Design Calculations. ETSEIB - UPC Josep Mª Mabres Anter TFG

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4 Table of Contents Table of Contents... Codes, Guidelines and Standards Implemented Design Conditions Allowable stresses and safety factors... 6 Shell (comp. 1)... 6 Tube (comp. )... 6 Test Pressure... 7 Tube layout Tube layout report flow section Pass Partition Plate Element(s) of geometry in internal pressure...1 Korbbogen Type Head (30.10) Internal pressure....1 Conical shell (30.4) internal pressure Korbbogen Type Head (5.1) Internal pressure Cylindrical shell under internal pressure Body flange(s) and cover(s)...16 Body Flange and Cover 5.01 in operation Body Flange and Cover in operation Body Flange and Cover 5.01 in test....0 Body Flange and Cover in test....1 Body Flange and Cover 3903 in test.... Tubesheet(s) and Expansion Joint...3 Tubesheet, Loading conditions 1 [corroded normal condition] AD 000-Merkblatt B 5, Tubesheet, Loading conditions [corroded normal condition] AD 000-Merkblatt B 5, Tubesheet, Loading conditions 3 [corroded normal condition] AD 000-Merkblatt B 5, Tubesheet, Loading conditions T0 [test condition] AD 000-Merkblatt B 5, Tubesheet, Loading conditions 0T [test condition] AD 000-Merkblatt B 5, Tubes of the bundle Tube of bundle in internal pressure Tube of bundle in external pressure Vessel under combination loading...34 Model for stress analysis due to supporting Location of dominant stresses and worst cases Case 1 - Operation Int.Max.P. (Corroded Weight) Maximum Allowable Working Pressure...40 Maximum Allowable Working Pressure(Geometry) Maximum Allowable Working Pressure (Nozzles) Maximum Allowable Working Pressure (tubes of bundle) Maximum Allowable Working Pressure (compartment) Isolated Opening(s)...4 Isolated opening S [ in operation Int.P. ] (Shell Outlet)...4 Isolated opening S [ in test Int.P. ] (Shell Outlet)...43 Isolated opening S1 [ in operation Int.P. ] (Shell Outlet)...44 Isolated opening S1 [ in test Int.P. ] (Shell Outlet)...45 Isolated opening T [ in operation Int.P. ] (Channel Outlet)...46 Isolated opening T [ in test Int.P. ] (Channel Outlet)...47 Isolated opening T1 [ in operation Int.P. ] (Channel inlet)...48 Isolated opening T1 [ in test Int.P. ] (Channel inlet)...49 Summary...50 Summary of nozzles [ Location and Dimensions ] AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

5 Summary of nozzles [ Type, Adjacent Openings, Goose and Material ] Summary of nozzles [ Type, Weight and Local Loads ] Summaries of bundle Summary of Forged Items and Relevant Accessories....5 Summary of Geometry Summary of Weights, Capacities and Painting Areas Summary of saddles...55 Summary of Foundation Loads...55 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

6 Codes, Guidelines and Standards Implemented. Pressure vessel design code : AD 000-Merkblätter (07-01) B 0, B 1, B, B 3, B 5, B 6, B 7, B 8, B 9, Design Code of Tubesheets : AD 000-Merkblatt B 5, Manufacturing standard : TEMA 9th Edition - Nov. 007 Type = BKU Local load design method: PD 5500:01 G - (09-01) Standard of flange ratings : DIN 401:1996 Standard of pipes: ASME B36.10M-004/B36.19M-004 Standard of material : DIN17440 September 1996 X CrNiMo Plate DIN17458 July 1985 X CrNiMo Seamless pipe DIN17440 September 1996 X CrNiMo Forging EN10- April 000 P65GH Forging EN1016- December 00 P65GH Seamless pipe EN1008- June 009 P65GH Plate EN March 005 XCrNiMo17-1- Seamless tube ASME II 01 SA193GRB7 Bolting ASME II 01 SA516GR60 Plate Units : SI g = 9,80665 m/s [ Weight (N) = Mass (kg) g ] AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

7 Design Conditions. Shell (comp. 1) Tube (comp. ) / Internal pressure : 0,8 MPa 1, MPa / Requested MAWP : 0,8 MPa 1, MPa / Design Temperature : 104,4 C 60 C / Height of liquid : 0 mm 0 mm / Operating fluid spec. gravity : 1 1 / Corrosion : 0 mm 3,175 mm / External pressure : / Design temp., external : / Test Pressure : / Test fluid spec. gravity : 1 1 / Insulation Thickness : 0 mm 0 mm / Weight/density of insulation : 35 kg/m 3 35 kg/m 3 / Construction Category : / Nominal stress : 1 1 / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

8 Allowable stresses and safety factors AD B0 / AD B6 f Allowable stress at design temperature. R m tensile strength. R p0. yield strength 0, %. R p1 yield strength 1 %. R Average stress to cause rupture at the end of hours at design temperature. Flanges in operation f = f 1 In test and gasket seating f = f 1 Shell (comp. 1) Allowable stress at design temperature f Materials Normal Conditions Exceptional and test conditions Creep Excluding bolting B0 B6 B0 B6 B0 B6 Carbon steel R p0. / 1,5 R p0. / 1,6 R p0. / 1,05 R p0. / 1,1 R / 1,5 R / 1,6 Stainless steel R p1 / 1,5 R p1 / 1,6 R p1 / 1,05 R p1 / 1,1 R / 1,5 R / 1,6 Copper alloy R m / 3,5 R m / 4 R m /,5 R m /,5 R / 3,5 R / 4 Aluminum Alloy R p1 / 1,5 R p1 / 1,6 R p1 / 1,05 R p1 / 1,1 R / 1,5 R / 1,6 Nickel alloy R p0. / 1,5 R p0. / 1,6 R p0. / 1,05 R p0. / 1,1 R / 1,5 R / 1,6 Titanium and Zirconium R p0. / 1,5 R p0. / 1,6 R p0. / 1,05 R p0. / 1,1 R / 1,5 R / 1,6 Cast Iron R p0. / R p0. / R p0. / 1,4 R p0. / 1,5 R / R / Bolting Standard Neckdown Standard Neckdown Standard Neckdown Carbon steel R p0. / 1,8 R p0. / 1,5 R p0. / 1,3 R p0. / 1,1 R / 1,8 R / 1,5 Stainless steel R p1 / 1,8 R p1 / 1,5 R p1 / 1,3 R p1 / 1,1 R / 1,8 R / 1,5 Tube (comp. ) Allowable stress at design temperature f Materials Normal Conditions Exceptional and test conditions Creep Excluding bolting B0 B6 B0 B6 B0 B6 Carbon steel R p0. / 1,5 R p0. / 1,6 R p0. / 1,05 R p0. / 1,1 R / 1,5 R / 1,6 Stainless steel R p1 / 1,5 R p1 / 1,6 R p1 / 1,05 R p1 / 1,1 R / 1,5 R / 1,6 Copper alloy R m / 3,5 R m / 4 R m /,5 R m /,5 R / 3,5 R / 4 Aluminum Alloy R p1 / 1,5 R p1 / 1,6 R p1 / 1,05 R p1 / 1,1 R / 1,5 R / 1,6 Nickel alloy R p0. / 1,5 R p0. / 1,6 R p0. / 1,05 R p0. / 1,1 R / 1,5 R / 1,6 Titanium and Zirconium R p0. / 1,5 R p0. / 1,6 R p0. / 1,05 R p0. / 1,1 R / 1,5 R / 1,6 Cast Iron R p0. / R p0. / R p0. / 1,4 R p0. / 1,5 R / R / Bolting Standard Neckdown Standard Neckdown Standard Neckdown Carbon steel R p0. / 1,8 R p0. / 1,5 R p0. / 1,3 R p0. / 1,1 R / 1,8 R / 1,5 Stainless steel R p1 / 1,8 R p1 / 1,5 R p1 / 1,3 R p1 / 1,1 R / 1,8 R / 1,5 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

9 Test Pressure AD HP 30 p p = Fp. p F p = max [ 1,43 ; 1,5 (K 0 / K ) min ] p = Design Pressure K 0 = design strength value at test temperature K = design strength value at design temperature For each component p K 0 K s e c p p (MPa) (MPa) (MPa) (MPa) Korbbogen Type Head (01) , ,144 Shell (0) , ,144 Cone (03) , ,144 Shell (04) , ,35 0 1,144 Shell (10) , ,6 7,9 3,175,3717 Korbbogen Type Head (11) 5.1 1, ,1487 Shell (comp. 1) Tube (comp. ) / Test Pressure at the Top P e : 1,144 MPa,1487 MPa / Use PED : P t = MAX [ 1,43 P s ; 1,5 P s ( f a / f t ) min ] P s = maximum allowable pressure P = Design Pressure f a = allowable stress at room temperature, normal condition f t = allowable stress at design temperature For each component P f a f t e c P t (MPa) (MPa) (MPa) (MPa) Korbbogen Type Head (01) , ,144 Shell (0) , ,144 Cone (03) , ,144 Shell (04) , ,35 0 1,144 Shell (10) , ,6 7,9 3,175,3717 Korbbogen Type Head (11) 5.1 1, ,1487 Shell (comp. 1) Tube (comp. ) / maximum allowable pressure : 0,8 MPa 1, MPa / Test Pressure at the Top : 1,144 MPa,1487 MPa / AD HP : for vertical vessel : p p = p p + p p AD HP : Test in vertical position, pressure measured at the top of the vessel in vertical position p p = 0.1 ( F H F P H) 0 AD HP : Test in horizontal position before a test in vertical position, pressure measured at the top of the vessel in horizontal position :p p = 0 AD HP : Test in horizontal position alone, pressure measured at the top of the vessel in horizontal position p p = max [ 0.1 P H ; 0.1 F H F ] H F = liquid level in operation H = liquid level in test F = Specific gravity of the liquid in operation P = Specific gravity of the liquid in test Shell (comp. 1) Tube (comp. ) / Design Pressure p : 0,8 MPa 1, MPa / Test Pressure at the Top p p : 1,144 MPa,1487 MPa / p p AD HP / / / p p AD HP / / / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

