lauterbach Verfahrenstechnik GmbH 8 27-Feb-2014

9 4.3.3 Example E Spherical Shell Determine the required thickness for a spherical shell considering the following design conditions. All Category A joints are Type 1 butt welds and have been 100% radiographically examined. Vessel Data: Material = SA -542, TypeD, Class 4a Design Conditions = 2080 psig@850 F Inside Diameter = in Corrosion Allowance = 0.0 in Allowable Stress = ps Weld Joint Efficiency = 1.0 Lauterbach Verfahrenstechnik GmbH 9 27-Feb-2014

10 E LV Calculation * Spherical shells Design pressure PD 2080 psi = pd 2080 psi Hydrostatic head DP 0 psi = Dp 0 psi Calculation pressure P psi = p psi Calulation temperature T0 850 F Outside diameter D0 157 in Design wall thickness te 4 in Wall thickness allowance c1 0 in Allowance (corrosion) c2 0 in Weld joint efficiency E 1 - Material: K31835-SA-542-D-Class:4a-Size: Allowable stress S psi Results Outside radius R in Effective thickness t0 4 in Required thickness t(r0) t(r) thin shell acc. UG in in thick shell (not applicable) in in Minimum t = Min[t(R);t(R0)] t mm with allowances t+c1+c in Allowable excess pressure P 2231 psi Allowable excess pressure without hydr. head MAWP 2231 psi Remark: For calculation of openings according to UG-37: Minimum required thickness for openings t(e=1) mm Allowable unreinforced opening diameter da for welded, brazed, and flued connections acc. UG 36(c)3: da 89 mm for t 10 mm or: da 3 1/2 in for t 3/8 in da 60 mm for t > 10 mm or: da 2 3/8 in for t > 3/8 in For a vessel thickness > 2*t(E=1) the reinforcement of the vessel alone is sufficient for unreinforced openings, unless additional conditions acc. to UG-37 apply. * Thickness of shells under internal pressure ASME BPVC VIII UG-27 & APPENDIX-1, 2013 Edition Lauterbach Verfahrenstechnik GmbH Feb-2014

11 Equations P0 = 0.1*p0 = = 0.1 * R0 = D0 / 2 = 1994 = 3988 / 2 t+c1+c2 = = R = R0 - t0 = = 1892 = corroded inside radius 1) Thin shell: For P0 = 2080 psi 0.665*S*E = psi and te = *(R0-te) = 0.356*( ) = acc. UG-27 Eq.(3) with the inside radius R: P0*R * 1892 t(r) = = = *S*E-0.2*P0 2* * 1-0.2* *S*E*t0 2* * 1 * P(R) = = = R + 0.2*t * or with outside radius R0 acc. App.1-1 Eq.(2): P0*R * 1994 t(r0) = = = *S*E+0.8*P0 2* * * *S*E*t0 2* * 1 * P(R0) = = = R0-0.8*t * ) Thick shell: Für P0 = 2080 psi > 0.665*S*E = psi or te = > 0.356*(R0-te) = 0.356*( ) = with inside radius R acc. App.1-3: t(r) = R * ( Exp(0.5*P0/(S*E)) - 1 ) = 1994 * ( exp(0.5* / ( * 1 ) - 1 ) P(R) = 2*S*E*Log((R+t0)/R) = 2* * 1 * Log(( )/ 1892 ) or with outside radius R0 acc. App.1-3: t(r0) = R0 * ( 1 - Exp(-0.5*P0/(S*E)) ) = 1994 * ( 1 - exp(-0.5* / ( * 1 ) ) P(R0) = 2*S*E*Log(R0/(R0-t0)) = 2* * 1 * Log( 1994 /( )) Log(x) = Ln(x) Lauterbach Verfahrenstechnik GmbH Feb-2014

12 Example E Torispherical Head Determine the maximum allowable working pressure (MAWP) for the proposed seamless torispherical head. The Category B joint joining the head to the shell is a Type 1 butt weld and has been 100% radiographically examined. Vessel Data: Material = SA -387, Grade 11, Class 1 Design Temperature = 650 F Inside Diameter = 72.0 in Crown Radius = 72.0 in Knuckle Radius = in Thickness = in Corrosion Allowance = in Allowable Stress = psi Weld Joint Efficiency = 1.0 Modulus of Elasticity at Design Temperature = 26.55E + 06 psi Yield Strength at Design Temperature = psi Adjust for corrosion allowance Lauterbach Verfahrenstechnik GmbH Feb-2014