10 Tube layout. A A-A A 1 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

11 Tube layout report. Shell inside diameter : 399,65 mm Outer tube limit diameter 9,14 mm Baffle Outside Diameter : 396,48 mm Tube Pitch : 31,75 mm Tube Diameter : 5,4 mm Number of Tubes : 56 Mean Deviation : 0 % Number of Tie Rods : 0 Variance Factor : 0 % Number of sealing strips : 0 Mean tolerance : 0 % Number of Sealing Rods : 0 Max. pass tolerance : 0 % Number of sliding rails : 0 Actual shell inlet free height : 0 mm Actual shell outlet free height : 65,84 mm Pass number Number of Tubes Adj. Tol. Adj. Tol Tol. 1- : 0,00 % No. of support plates = 0 Type no.. flow section No. of baffles (Support Plate) = 0 / / / Unsupported tube spans (calculated values) : between two Tubesheets (both ends fixed) = / between a Tubesheet and a tube support (one end fixed, the other pinned) = 0 mm between two tube supports (both ends pinned) = 0 mm Unsupported tube spans (fixed value) : between a Tubesheet and a tube support (one end fixed, the other pinned) = / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

12 flow section. Minimum inside depth of channels. The minimum cross-over area for flow between successive tube passes is at least equal to 1.3 times the flow area through the tubes of one pass. Channel inlet : mm Channel outlet (or rear box) : / (for a floating head, it s the length of flange under the crown) TEMA RGP-RCB-4.6 Shell or Bundle Entrance and Exit Areas. Outer tube limit diameter : OTL = 9,14 mm Factor indicating tube pitch type and orientation : F = 0,866 Impingement plate length : L p = 0 mm Tube Pitch : P t = 31,75 mm Tube outside diameter : D t = 5,4 mm Impingement plate edge length : I p = 0 mm Fluid velocity Inlet Outlet flow section area (nozzle) : V n = 0 Jm 3 0 Jm 3 flow section area (shell cross section) : V s = 0 Jm 3 0 Jm 3 flow section area (bundle) : V b = 0 Jm 3 0 Jm 3 Shell inside diameter : D s = 399,65 mm 399,65 mm Nozzle internal diameter : D n = 0 mm 54,76 mm RGP-RCB Shell entrance or exit area Inlet Outlet Factor indicating presence of impingement plate : F 1 = 1 1 Free height at nozzle centerline : h 1 = 0 mm 65,84 mm Free height at nozzle edge : h = h 1-0.5[D s -(D s -D n ) 0.5 ] = 0 mm 63,95 mm Average free height above tube bundle or impingement plate : h = 0.5(h 1 +h ) = 0 mm 64,89 mm Requested : Dn Vs A s,min = V = 0 mm.355,1 mm 4 n D n Pt Dt calculated : A s = Dnh F 1 4 = 0 mm ,8 mm F Pt Required free height at nozzle centerline : h 1,min = 0 mm 11,47 mm RGP-RCB Bundle entrance or exit area Inlet Outlet Effective chord distance across bundle : K = Area of Impingement Plate : A p = Unrestricted longitudinal flow area : A l = Distance 1st Baffle : B s = Requested : Dn Vb A b,min = = V D OTL B K A P D F P 4 n t t calculated : A b = s s s p l B t A = Required baffle spacing : B s,min = AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

13 Pass Partition Plate. TEMA RCB Material : SA516GR60 Temperature : 60 C Allowable stress : S = 10 MPa Nominal thickness : t n = 9,5 mm Corrosion : RCB Pressure drop across plate : q = 0 MPa RCB-9.13 : t b Factor B Fixing qb Table RCB = Three sides fixed, one side simply supported 1.5S = Long sides fixed, short sides simply supported t min : Table RCB = Short sides fixed, long sides simply supported (Carbon Steel) Roark s Formulas 4 = semicircular plate, all edges fixed RCB : The plate shall be attached with fillet welds on each sides with a minimum leg of t leg = ¾ t. Front Pass Partition Plate. Fixing a b a/b B t min t t leg 1 390,56 41,61 0,93 0,675 9,50 0,00 0,00 t req = max [ max(t) ; max(t min ) ] = 9,5 mm The pass partition plate thickness is adequate. AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

14 Element(s) of geometry in internal pressure Korbbogen Type Head (30.10) Internal pressure. AD 000-Merkblätter (07-01) B3 h h 1 s e = nominal thickness v = Joint efficiency K/S = Allowable stress T = Temperature s = minimum required thickness = circular stress p = internal pressure p max = Max. allowable pressure R = equivalent inside radius p h = Hydrostatic pressure r = inside knuckle radius D a = External Diameter = 7 mm h = outside height = 186,4 mm c 1 +c = corrosion + tolerance h 1 = Knuckle Length = 18 mm Tol % = tolerance for pipes Straight flange = 50,00 mm d i (nozzle : /) s n,min = s/tol % shall be s e X CrNiMo Plate Stainless Steel Schedule : / NPS : / s e = 6,000 mm Tol % = / PWHT : No Radiography : Full Seamless Cor. = 0 mm Tol. = 0 mm TEMA RCB-3.13 = 4,76 mm Operation Horizontal test N X p (MPa) p h (MPa) T ( C) K/S (MPa) v r R 0, ,4 13, , ,600 1,151 0, , , ,600 opening factor : d i /D a design factor : (AD B3 fig 9 ((s e -c 1 -c )/D a )) Da pβ R se p Knuckle thickness : s1 c1 c Head thickness : s c1 c 4 K S v K S v p Da p Cyl. Part thickness : s3 c1 c s = max(s K S v p 1,s,s 3 ) Operation Horizontal test L.T Operation Horizontal test K/S shall be D a N X N X MAWP (104,4 C, Corroded) =, MPa R r d i d i /D a (s e -c 1 -c )/D a s 1 s s 3 0,000 0,00 8, ,989,161 1,759,173 0,000 0,00 8, ,989 1,95 1,567 1,936 s (MPa) p max (MPa) s n,min,173 47,8,,173 1,936 68,77 3,59 1,936 MAWP (0 C, new) =,51 MPa AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

15 Conical shell (30.4) internal pressure. AD 000-Merkblätter (07-01) B s n = nominal thickness = 6,00 mm r = Knuckle radius at large end = 0,00 mm p = internal pressure = Half angle = 30 Flare radius at small end = 0,00 mm K/S = Nominal stress T = Temperature D a1 = Large end diameter = 710,00 mm v = Joint efficiency Cone height = 547,85 mm Small end diameter = 393,70 mm c 1 +c = corrosion + tolerance X CrNiMo Plate PWHT : No Radiography : 10% Scope of application sc 1 c / D a r / D a Required thickness of cone. s g = D K p/( K/S vp) (1 / cos)+c 1 +c D = D (s +r(1cos)+x sin) K a1 l p (MPa) T ( C) K/S (MPa) c 1 +c v D k s g Large end Operation Horizontal test 0,8 1, ,4 0 13,67 14,9 0,00+0,00 0,00+0,00 0,85 0,85 676,66 678,5,78,48 Small end Operation 0,8 104,4 13,67 0,00+0,00 0,85 434,84 1,79 Horizontal test 1, ,9 0,00+0,00 0,85 433,81 1,59 MAWP (104,4 C, Corroded) = 1,81 MPa MAWP (0 C, new) =,05 MPa large end junction without knuckle. x 1 x sl Da1 s l DK s g s l : ( AD B Fig ) x 1 Da1 sl c1 c s c cos x.7 Da1 l 1 c 0 x3 0. 5x1 Operation Horizontal test N X s l D a1 x 1 x x 3 3,57 7,00 50,78 38,0 5,39 3,3 7,00 48,97 36,83 4, Small end junction. D a1 Operation Horizontal test x 1 N X 1.4 x s g s l D K s l : ( AD B Fig. 3.8 ) x 1 Da1 sl c1 c s c cos x.7 Da1 l 1 c 0 x3 0. 5x1 s l D a1 x 1 x x 3,63 405,70 3,67 4,57 16,33,41 405,70 31,8 3,53 15,64 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