13 E LV Calculation * Input: Type of head (1=Kloepper-, 2=Korbbogen-, 3=Torispherical, 4=Semi-spherical, 5=Elliptical 2:1) 3 Torispherical Design pressure PD 136 psi = pd 136 psi Hydrostatic head DP 0 psi = Dp 0 psi Calculation pressure P0 136 psi = p0 136 psi Calculation temperature T0 650 F Final wall thickness te in Wall thickness allowance c1 0 in Allowance (corrosion) c in Effective thickness witout allowances t0 0.5 in Outside diameter of cylindrical shell D in Inside diameter of cylindrical shell (= D0-2t0) D in Outside crown radius L in Inside crown radius (= L0-t0) L in Knuckle radius r 4.5 in Weld joint efficiency E 1 - Material: K11789-SA Class:1-Size: Elasticity modulus ET 2.660E+7 psi Elastic limit Sy psi Reduce allowable *) stress for Rm20 > 485 MPa? Yes (Yes/No) Tensile strength at 20 C Rm psi Allowable stress: at working temperature acc. ASME-table ST psi at 20 C S psi acc. UG-32(e) or App. 1-4(c) S psi *) According to App. 1-4(c) the allowable stress must be reduced to 138 * ST /S20 (=20 ksi*...) for Rm20 > 485 MPa (70 ksi) Calculation: Ratio L/r Factor M Required thickness without allowance t in inc. allowances (te= in t+) t in Allowable excess pressure incl. hydrost. head P psi without hydrostatic head MAWP psi Geometrical conditions: valid Strength condition: Final wall thickness 15,875 < 15,9403 = required thickness * Dished heads and cones under internal pressure ASME VIII UG-32 and APPENDIX-1 BPVC 2013 Edition Lauterbach Verfahrenstechnik GmbH Feb-2014

14 Required thickness for openings acc. to UG-37(a) in nomenclature for tr: Using UG-32 with E=1 t(e=1) = in acc. section (a) in the crown region t1(e=1) = in Allowable unreinforced opening diameter da for welded, brazed, and flued connections acc. UG 36(c)3: da 89 mm (3.5 in.) for t 10 mm (3/8 in.) da 60 mm (2 3/8 in.) for t > 10 mm (3/8 in.) Remark: Equations: P0*L*M * 1832 * t = = = 2*S*E-0.2*P0 2* * * *S*E*t0 2 * * 1 * 12.7 P = = L*M + 0.2*t * * 12.7 For openings in the crown region with: Opening diameter di in Distance between opening center and head center e in Available reinforcement width acc. UG37: Available reinforcement width of the crown b' in Diameter of the crown region dka in Angle of the knuckle region phi Arc length of the knuckle region b in dka = (2*L+te)*(D/2-r)/(L-r) phi = Arccos( (D/2-r)/(L-r) ) b' = (dka-di)/2 - e b = (r+te)*phi Lauterbach Verfahrenstechnik GmbH Feb-2014

15 Example E Elliptical Head Determine the maximum allowable working pressure (MAWP) for the proposed seamless 2:1 elliptical head. The Category B joint joining the head to the shell is a Type 1 butt weld and has been 100% radiographically examined. Vessel Data: Material Design Temperature = = SA-516, Grade 70, Norm. 300 F Inside Diameter = 90.0 in Thickness = in Corrosion Allowance = in Allowable Stress = psi Weld Joint Efficiency = 1.0 Modulus of Elasticity at Design Temperature = = 28.3E + 06 psi Yield Strength at Design Temperature = psi Determine the elliptical head diameter to height ratio, k, and adjust for corrosion allowance. Lauterbach Verfahrenstechnik GmbH Feb-2014

16 E LV Calculation * Ellipsoidal heads acc. UG-32(d) and Appendix 1-4(f) Design pressure PD psi = pd psi Hydrostatic head DP 0 psi = Dp 0 psi Calculation pressure P psi = p psi Calculation temperature T0 300 F Final wall thickness te in Wall thickness allowance c1 0 in Allowance (corrosion) c in Effective thickness witout allowances t0 1 in Outside diameter of cylindrical shell D in Inside diameter of cylindrical shell (= D0-2t0) D in Outer height of head (minor semi-axis) h in Inside depth of head (minor semi-axis= h0-t0) h 22.5 in Weld joint efficiency E 1 - Material: K02700-SA Class:-Size: Elasticity modulus ET 2.829E+7 psi Elastic limit Sy psi Reduce allowable *) stress for Rm20 > 485 MPa? Yes (Yes/No) Tensile strength at 20 C Rm psi Allowable stress: at working temperature acc. ASME-table ST psi at 20 C S psi acc. UG-32(e) or App. 1-4(c) S psi *) According to App.1-4(c) the allowable stress must be reduced to 138 * ST / S20 (=20 ksi*...) for Rm20 > 485 MPa (70 ksi) and K > 1 Results: Ratio D/2h 2 - Factor K 1 - Factor K1 acc. Table UG-37 K Required thickness t 1 in incl. allowances (te= in t+) t in Allowable excess pressure incl. hydrost. Head P psi without hydrostatic head MAWP psi Required thickness for openings acc. to UG-37(a) in nomenclature for tr: Using UG-32 with E=1 t(e=1) 1 in Section (c) in the centre circle < 0.8*D t1(e=1) 0.9 in Equivalent spherical diameter 2*K1*D0 Dk in Geometrical conditions: valid Strength: Wall thickness acceptable * Dished heads and cones under internal pressure ASME VIII UG-32 and APPENDIX-1 BPVC 2013 Edition Lauterbach Verfahrenstechnik GmbH Feb-2014