16 Korbbogen Type Head (5.1) Internal pressure. AD 000-Merkblätter (07-01) B3 h h 1 s e = nominal thickness v = Joint efficiency K/S = Allowable stress T = Temperature s = minimum required thickness = circular stress p = internal pressure p max = Max. allowable pressure R = equivalent inside radius p h = Hydrostatic pressure r = inside knuckle radius D a = External Diameter = 406,4 mm h = outside height = 106,54 mm c 1 +c = corrosion + tolerance h 1 = Knuckle Length = 4 mm Tol % = tolerance for pipes Straight flange = 50,00 mm d i (nozzle : /) s n,min = s/tol % shall be s e P65GH Plate Carbon Steel Schedule : / NPS : / s e = 8,000 mm Tol % = / PWHT : No Radiography : Full Seamless Cor. = 0 mm Tol. = 0 mm TEMA RCB-3.13 = 7,938 mm Operation Horizontal test N X p (MPa) p h (MPa) T ( C) K/S (MPa) v r R 1, ,33 1 6,586 35,10,155 0, ,38 1 6,586 35,10 opening factor : d i /D a design factor : (AD B3 fig 9 ((s e -c 1 -c )/D a )) Da pβ R se p Knuckle thickness : s1 c1 c Head thickness : s c1 c 4 K S v K S v p Da p Cyl. Part thickness : s3 c1 c s = max(s K S v p 1,s,s 3 ) Operation Horizontal test L.T Operation Horizontal test K/S shall be D a N X N X MAWP (60 C, Corroded) = 4,95 MPa R r d i d i /D a (s e -c 1 -c )/D a s 1 s s 3 0,000 0,00 1, ,8 1,779 1,617 1,968 0,000 0,00 1, ,8 1,560 1,418 1,76 s (MPa) p max (MPa) s n,min 1,968 9,88 4,95 1,968 1,76 53,6 10,14 1,76 MAWP (0 C, new) = 7,1 MPa AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

17 Cylindrical shell under internal pressure. AD-Merkblatt B1 et B 10 p = internal pressure K/S = Nominal stress T = temperature in operation D a = External Diameter D i = Internal Diameter v = Joint efficiency s e = nominal thickness c = corrosion + tolerance tol = tolerance for pipes = circular stress va = stress on the outer surface vi = stress on the inner surface s = required wall thickness including allowances s e shall be s s = (e c) tol e = minimum required thickness to withstand to pressure K/S shall be e u = (s e tol) c If D a /D i 1, or If Pipe (with D a 00mm) And D a /D i 1,7 e = D a.p / (K/S.vp) = (D a.p / e u p) / ( v) If D a /D i 1,5 e = D a.p / (,3K/Sp) vi = p (D a + e u ) / (,3 e u ) va = p (D a -3.e u ) / (,3 e u ) = max( vi va ) Shell (0) : (Barrel) X CrNiMo Plate Stainless Steel Schedule : / NPS : / s e = 6,000 mm D i = 710,00 mm Tol % = / PWHT : No Radiography : Spot D a = 7,00 mm Cor. = 0 mm Tol. = 0 mm TEMA RCB-3.13 = 4,76 mm p (MPa) p h (MPa) T ( C) Operation N 0, ,4 Horizontal test X 1,151 0,007 0 MAWP (to 104,4 C, corroded) = 1,89 MPa K/S (MPa) 13,67 14,9 v e u (MPa) p a (MPa) e s 0,85 0,85 6,000 6,000 56,16 80,79 1,89 3,05 PMA (to 0 C, new) =,14 MPa,55,74,55,74 Shell (04) : (Barrel) X CrNiMo Seamless pipe Stainless Steel Schedule : 10 NPS : 16 s e = 6,350 mm D i = 393,70 mm Tol % = 7/8 (1.5%) PWHT : No Radiography : Full D a = 406,40 mm Cor. = 0 mm Tol. = 0 mm TEMA RCB-3.13 = 3, mm p (MPa) p h (MPa) T ( C) Operation N 0, ,4 Horizontal test X 1,1509 0, MAWP (to 104,4 C, corroded) = 3,68 MPa K/S (MPa) 13,67 14,9 v e u (MPa) p a (MPa) e s 1 1 5,556 5,556 8,86 41,51 3,68 5,94 PMA (to 0 C, new) = 4,16 MPa 1, 1,088 1,396 1,44 Shell (10) : 5.06 (Barrel) P65GH Seamless pipe Carbon Steel Schedule : 0 NPS : 16 s e = 7,90 mm D i = 390,56 mm Tol % = 7/8 (1.5%) PWHT : No Radiography : Full D a = 406,40 mm Cor. = Tol. = 0 mm TEMA RCB-3.13 = 7,9 mm p (MPa) p h (MPa) T ( C) Operation N 1, 0 Horizontal test X,155 0,0038 MAWP (to 60 C, corroded) =,08 MPa 3,175 mm 60 0 K/S (MPa) 111,73 5,38 v e u (MPa) p a (MPa) e s 1 1 3,755 3,755 64,34 115,4,08 4,71 PMA (to 0 C, new) = 6,13 MPa,171 1,76 6,109 5,601 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

18 Body flange(s) and cover(s) Body Flange and Cover 5.01 in operation. AD 000-Merkblätter (07-01) B8 Integral with hub Design Pressure p = 1, MPa Corrosion : 3,17 mm Design Temperature T = 60 C Tolerance : 1,6 mm Flange K/S = 104 MPa K 0 /S = 04,76 MPa Material : P65GH E = MPa E 0 = MPa d i = 390,56 mm d a = 515 mm h = 3 mm s F = 1 mm h 1 = 35 mm d 4 = / Raised face (female) height : 5 mm Bolt Material : SA193GRB7 K B /S B = 338,89 MPa K B0 /S B = 556,9 MPa n = 0 = 1 d t = 473 mm d L = 17,5 mm d = 16 mm d K = 14,13 mm S D = 1, Shell K v /S v = 111,73 MPa K V0 /S V = 176,67 MPa d i = 390,56 mm s 1 = 7,9 mm d D = 406,91 mm b = 10 mm h D = 3 mm d Dext = 416,91 mm Gasket b D0 = 10 mm b D = 10 mm k 0 = / k 1 = 5 mm K D0 = / K D = / k 0 K D = 10 N/mm X = / Corroded dimensions h F = 5,4 mm h A = 60,4 mm d i = 396,91 mm s 1 = 4,74 mm s F = 8,8 mm FRB pd i 4 = ,6 dan FFB pd D di 4 = 757,6 dan FDB pd DSDk1 = 90,4 dan FSB FRB FFB FDB = 16.55,6 dan F D = πd D k 0 K D = / FDV d Dk0KD = 1.78,3 dan F * : F F = / FDV FSB : FDV FDV= 1.78,3 dan * DV FSB FDV 0.FDV 0. 8 SBX F SB max DV SB * F = 16.55,6 dan DVX F DV max Bolting F = 1.78,3 dan Actual bolt cross-section : S n 4 = mm Z 4 S Required area : F K / S BN d a a D BN D c 4 req d t d D SB B B B d K S = 487,64 mm D S πn = 5,57 mm c 5 = 3 mm (Z(F SB /(Kn)) 0.5 0) S n = 1.154,13 mm S BNE FDV K B0 / SB0 =,95 mm 5 h h F h A A-A s F d L h 1 B-B a d i s 1 B SR =d t /n = 74,3 mm B SX = 5d L = 87,5 mm B S min = 45 mm F SO = F DVX = 1.78,3 dan F SOmax = VO b D d D = 1.783,5 dan DIN 8090: VO = 10 MPa Fs max = BO b D d D = 1.783,5 dan DIN 8090: BO = 10 MPa F S = F SO (F RB +F FB ) = ,8 dan Bolt Load : F SO /n = 63,9 dan Real bolt stresses : F SBX /S B = 5,7 MPa F SO /S B = 4,1 MPa Design parameters v = 0,6 d L = vd L = 10,55 mm b = d a d i d L = 96,98 mm s F = min(s F,h F /3) = 8,47 mm s m = (s F +s 1 )/ = 6,78 mm B 1 = (h A h F )/h F = 1,378 > 1 (s F +s 1 )/b = 0,14 Configuration out of the scope B = (1+B 1 s m /b)/(1+s m (B 1 + B 1 )/b) = / Z = (d i +s F )s F = 9.059, mm 3 Z 1 = 0.75 (d i +s 1 )s 1 = 6.78,45 mm 3 a A = (d t d i s F )/ = 33,81 mm a D = (d t d D )/ =33,04 mm a B = (d t d i s 1 )/ = 35,67 mm req 4 BN AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

19 Design for bolting-up condition K/S = K 0 /S' F = F DV Section A-A Section B-B FS W a D =.063,03 mm 3 FS W a D =.063,03 mm 3 K K 1.7W Z 1.7W Z hf = 0 mm 1 hf B b b = / DIN 505 (14a) W 505 = / DIN 505 (14b) W 505 = ,4 mm 3 W DIN Flange deflection in the bolt circle F = 0,01 mm tan -1 ( F /a D ) = 0,0 Design for service condition K/S = K/S F = F SB Section A-A Section B-B FS W a A = 53.76,6 mm 3 FS W a B = ,45 mm 3 K K 1.7W Z 1.7W Z1 hf = 0,1 mm hf B b b = / DIN 505 (14a) W 505 = / DIN 505 (14b) W 505 = ,55 mm 3 W DIN Flange deflection in the bolt circle F = 0,15 mm tan -1 ( F /a D ) = 0,7 h Fmin = (h F ) max + tol = 1,7 mm AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

20 Body Flange and Cover in operation. AD 000-Merkblätter (07-01) B8 Integral with hub Design Pressure p = 0,8 MPa Corrosion : 0 mm Design Temperature T = 104,4 C Tolerance : 1,6 mm Flange K/S = 13,67 MPa K 0 /S = 14,9 MPa Material : X CrNiMo E = MPa E 0 = MPa d i = 393,7 mm d a = 515 mm h = 3 mm s F = 10 mm h 1 = 35 mm d 4 = / Raised face (female) height : 5 mm Material : SA193GRB7 K Bolt B /S B = 338,89 MPa K B0 /S B = 556,9 MPa n = 0 = 1 d t = 473 mm d L = 17,5 mm d = 16 mm d K = 14,13 mm S D = 1, Shell K v /S v = 13,67 MPa K V0 /S V = 150 MPa d i = 393,7 mm s 1 = 6,35 mm d D = 406,91 mm b = 10 mm h D = 3 mm d Dext = 416,91 mm Gasket b D0 = 10 mm b D = 10 mm k 0 = / k 1 = 5 mm K D0 = / K D = / k 0 K D = 10 N/mm X = / Corroded dimensions h F = 5,4 mm h A = 60,4 mm d i = 393,7 mm s 1 = 6,35 mm s F = 10 mm FRB pd i 4 = 9.738,9 dan FFB pd D di 4 = 664,5 dan FDB pd DSDk1 = 613,6 dan FSB FRB FFB FDB = dan F D = πd D k 0 K D = / FDV d Dk0KD = 1.78,3 dan F * : F F = / FDV FSB : FDV FDV= 1.78,3 dan * DV FSB FDV 0.FDV 0. 8 SBX F SB max DV SB * F = 16.55,6 dan DVX F DV max Bolting F = 1.78,3 dan Actual bolt cross-section : S n 4 = mm Z 4 S Required area : F K / S BN d a a D BN D c 4 req d t d D SB B B B d K S = 35,09 mm D S πn = 4,55 mm c 5 = 3 mm (Z(F SB /(Kn)) 0.5 0) S n = 895,3 mm S BNE FDV K B0 / SB0 =,95 mm 5 h h F h A A-A s F d L h 1 B-B a d i s 1 B SR =d t /n = 74,3 mm B SX = 5d L = 87,5 mm B S min = 45 mm F SO = F DVX = 1.78,3 dan F SOmax = VO b D d D = 1.783,5 dan DIN 8090: VO = 10 MPa Fs max = BO b D d D = 1.783,5 dan DIN 8090: BO = 10 MPa F S = F SO (F RB +F FB ) = -9.15,1 dan Bolt Load : F SO /n = 63,9 dan Real bolt stresses : F SBX /S B = 5,7 MPa F SO /S B = 4,1 MPa Design parameters v = 0,61 d L = vd L = 10,61 mm b = d a d i d L = 100,08 mm s F = min(s F,h F /3) = 8,47 mm s m = (s F +s 1 )/ = 8,18 mm B 1 = (h A h F )/h F = 1,378 > 1 (s F +s 1 )/b = 0,163 Configuration out of the scope B = (1+B 1 s m /b)/(1+s m (B 1 + B 1 )/b) = / Z = (d i +s F )s F = 8.89,09 mm 3 Z 1 = 0.75 (d i +s 1 )s 1 = 1.098,6 mm 3 a A = (d t d i s F )/ = 35,4 mm a D = (d t d D )/ =33,04 mm a B = (d t d i s 1 )/ = 36,48 mm req 4 BN AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

21 Design for bolting-up condition K/S = K 0 /S' F = F DV Section A-A Section B-B FS W a D = 1.971,33 mm 3 FS W a D = 1.971,33 mm 3 K K 1.7W Z 1.7W Z hf = 0 mm 1 hf B b b = / DIN 505 (14a) W 505 = / DIN 505 (14b) W 505 = ,8 mm 3 W DIN Flange deflection in the bolt circle F = 0,01 mm tan -1 ( F /a D ) = 0,0 Design for service condition K/S = K/S F = F SB Section A-A Section B-B FS W a A = ,49 mm 3 FS W a B = ,8 mm 3 K K 1.7W Z 1.7W Z1 hf = 16,49 mm hf B b b = / DIN 505 (14a) W 505 = / DIN 505 (14b) W 505 = ,6 mm 3 W DIN Flange deflection in the bolt circle F = 0,17 mm tan -1 ( F /a D ) = 0,9 h Fmin = (h F ) max + tol = 18,09 mm AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

22 Body Flange and Cover 5.01 in test. AD 000-Merkblätter (07-01) B8 Integral with hub Design Pressure p =,15 MPa Corrosion : 3,17 mm Design Temperature T = 0 C Tolerance : 1,6 mm Flange K/S = 04,76 MPa K 0 /S = 04,76 MPa Material : P65GH E = MPa E 0 = MPa d i = 390,56 mm d a = 515 mm h = 3 mm s F = 1 mm h 1 = 35 mm d 4 = / Raised face (female) height : 5 mm Bolt Material : SA193GRB7 K B /S B = 556,9 MPa K B0 /S B = 556,9 MPa n = 0 = 1 d t = 473 mm d L = 17,5 mm d = 16 mm d K = 14,13 mm S D = 1, Shell K v /S v = 5,38 MPa K V0 /S V = 176,67 MPa d i = 390,56 mm s 1 = 7,9 mm d D = 406,91 mm b = 10 mm h D = 3 mm d Dext = 416,91 mm Gasket b D0 = 10 mm b D = 10 mm k 0 = / k 1 = 5 mm K D0 = / K D = / k 0 K D = 10 N/mm X = / Corroded dimensions h F = 5,4 mm h A = 60,4 mm d i = 396,91 mm s 1 = 4,74 mm s F = 8,8 mm FRB pd i 4 = 6.63,7 dan FFB pd D di 4 = 1.358,9 dan FDB pd DSDk1 = dan FSB FRB FFB FDB = 9.64,6 dan F D = πd D k 0 K D = / FDV d Dk0KD = 1.78,3 dan F * : F F = / FDV FSB : FDV FDV = 1.78,3 dan * DV FSB FDV 0.FDV 0. 8 SBX F SB max F = 9.64,6 dan Actual bolt cross-section : S n 4 = mm DV SB B d K Required area : F K / K B0 S = 53,6 mm BN SB B0 B SR =d t /n = 74,3 mm B SX = 5d L = 87,5 mm B Smin = 45 mm F SOmax = VO b D d D = 1.783,5 dan F S = F SO (F RB +F FB ) = , dan Real bolt stresses : F SBX /S B = 94,6 MPa DIN 8090: VO = 10 MPa Design parameters v = 0,6 d L = vd L = 10,55 mm b = d a d i d L = 96,98 mm s F = min(s F,h F /3) = 8,47 mm s m = (s F +s 1 )/ = 6,78 mm B 1 = (h A h F )/h F = 1,378 > 1 (s F +s 1 )/b = 0,14 Configuration out of the scope B = (1+B 1 s m /b)/(1+s m (B 1 + B 1 )/b) = / Z = (d i +s F )s F = 9.059, mm 3 Z 1 = 0.75 (d i +s 1 )s 1 = 6.78,45 mm 3 a A = (d t d i s F )/ = 33,81 mm a D = (d t d D )/ =33,04 mm a B = (d t d i s 1 )/ = 35,67 mm Design for service condition K/S = K/S F = F SB Section A-A Section B-B FS W a A = ,77 mm 3 FS W a B = ,6 mm 3 K K h F d a a D d t d D 1.7W Z = 18,48 mm b h h F h A A-A s F d L h 1 B-B a d i s 1 1.7W Z B = / b 1 hf DIN 505 (14a) W 505 = / DIN 505 (14b) W 505 = ,77 mm 3 W DIN Flange deflection in the bolt circle F = 0,5 mm tan -1 ( F /a D ) = 0,44 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