17 Allowable unreinforced opening diameter da for welded, brazed, and flued connections acc. UG 36(c)3: da 89 mm (3.5 in.) for t 10 mm (3/8 in.) da 60 mm (2 3/8 in.) for t > 10 mm (3/8 in.) Remark: Equations according to UG-32: P0*D*K * 2292 * 1 t = 25.4 = 2*S*E - 0.2*P0 2* * 1-0.2* *S*E*t0 2 * * 1 * 25.4 P = = K*D + 0.2*t0 1 * * 25.4 Geometry of an equivalent torispherical head: Equivalent spherical inside radius = K1*D L = in Knuckle inside radius acc. Table r = in Lauterbach Verfahrenstechnik GmbH Feb-2014

18 Appendix : Material documentation Section no 2: Schale/UG27Section no 3: Boden/UG32 Material specification: Regulation: ASMET1A:2010Spec. No.: SA-516 Product: Plate Material code: K02700-SA Class:-Size: Short name: Carbon steel Design conditions and dimensions: Temperature [ C]: 148,8889 Pressure [bar]: 30,49 Thickness [mm]: 101,6 Outside diameter [mm]: 2489,2 Material values for test and design conditions: Test condition Operating condition Nominal design strength [N/mm²]: 138,00 138,00 Safety factor: 1,00 1,00 Allowable stress [N/mm²]: 138,00 138,00 Modulus of elasticity [kn/mm²]: ,0667 Creep rupture strength for h [MPa]: Tensile strength and yield stress at ambient temperature: Diam./ Tensile str. ReH Rupture Rupture Thick. Rm min Rm max elong. elong <= mm MPa MPa MPa längs % quer % K-values as function of the temperature Diam./ Thickn. 50 C 100 C 150 C 200 C 250 C 300 C 350 C 400 C <= mm MPa MPa MPa MPa MPa MPa MPa MPa K-values as function of the temperature Diam./ Thickn. 450 C 500 C 550 C 600 C 650 C 700 C 800 C <= mm MPa MPa MPa MPa MPa MPa MPa Modulus of elasticity in dependence of the temperature: Static modulus of elasticity in [kn/mm²] at the temperature of Coefficient of linear expansion: Thermal coefficient of expansion between 20 C and Density 100 C 200 C 300 C 400 C 500 C 600 C 700 C 800 C Heat Heat (20 C) cond. capac. kg/dm³ 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K W/Km J/kgK ,85 12,1 12,7 13,3 13,8 14, Lauterbach Verfahrenstechnik GmbH Feb-2014

19 Section no 4: Schale/UG27 Material specification: Regulation: ASMET1A:2010Spec. No.: SA-542 Product: Plate Material code: K31835-SA-542-D-Class:4a-Size: Short name: 2.25Cr-1Mo-V Design conditions and dimensions: Temperature [ C]: 454,44 Pressure [bar]: 30,49 Thickness [mm]: 101,6 Outside diameter [mm]: 3987,8 Material values for test and design conditions: Test condition Operating condition Nominal design strength [N/mm²]: 168,00 144,29 Safety factor: 1,00 1,00 Allowable stress [N/mm²]: 168,00 144,29 Modulus of elasticity [kn/mm²]: ,5062 Creep rupture strength for h [MPa]: Tensile strength and yield stress at ambient temperature: Diam./ Tensile str. ReH Rupture Rupture Thick. Rm min Rm max elong. elong <= mm MPa MPa MPa längs % quer % K-values as function of the temperature Diam./ Thickn. 50 C 100 C 150 C 200 C 250 C 300 C 350 C 400 C <= mm MPa MPa MPa MPa MPa MPa MPa MPa K-values as function of the temperature Diam./ Thickn. 450 C 500 C 550 C 600 C 650 C 700 C 800 C <= mm MPa MPa MPa MPa MPa MPa MPa Modulus of elasticity in dependence of the temperature: Static modulus of elasticity in [kn/mm²] at the temperature of Coefficient of linear expansion: Thermal coefficient of expansion between 20 C and Density 100 C 200 C 300 C 400 C 500 C 600 C 700 C 800 C Heat Heat (20 C) cond. capac. kg/dm³ 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K W/Km J/kgK ,1 12,7 13,3 13,8 14, Lauterbach Verfahrenstechnik GmbH Feb-2014