23 Body Flange and Cover in test. AD 000-Merkblätter (07-01) B8 Integral with hub Design Pressure p = 1,15 MPa Corrosion : 0 mm Design Temperature T = 0 C Tolerance : 1,6 mm Flange K/S = 14,9 MPa K 0 /S = 14,9 MPa Material : X CrNiMo E = MPa E 0 = MPa d i = 393,7 mm d a = 515 mm h = 3 mm s F = 10 mm h 1 = 35 mm d 4 = / Raised face (female) height : 5 mm Material : SA193GRB7 K Bolt B /S B = 556,9 MPa K B0 /S B = 556,9 MPa n = 0 = 1 d t = 473 mm d L = 17,5 mm d = 16 mm d K = 14,13 mm S D = 1, Shell K v /S v = 14,9 MPa K V0 /S V = 150 MPa d i = 393,7 mm s 1 = 6,35 mm d D = 406,91 mm b = 10 mm h D = 3 mm d Dext = 416,91 mm Gasket b D0 = 10 mm b D = 10 mm k 0 = / k 1 = 5 mm K D0 = / K D = / k 0 K D = 10 N/mm X = / Corroded dimensions h F = 5,4 mm h A = 60,4 mm d i = 393,7 mm s 1 = 6,35 mm s F = 10 mm FRB pd i 4 = ,7 dan FFB pd D di 4 = 956 dan FDB pd DSDk1 = 88,7 dan FSB FRB FFB FDB = ,4 dan F D = πd D k 0 K D = / FDV d Dk0KD = 1.78,3 dan * F : FDVFSB = / FDV FSB : FDV FDV = 1.78,3 dan F = 9.64,6 dan * DV FSB FDV 0.FDV 0. 8 SBX F SB max Actual bolt cross-section : S n 4 = mm B d K Required area : F K / K B0 S = 84,59 mm BN SB B0 B SR =d t /n = 74,3 mm B SX = 5d L = 87,5 mm B Smin = 45 mm F SOmax = VO b D d D = 1.783,5 dan F S = F SO (F RB +F FB ) = ,3 dan Real bolt stresses : F SBX /S B = 94,6 MPa DIN 8090: VO = 10 MPa Design parameters v = 0,61 d L = vd L = 10,61 mm b = d a d i d L = 100,08 mm s F = min(s F,h F /3) = 8,47 mm s m = (s F +s 1 )/ = 8,18 mm B 1 = (h A h F )/h F = 1,378 > 1 (s F +s 1 )/b = 0,163 Configuration out of the scope B = (1+B 1 s m /b)/(1+s m (B 1 + B 1 )/b) = / Z = (d i +s F )s F = 8.89,09 mm 3 Z 1 = 0.75 (d i +s 1 )s 1 = 1.098,6 mm 3 a A = (d t d i s F )/ = 35,4 mm a D = (d t d D )/ =33,04 mm a B = (d t d i s 1 )/ = 36,48 mm Design for service condition K/S = K/S F = F SB Section A-A Section B-B FS W a A = 48.99,51 mm 3 FS W a B = ,5 mm 3 K K h F d a a D d t d D 1.7W Z = 18,7 mm b h h F h A A-A s F d L h 1 B-B a d i s 1 1.7W Z B = / b 1 hf DIN 505 (14a) W 505 = / DIN 505 (14b) W 505 = ,8 mm 3 W DIN Flange deflection in the bolt circle F = 0,9 mm tan -1 ( F /a D ) = 0,51 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

24 Body Flange and Cover 3903 in test. AD 000-Merkblätter (07-01) B8 Backing Flange Design Pressure p =,15 MPa Corrosion : 0 mm Design Temperature T = 0 C Tolerance : 1,6 mm Flange K/S = 33,33 MPa K 0 /S = 33,33 MPa Material : P65GH E = MPa E 0 = MPa d i = 393,7 mm d a = 515 mm h = 3 mm s F = / h 1 = / d 4 = 416,91 mm Flat face Bolt Material : SA193GRB7 K B /S B = 556,9 MPa K B0 /S B = 556,9 MPa n = 0 = 1 d t = 473 mm d L = 17,5 mm d = 16 mm d K = 14,13 mm S D = 1, Shell K v /S v = 14,9 MPa K V0 /S V = 150 MPa d i = 0 mm s 1 = 0 mm d D = 406,91 mm b = 10 mm h D = 3 mm d Dext = 416,91 mm Gasket b D0 = 10 mm b D = 10 mm k 0 = / k 1 = 5 mm K D0 = / K D = / k 0 K D = 10 N/mm X = / Corroded dimensions h F = 30,4 mm h A = / d = / s 1 = / s F = / FRB pd i 4 = 6.03,6 dan FFB pd D di 4 = 1.787,9 dan FDB pd DSDk1 = dan FSB FRB FFB FDB = 9.64,6 dan F D = πd D k 0 K D = / FDV d Dk0KD = 1.78,3 dan F * : F F = / FDV FSB : FDV FDV= 1.78,3 dan * DV FSB FDV 0.FDV 0. 8 SBX F SB max DV SB * F = 9.64,6 dan DVX F DV max Bolting F = 1.78,3 dan Actual bolt cross-section : S n 4 = mm Z 4 S Required area : F K / S BN d a d t BN D c 4 req a SB B B B d K S = 53,6 mm D S πn = 5,8 mm c 5 = 3 mm (Z(F SB /(Kn)) 0.5 0) S n = 53,6 mm S BNE FDV K B0 / SB0 =,95 mm 5 h F d i d L B SR =d t /n = 74,3 mm B SX = 5d L = 87,5 mm B S min = 45 mm F SO = User Defined = 1.78,3 dan > F DV F SOmax = VO b D d D = 1.783,5 dan DIN 8090: VO = 10 MPa Fs max = BO b D d D = 1.783,5 dan DIN 8090: BO = 10 MPa F S = F SO (F RB +F FB ) = , dan Bolt Load : F SO /n = 63,9 dan Real bolt stresses : F SBX /S B = 94,6 MPa F SO /S B = 4,1 MPa Design parameters v = 0,61 d L = vd L = 10,61 mm b = d a d i d L = 100,08 mm a = (d t d 4 )/ = 8,04 mm a = (d t d i s 1 )/ = / a D = (d t d 4 )/ = 8,04 mm req 4 BN Design for bolting-up condition K/S = K 0 /S' F = F DV W FS a K D = 1.536,48 mm 3 1.7W hf b Design for service condition K/S = K/S F = F SB W FS a K = 35.68,9 mm 3 1.7W hf b = 4,4 mm = 1,6 mm F pf 1. 7 d SB 4 di = 0,01 MPa 5 MPa AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

25 Tubesheet(s) and Expansion Joint Tubesheet, Loading conditions 1 [corroded normal condition] AD 000-Merkblatt B 5, AD B5 ch 6.7. Plate Tubeside Shellside Tubes Tubeside Shellside Pressure p i = 1, MPa p u = 0,8 MPa Corrosion c i = 3,17 mm c u = 0 mm Material X CrNiMo XCrNiMo17-1- Design Temperature 60 C 60 C / / Nominal stress K/S = 103,1 MPa K 0 /S 0 = / K t /S t = 100,9 MPa / / Modulus of elasticity E = MPa E t = MPa / / Nominal thicknesses s a = 43 mm s t =,11 mm 3,76 mm 5,56 mm Diameter D a = 416,91 mm d a =5,4 mm d i =1,18 m m D It = 398,89 mm D Ic = 395,9 mm Tolerance c 1 = 1,6 mm Pattern Rotated Triangular n = 56 A ro = / t = 31,75 mm l A = / d t D It s R d Dt s a D Ic d Dc Tubeside Shellside Design Diameter : D 1t = 406,91 mm D 1c = 406,91 mm Partition groove depth : 0 mm 5 mm d t = 473 mm d Dc = 406,91 mm Peripheral extra thicknesses : 10 mm Central extra thicknesses xx: 5 mm Design parameters Exp. Length : l * w * d a max d a Et st E * t da Ligament efficiency v Tube cross-section : At t Kt K da di 4 * l w s d a ; 1. l * w d * a v A t stationary Tubesheet 1 mm 4,5 mm 0, ,5 mm Calculation of tube loads di πpi di πp Tensile load / inner tube : Fti Compressive load / inner tube : F i ci 4 4 Maximum load / tube F R = max (F ti, F ci ) F ti F ci F R 43 N 0 N 43 N Calculation of admissible loads per tube In tensile/compressive case : FTX At Kt St = N F R F TX Tube-to-Tubesheet Joint Minimum expanded length : -Even l w1 = F R / [150 min(d a d i, 0.1d a )] -With groove l w = F R / [300 min(d a d i, 0.1d a )] -With flange l w3 = F R / [400 min(d a d i, 0.1d a )] Welded tubes : -Minimum thickness of welded joints g = 0.4(F R S)/(d a K) l w1 l w l w3 g 1,11 mm 0,56 mm 0,4 mm / Connection-manufacturing must respect code rules (AD B : l w mini = 1 mm) AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

26 Theoretical thickness at center of tubesheet TABLE 1 fig g 1 4 k 1 s D CD ps Kv s 1 1 Shellside Tubeside C d t /d D C 1 s 1 s = (s 1 ) max 0,4 / / / 9,5 mm 36,13 mm 0,4 / / / 36,13 mm Required thickness at peripheral part of tubesheet At the level of the stress-relieving grooves D1c 1.3S D1t 1.3S sr1 p rc s p rt K K R s 0. s xx c R 7 s R1 s R s R / / 9,91 mm 1 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

27 Tubesheet, Loading conditions [corroded normal condition] AD 000-Merkblatt B 5, AD B5 ch 6.7. Plate Tubeside Shellside Tubes Tubeside Shellside Pressure p i = 1, MPa p u = 0 MPa Corrosion c i = 3,17 mm c u = 0 mm Material X CrNiMo XCrNiMo17-1- Design Temperature 60 C 60 C / / Nominal stress K/S = 103,1 MPa K 0 /S 0 = / K t /S t = 100,9 MPa / / Modulus of elasticity E = MPa E t = MPa / / Nominal thicknesses s a = 43 mm s t =,11 mm 3,76 mm 5,56 mm Diameter D a = 416,91 mm d a =5,4 mm d i =1,18 m m D It = 398,89 mm D Ic = 395,9 mm Tolerance c 1 = 1,6 mm Pattern Rotated Triangular n = 56 A ro = / t = 31,75 mm l A = / d t D It s R d Dt s a D Ic d Dc Tubeside Shellside Design Diameter : D 1t = 406,91 mm D 1c = 406,91 mm Partition groove depth : 0 mm 5 mm d t = 473 mm d Dc = 406,91 mm Peripheral extra thicknesses : 10 mm Central extra thicknesses xx: 5 mm Design parameters Exp. Length : l * w * d a max d a Et st E * t da Ligament efficiency v Tube cross-section : At t Kt K da di 4 * l w s d a ; 1. l * w d * a v A t stationary Tubesheet 1 mm 4,5 mm 0, ,5 mm Calculation of tube loads di πpi di πp Tensile load / inner tube : Fti Compressive load / inner tube : F i ci 4 4 Maximum load / tube F R = max (F ti, F ci ) F ti F ci F R 43 N 0 N 43 N Calculation of admissible loads per tube In tensile/compressive case : FTX At Kt St = N F R F TX Tube-to-Tubesheet Joint Minimum expanded length : -Even l w1 = F R / [150 min(d a d i, 0.1d a )] -With groove l w = F R / [300 min(d a d i, 0.1d a )] -With flange l w3 = F R / [400 min(d a d i, 0.1d a )] Welded tubes : -Minimum thickness of welded joints g = 0.4(F R S)/(d a K) l w1 l w l w3 g 1,11 mm 0,56 mm 0,4 mm / Connection-manufacturing must respect code rules (AD B : l w mini = 1 mm) AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

28 Theoretical thickness at center of tubesheet TABLE 1 fig g 1 4 k 1 s D CD ps Kv s 1 1 C d t /d D C 1 s 1 s = (s 1 ) max Tubeside 0,4 / / / 36,13 mm 36,13 mm Required thickness at peripheral part of tubesheet At the level of the stress-relieving grooves D1c 1.3S D1t 1.3S sr1 p rc s p rt K K R sr 0. 7s xx c1 s R1 s R s R / / 9,91 mm AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

29 Tubesheet, Loading conditions 3 [corroded normal condition] AD 000-Merkblatt B 5, AD B5 ch 6.7. Plate Tubeside Shellside Tubes Tubeside Shellside Pressure p i = 0 MPa p u = 0,8 MPa Corrosion c i = 3,17 mm c u = 0 mm Material X CrNiMo XCrNiMo17-1- Design Temperature 60 C 60 C / / Nominal stress K/S = 103,1 MPa K 0 /S 0 = / K t /S t = 100,9 MPa / / Modulus of elasticity E = MPa E t = MPa / / Nominal thicknesses s a = 43 mm s t =,11 mm 3,76 mm 5,56 mm Diameter D a = 416,91 mm d a =5,4 mm d i =1,18 m m D It = 398,89 mm D Ic = 395,9 mm Tolerance c 1 = 1,6 mm Pattern Rotated Triangular n = 56 A ro = / t = 31,75 mm l A = / d t D It s R d Dt s a D Ic d Dc Tubeside Shellside Design Diameter : D 1t = 406,91 mm D 1c = 406,91 mm Partition groove depth : 0 mm 5 mm d t = 473 mm d Dc = 406,91 mm Peripheral extra thicknesses : 10 mm Central extra thicknesses xx: 5 mm Design parameters Exp. Length : l * w * d a max d a Et st E * t da Ligament efficiency v Tube cross-section : At t Kt K da di 4 * l w s d a ; 1. l * w d * a v A t stationary Tubesheet 1 mm 4,5 mm 0, ,5 mm Calculation of tube loads di πpi di πp Tensile load / inner tube : Fti Compressive load / inner tube : F i ci 4 4 Maximum load / tube F R = max (F ti, F ci ) F ti F ci F R 0 N 0 N 0 N Calculation of admissible loads per tube In tensile/compressive case : FTX At Kt St = N F R F TX Tube-to-Tubesheet Joint Minimum expanded length : -Even l w1 = F R / [150 min(d a d i, 0.1d a )] -With groove l w = F R / [300 min(d a d i, 0.1d a )] -With flange l w3 = F R / [400 min(d a d i, 0.1d a )] Welded tubes : -Minimum thickness of welded joints g = 0.4(F R S)/(d a K) l w1 l w l w3 g 0 mm 0 mm 0 mm / Connection-manufacturing must respect code rules (AD B : l w mini = 1 mm) AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

30 Theoretical thickness at center of tubesheet TABLE 1 fig g 1 4 k 1 s D CD ps Kv s 1 1 C d t /d D C 1 s 1 s = (s 1 ) max Shellside 0,4 / / / 9,5 mm 9,5 mm Required thickness at peripheral part of tubesheet At the level of the stress-relieving grooves D1c 1.3S D1t 1.3S sr1 p rc s p rt K K R sr 0. 7s xx c1 s R1 s R s R / / 5,7 mm AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

31 Tubesheet, Loading conditions T0 [test condition] AD 000-Merkblatt B 5, AD B5 ch 6.7. Plate Tubeside Shellside Tubes Tubeside Shellside Pressure p p i = 0 MPa u = 1,144 MPa Corrosion c i = 3,17 mm c u = 0 mm Material X CrNiMo XCrNiMo17-1- Design Temperature 0 C 0 C / / Nominal stress K/S = 14,3 MPa K 0 /S 0 = / K t /S t = 14,3 MPa / / Modulus of elasticity E = MPa E t = MPa / / Nominal thicknesses s a = 43 mm s t =,11 mm 3,76 mm 5,56 mm Diameter D a = 416,91 mm d a =5,4 mm d i =1,18 m m D It = 398,89 mm D Ic = 395,9 mm Tolerance c 1 = 1,6 mm Pattern Rotated Triangular n = 56 A ro = / t = 31,75 mm l A = / d t D It s R d Dt s a D Ic d Dc Tubeside Shellside Design Diameter : D 1t = 406,91 mm D 1c = 406,91 mm Partition groove depth : 0 mm 5 mm d t = 473 mm d Dc = 406,91 mm Peripheral extra thicknesses : 10 mm Central extra thicknesses xx: 5 mm Design parameters Exp. Length : l * w * d a max d a Et st E * t da Ligament efficiency v Tube cross-section : At t Kt K da di 4 * l w s d a ; 1. l * w d * a v A t stationary Tubesheet 1 mm 4, mm 0, ,5 mm Calculation of tube loads di πpi di πp Tensile load / inner tube : Fti Compressive load / inner tube : F i ci 4 4 Maximum load / tube F R = max (F ti, F ci ) F ti F ci F R 0 N 0 N 0 N Calculation of admissible loads per tube In tensile/compressive case : FTX At Kt St = N F R F TX Tube-to-Tubesheet Joint Minimum expanded length : -Even l w1 = F R / [150 min(d a d i, 0.1d a )] -With groove l w = F R / [300 min(d a d i, 0.1d a )] -With flange l w3 = F R / [400 min(d a d i, 0.1d a )] Welded tubes : -Minimum thickness of welded joints g = 0.4(F R S)/(d a K) l w1 l w l w3 g 0 mm 0 mm 0 mm / Connection-manufacturing must respect code rules (AD B : l w mini = 1 mm) AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

32 Theoretical thickness at center of tubesheet TABLE 1 fig g 1 4 k 1 s D CD ps Kv s 1 1 C d t /d D C 1 s 1 s = (s 1 ) max Shellside 0,4 / / / 4,43 mm 4,43 mm Required thickness at peripheral part of tubesheet At the level of the stress-relieving grooves D1c 1.3S D1t 1.3S sr1 p rc s p rt K K R sr 0. 7s xx c1 s R1 s R s R / / 1,7 mm AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

33 Tubesheet, Loading conditions 0T [test condition] AD 000-Merkblatt B 5, AD B5 ch 6.7. Plate Tubeside Shellside Tubes Tubeside Shellside Pressure p i =,149 MPa p u = 0 MPa Corrosion c i = 3,17 mm c u = 0 mm Material X CrNiMo XCrNiMo17-1- Design Temperature 0 C 0 C / / Nominal stress K/S = 14,3 MPa K 0 /S 0 = / K t /S t = 14,3 MPa / / Modulus of elasticity E = MPa E t = MPa / / Nominal thicknesses s a = 43 mm s t =,11 mm 3,76 mm 5,56 mm Diameter D a = 416,91 mm d a =5,4 mm d i =1,18 m m D It = 398,89 mm D Ic = 395,9 mm Tolerance c 1 = 1,6 mm Pattern Rotated Triangular n = 56 A ro = / t = 31,75 mm l A = / d t D It s R d Dt s a D Ic d Dc Tubeside Shellside Design Diameter : D 1t = 406,91 mm D 1c = 406,91 mm Partition groove depth : 0 mm 5 mm d t = 473 mm d Dc = 406,91 mm Peripheral extra thicknesses : 10 mm Central extra thicknesses xx: 5 mm Design parameters Exp. Length : l * w * d a max d a Et st E * t da Ligament efficiency v Tube cross-section : At t Kt K da di 4 * l w s d a ; 1. l * w d * a v A t stationary Tubesheet 1 mm 4, mm 0, ,5 mm Calculation of tube loads di πpi di πp Tensile load / inner tube : Fti Compressive load / inner tube : F i ci 4 4 Maximum load / tube F R = max (F ti, F ci ) F ti F ci F R 757 N 0 N 757 N Calculation of admissible loads per tube In tensile/compressive case : FTX At Kt St = N F R F TX Tube-to-Tubesheet Joint Minimum expanded length : -Even l w1 = F R / [150 min(d a d i, 0.1d a )] -With groove l w = F R / [300 min(d a d i, 0.1d a )] -With flange l w3 = F R / [400 min(d a d i, 0.1d a )] Welded tubes : -Minimum thickness of welded joints g = 0.4(F R S)/(d a K) l w1 l w l w3 g 1,99 mm 0,99 mm 0,75 mm / Connection-manufacturing must respect code rules (AD B : l w mini = 1 mm) AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