20 Section no 5: Boden/UG32 Material specification: Regulation: ASMET1A:2010Spec. No.: SA-387 Product: Plate Material code: K11789-SA Class:1-Size: Short name: 1.25Cr-0.5Mo-Si Design conditions and dimensions: Temperature [ C]: 343,33 Pressure [bar]: 30,49 Thickness [mm]: 15,88 Outside diameter [mm]: 1860,55 Material values for test and design conditions: Test condition Operating condition Nominal design strength [N/mm²]: 118,00 118,00 Safety factor: 1,00 1,00 Allowable stress [N/mm²]: 118,00 118,00 Modulus of elasticity [kn/mm²]: ,4002 Creep rupture strength for h [MPa]: Tensile strength and yield stress at ambient temperature: Diam./ Tensile str. ReH Rupture Rupture Thick. Rm min Rm max elong. elong <= mm MPa MPa MPa längs % quer % K-values as function of the temperature Diam./ Thickn. 50 C 100 C 150 C 200 C 250 C 300 C 350 C 400 C <= mm MPa MPa MPa MPa MPa MPa MPa MPa K-values as function of the temperature Diam./ Thickn. 450 C 500 C 550 C 600 C 650 C 700 C 800 C <= mm MPa MPa MPa MPa MPa MPa MPa Modulus of elasticity in dependence of the temperature: Static modulus of elasticity in [kn/mm²] at the temperature of Static modulus of elasticity in [kn/mm²] at the temperature of Coefficient of linear expansion: Thermal coefficient of expansion between 20 C and Density 100 C 200 C 300 C 400 C 500 C 600 C 700 C 800 C Heat Heat (20 C) cond. capac. kg/dm³ 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K W/Km J/kgK ,85 12,1 12,7 13,3 13,8 14, Lauterbach Verfahrenstechnik GmbH Feb-2014

21 Section no 6: Boden/UG32 Material specification: Regulation: ASMET1A:2010Spec. No.: SA-516 Product: Plate Material code: K02700-SA Class:-Size: Short name: Carbon steel Design conditions and dimensions: Temperature [ C]: 148,89 Pressure [bar]: 30,49 Thickness [mm]: 28,58 Outside diameter [mm]: 2343,15 Material values for test and design conditions: Test condition Operating condition Nominal design strength [N/mm²]: 138,00 138,00 Safety factor: 1,00 1,00 Allowable stress [N/mm²]: 138,00 138,00 Modulus of elasticity [kn/mm²]: ,0666 Creep rupture strength for h [MPa]: Tensile strength and yield stress at ambient temperature: Diam./ Tensile str. ReH Rupture Rupture Thick. Rm min Rm max elong. elong <= mm MPa MPa MPa längs % quer % K-values as function of the temperature Diam./ Thickn. 50 C 100 C 150 C 200 C 250 C 300 C 350 C 400 C <= mm MPa MPa MPa MPa MPa MPa MPa MPa K-values as function of the temperature Diam./ Thickn. 450 C 500 C 550 C 600 C 650 C 700 C 800 C <= mm MPa MPa MPa MPa MPa MPa MPa Modulus of elasticity in dependence of the temperature: Static modulus of elasticity in [kn/mm²] at the temperature of Coefficient of linear expansion: Thermal coefficient of expansion between 20 C and Density 100 C 200 C 300 C 400 C 500 C 600 C 700 C 800 C Heat Heat (20 C) cond. capac. kg/dm³ 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K 10E-6/K W/Km J/kgK ,85 12,1 12,7 13,3 13,8 14, Lauterbach Verfahrenstechnik GmbH Feb-2014

Weight [lb] = (Do-t)*π*L*t*40.84/ (60-1)*3.1416*100*1*40.84/144 = (20000*1*1)/(29+0.6*1) = Pipe and Shell ver 4.

Weight [lb] = (Do-t)*π*L*t*40.84/ (60-1)*3.1416*100*1*40.84/144 = (20000*1*1)/(29+0.6*1) = Pipe and Shell ver 4. 1 Pipe and Shell ver 4.08 Page 1 of 2 2 Host Shell Description 3 Options: 4 Interior ip? - Calculate interior pressure 5 No Exterior ep? - Calculate exterior pressure 6 Rolled Plate pr? - Pipe or rolled

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