34 Theoretical thickness at center of tubesheet TABLE 1 fig g 1 4 k 1 s D CD ps Kv s 1 1 C d t /d D C 1 s 1 s = (s 1 ) max Tubeside 0,4 / / / 33,47 mm 33,47 mm Required thickness at peripheral part of tubesheet At the level of the stress-relieving grooves D1c 1.3S D1t 1.3S sr1 p rc s p rt K K R sr 0. 7s xx c1 s R1 s R s R / / 8,05 mm AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

35 Tubes of the bundle. Tube of bundle in internal pressure. Material : XCrNiMo17-1- Seamless tube temperature in operation : T = 60 C Joint efficiency : v = 1 Stainless Steel Nominal thickness : s e =,11 mm External Diameter : D a = 5,40 mm p = internal pressure K/S = Allowable stress c = corrosion + tolerance e = minimum required thickness = circular stress p max = maximum allowable pressure Horizontal test Operation p (MPa) K/S (MPa) e+c (MPa) c p max (MPa), ,9 0,34 13,31 0,1 34,5953 1, 100,93 0,36 7,43 0,1 16,951 Minimum U-Bends thickness TEMA RCB-.31 : t o = t 1 [1+d o /(4R)] = 0,4 mm (R = 38,1 mm ) Tube of bundle in external pressure. Material : XCrNiMo17-1- Seamless tube p = External Pressure t = Temperature Stainless Steel K/S= Allowable stress E = modulus of elasticity = 0.3 Analysis thickness : s e = 1,90 mm External Diameter : D a = 5,40 mm c 1 +c = corrosion + tolerance AD 000-Merkblätter (07-01) [AD B 6 7] 3 K s l =.454,00 mm E s p u = 1.5% 1 = 1 e c c p = 1 1 e c c S D S a u D l D k 1 D 1 a a a 100s c c p (MPa) t ( C) K/S (MPa) E (MPa) S k c 1 +c min(p 1 ; p ) (MPa) 1, , , 0,1 4,615 0, , ,1 11,593 Minimum U-Bends thickness TEMA RCB-.31 : t o = t 1 [1+d o /(4R)] = 0,74 mm (R = 38,1 mm ) e 1 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

36 Vessel under combination loading Model for stress analysis due to supporting. Reaction per support, bending moment and shear loads is done from a beam model simply supported, one of the support is fix at left or right of the beam. The beam study use the reduction matrix method found on the Falk transmission matrix. Boundary conditions allow solving slope and moment not affected when crossing the support. External single load and moment are applied at their acting point and are considered as a discontinuity as an inertia or modulus of elasticity change. Distributed loads do not constitute a discontinuity. Reference axis are : beam x on the right, y up with positive loads down, moments > 0 from x to y. Shell own weight, liquid, and bundle are considered as distributed loads while head weight, flange and cover, floating head and nozzle are considered as concentrated loads. Termination heads are removed and replaced as a concentrated load and an external moment. The resultant of the hydrostatic pressure applied to its location also result in an external moment. For each study case, analysis is done for the vertical and/or horizontal plan. Saddle reactions and bending moment used for shell stresses check are the vector sum of the two plans. This also provides the new angle where the shell stress check must be done Thermal effects are due to the friction factor at the bottom of the saddle and results in an additional moment at the saddle location. Fixed saddle resists to all others. ( = 0,3) Principal stresses are f 1 = 0.5[ σ θ + σ z + (σ θ σ z ) + 4 ] and f = 0.5[ σ θ + σ z (σ θ σ z ) + 4 ] and general primary membrane stress intensity is σ eq = max( f 1 f ; f p ; f +0.5p ), with σ θ : circumferential stress, σ z : longitudinal stress and : shear stress. Stresses in saddle are studied in the 3 axes. For wind and earthquake design purpose, vibration period are evaluated from the general modal equation [k-ω².m] Φ = 0 and solving the eigenvectors and eigenvalues. The flexibility matrix 1/k is found from the beam analysis method, using unit loads applied one after one at the masse location. The dynamic matrix is found to be 1/g.1/k.m with g = acceleration due to gravity and m = mass matrix. Eigenvectors correspond to the natural modes and eigenvalues to their frequencies. Subtracting the contribution of the studied mode from the starting vector allows converging to higher modes Dunkerley method is used for stacked vessels. This enables to find the global circular frequency to 1/ω = /ω 1 where ω 1 is the circular frequency of one vessel. Finally the vibration period is T = π/ω AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

37 Location of dominant stresses and worst cases. Studied cases : 1 Operation Int.Max.P. (Corroded Weight) Lifting (New Weight) 3 Erected (New Weight) During test Int.Max.P. (Corroded Weight) Shutdown (Corroded Weight) During test P = 0. (Corroded Weight) () vertical downside and horizontal longitudinal to the right () vertical upside and horizontal longitudinal to the right () vertical downside and horizontal longitudinal to the left () vertical upside and horizontal longitudinal to the left () vertical downside and horizontal cross () vertical upside and horizontal cross Out the plane of the supports 1 10[01] Primary membrane stress intensity (highest point) 38,7 111,7 MPa (35%) / / Longitudinal compressive stress (highest point) / 1 10[01] Primary membrane stress intensity (lowest point) 38,6 111,7 MPa (35%) 6 0[01] Longitudinal compressive stress (lowest point) 1,8 14,3 MPa (1%) 4 0[01] Stability 0, (1%) In the plane of the supports 1 No. Primary membrane stress intensity (highest point, left) 30, 13,7 MPa (3%) 4 No. 1 Primary membrane stress intensity (highest point, right) 48,6 14,3 MPa (3%) 1 No. Primary membrane stress intensity (lowest point, left) 7, 13,7 MPa (0%) 1 No. 1 Primary membrane stress intensity (lowest point, right) 6,8 13,7 MPa (0%) / No. / Longitudinal compressive stress (highest point, left) / / No. / Longitudinal compressive stress (highest point, right) / 6 No. 1 Longitudinal compressive stress (lowest point, left) 7,5 14,3 MPa (4%) 6 No. 1 Longitudinal compressive stress (lowest point, right) 7,5 14,3 MPa (4%) 4 No. 1 Tangential shearing stress in the shell 3, 171,4 MPa (%) / No. / Tangential shearing stress in the head / 4 No. 1 Circumferential stress (compression) (edge of support) 0,6 14,3 MPa (0%) / No. / Circumferential stress (compression) (edge of the plate) / 4 No. 1 Circumferential stress (compression + bending) (edge of the support) 5, 67,9 MPa (9%) / No. / Circumferential stress (compression + bending) (edge of the plate) / / No. / Circumferential stress (compression + bending) (edge of the support + stiffener) / / No. / Circumferential stress (compression + bending) (edge of the plate + stiffener) / / No. / Circumferential stress (compression + bending) in stiffener (edge of the support) / / No. / Circumferential stress (compression + bending) in stiffener (edge of the plate) / In the supports 4 No. 1 Stress at the low point of the saddle,7 38,5 MPa (1%) 1 No. 1 Maximum bending stress 1,3 16,9 MPa (1%) / No. / Compressive stress / 1 No. 1 Bending and compression combination 0, (1%) 1 No. Tensile stress in the bolts -6,8 100 MPa (-7%) 4 No. 1 Stability (Ribs Number ) 1.059,3 8.66,5 dan (1%) 1 No. Shear stress in the bolts 1,7 100 MPa (%) AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

38 Case 1 - Operation Int.Max.P. (Corroded Weight). Moments and loads in plane of saddles. N o. Support saddles Location Stiffness (dan/mm) Reactions (dan) ,0 14,9.600,0 68,7 Vertical Horizontal Combined Shear Force (dan) -143,0 71,9-90,1 178,7 Bending moments (dan m) -94,9-137,6-151,1-108,4 Graph of bending moments and shear forces. Reactions Transverse (dan) Shear Force (dan) Bending moments (dan m) Reactions Longitudinal (dan) Reactions (dan) 0,0 0,0 0,0 75,9 14,9 0,0 0,0 0,0-75,9 68,7 Shear Force (dan) -143,0 71,9-90,1 178,7 Bending moments (dan m) -94,9-137,6-151,1-108,4 Vertical Moment Horizontal 100 dan m 1 dan m 1 Shear 100 dan 1 dan 1 Periods and Center of Gravity. Mode Center of Gravity Period 4, s 3, s 886, s 631, s 404, s mm maximum Longitudinal Bending Stresses Verification. Circumferential stress : = (P+P )R / t P : Hydrostatic pressure f t : allowable tensile stress Longitudinal stress : z = P m R / t M K 1 / R t P m : Pressure at the vessel equator f c : allowable compressive stress General primary membrane stress intensity : eq = MAX( - z ; z 0.5 P ) K 1 : Coef. EN ( ) Maximum allowable moment : M max = R t f c P max : allowable external pressure Component : 0[01] P = 0,8 MPa Maximum general primary membrane stress intensity : eq shall be f t Location M (dan m) R K 1 P m (MPa) (MPa) z (MPa) eq (MPa) v f t (MPa).599, ,1 358,0 1,94 0,80 47,73 4,68 9,50 0,85 13,67.599, ,1 358,0 1,94 0,80 47,73 3,06 9,03 0,85 13,67 Maximum longitudinal compressive stress : z < 0 z shall be MIN( f t ; f c ) Location M (dan m) R K 1 P m (MPa) z (MPa) v f t (MPa) f c (MPa) 0,0 - -1,8 358,0 1,94 0,80 3, ,67 198,65.599, ,1 358,0 1,94 0,80 3, ,67 198,65 Proof of stability : P / P max + M / M max shall be 1.0 (P > 0 P = 0) Location =.599 mm f c = 198,65 MPa M = -151,1 dan m M max = ,7 dan m P max = + MPa Stab. = 0,0031 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

39 Component : 03[0] 30.4 P = 0,8 MPa Maximum general primary membrane stress intensity : eq shall be f t Location M (dan m) R K 1 P m (MPa) (MPa) z (MPa) eq (MPa) v f t (MPa).600, ,6 358,5 1,94 0,80 47,80 8,6 33,7 0,85 13,67.600, ,6 358,5 1,94 0,80 47,80 6,9 3,15 0,85 13,67 Maximum longitudinal compressive stress : z < 0 z shall be MIN( f t ; f c ) Location M (dan m) R K 1 P m (MPa) z (MPa) v f t (MPa) f c (MPa) 3.147,8 - -4,9 00,3 1,0000 0,80 15, ,67 354, ,8 + -4,9 00,3 1,0000 0,80 15, ,67 354,1 Proof of stability : P / P max + M / M max shall be 1.0 (P > 0 P = 0) Location =.600 mm f c = 198,14 MPa M = -108,6 dan m M max = ,7 dan m P max = + MPa Stab. = 0,003 Component : 04[01] P = 0,8 MPa Maximum general primary membrane stress intensity : eq shall be f t Location M (dan m) R K 1 P m (MPa) (MPa) z (MPa) eq (MPa) v f t (MPa) 3.147,8 - -4,9 00,4 1,0000 0,80 8,86 14,78 17,86 0,85 13, ,8 + -0,7 00,4 1,0000 0,80 8,86 14,13 17,10 0,85 13,67 Maximum longitudinal compressive stress : z < 0 z shall be MIN( f t ; f c ) Location M (dan m) R K 1 P m (MPa) z (MPa) v f t (MPa) f c (MPa) 3.180,8 - -0,7 00,4 1,0000 0,80 14,7 1 13,67 38, ,8 + -4,9 00,4 1,0000 0,80 14, ,67 38,59 Proof of stability : P / P max + M / M max shall be 1.0 (P > 0 P = 0) Location = 3.147,8 mm f c = 38,59 MPa M = -4,9 dan m M max = 3.039,9 dan m P max = + MPa Stab. = 0,0011 Component : 10[01] 5.06 P = 1, MPa Maximum general primary membrane stress intensity : eq shall be f t Location M (dan m) R K 1 P m (MPa) (MPa) z (MPa) eq (MPa) v f t (MPa) 3.343,8 - -7,0 01,3 1,0130 1,0 64,34 3,3 38,73 0,85 111, ,8 + 0,0 01,3 1,0130 1,0 64,34 3,17 38,55 0,85 111,73 Maximum longitudinal compressive stress : z < 0 z shall be MIN( f t ; f c ) Location M (dan m) R K 1 P m (MPa) z (MPa) v f t (MPa) f c (MPa) 3.597,8-0,0 01,3 1,0130 1,0 3, ,73 6, ,8 + -7,0 01,3 1,0130 1,0 3, ,73 6,38 Proof of stability : P / P max + M / M max shall be 1.0 (P > 0 P = 0) Location = 3.343,8 mm f c = 6,38 MPa M = -7 dan m M max = 10.84,1 dan m P max = + MPa Stab. = 0,0006 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

40 Saddle No. 1 Calculation method : BS Zick informations Material of saddle : P65GH Pressure : pm = 0,8 MPa Horizontal reaction (longitudinal) : RaHL = 75,9 dan Horizontal reaction (cross) : RaH = 0 dan Maximum shear force : T = 143 dan Shell Head Stiffener Distance A = mm Length L = 3.47,8 mm Weight of saddle : Ws = 38, dan Vertical Load : RaV = 14,9 dan Reaction at support : Q = 14,9 dan Allowable stress f 13,7 MPa Allowable stress fr / All. compres. stress fc 13,7 MPa Thickness t1 10 mm Modulus of elasticity E MPa Width br 00 mm Thickness ts 6 mm Pad Angle ra 13,7 (not considered) Mean radius r 358 mm r = ra.arctan ( RaH / RaV) 13,7 Allowable stress fe 13,7 MPa b = b1+10ts = 30 mm Thickness te 6 mm A +1 = 13 Depth b 186, mm Yield Strength Leb 41 MPa Allowable stress ff / Width b1 170 mm Saddle Angle A 10 = A.arctan ( RaH / RaV) 10 Longitudinal stresses at the saddle pm.r M4 f3 = = 7,55 MPa / 9,1 MPa ts K1 r ts pm.r M4 f4 = = 1,8 MPa / 0,91 MPa ts Kr ts eq = 7,95 MPa / 9,61 MPa f (13,67 MPa) If f3 < 0 (Compressive) : f3 fc (13,67 MPa) eq = 5,91 MPa / 6,83 MPa f (13,67 MPa) If f4 < 0 (Compressive) : f4 fc (13,67 MPa) M 4 = -94,89 dan m / -137,57 dan m K1 = 0,107 K = 0,19 = p.r / ts (p = 0,8 MPa) shear stress K 3 = 1,1707 Circumferential stresses b = b ts = 30 mm K 5 = 0,076 K 6 = 0,059 q =K 3.T/(r.ts) = 0,78 MPa 106,13 MPa [Min(0.8 f, 0.06 E ts/r)] f 5 = - K 5.Q/(b.ts) = -0,1 MPa f 5 f f 6 = -Q/(4ts.b ) - 3K 6.Q/(ts ) = -5,1 MPa f f Design of saddle Stress due to horizontal reaction on the saddle (BS/PD5500 G ) K 9 = 0,035 H = K 9 Q = 437 N A b = 1.193,3 mm S b = H / (/3 A b ) = 0,55 MPa (90% Leb) (16,9 MPa) Bending and compression stresses I zz = 59, mm 4 S zz = I zz /v = mm 3 I xx = 14, mm 4 S xx = I xx /v = ,9 mm 3 M zz = 0 dan m Sb z = M zz / S zz M xx = 15,19 dan m Sb x = M xx / S xx Sb z = 0 MPa (90% Leb) (16,9 MPa) Sb x = 1,8 MPa (90% Leb) (16,9 MPa) A = mm f b = 160,67 MPa Sb c = Ra V / A Sb c = 0 MPa (0.8 f b ) (18,53 MPa) max(sb z ; Sb x ) / (90% Leb) + Sb c / (0.8 f b ) 1 Stability of web plate [CODAP C9.3..7] [AD S3/ 6.1.1] h b = 380,5 mm l b = 65,3 mm e ba = 10 mm E b = MPa f b = 90% Leb = 16,9 MPa b = f b 10 3 / E b x = h b / l b K b = 1,616 = 0,576 Q max = l b e ba f b = ,4 dan AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

41 Saddle No. Calculation method : BS Zick informations Material of saddle : P65GH Pressure : pm = 0,8 MPa Horizontal reaction (longitudinal) : RaHL = -75,9 dan Horizontal reaction (cross) : RaH = 0 dan Maximum shear force : T = 178,7 dan Shell Head Stiffener Distance A = 647,8 mm Length L = 3.47,8 mm Weight of saddle : Ws = 38, dan Vertical Load : RaV = 68,7 dan Reaction at support : Q = 68,7 dan Allowable stress f 13,7 MPa Allowable stress fr / All. compres. stress fc 13,7 MPa Thickness t1 10 mm Modulus of elasticity E MPa Width br 00 mm Thickness ts 6 mm Pad Angle ra 13,66 (not considered) Mean radius r 358,9 mm r = ra.arctan ( RaH / RaV) 13,66 Allowable stress fe / b = b1+10ts = 30 mm Thickness te / A +1 = 13 Depth b / Yield Strength Leb 41 MPa Allowable stress ff / Width b1 170 mm Saddle Angle A 10 = A.arctan ( RaH / RaV) 10 Longitudinal stresses at the saddle pm.r M4 f3 = = 9,77 MPa / 8,1 MPa ts K1 r ts pm.r M4 f4 = = 0,69 MPa / 1,61 MPa ts Kr ts eq = 30,17 MPa / 8,5 MPa f (13,67 MPa) If f3 < 0 (Compressive) : f3 fc (13,67 MPa) eq = 7,16 MPa / 6,5 MPa f (13,67 MPa) If f4 < 0 (Compressive) : f4 fc (13,67 MPa) M 4 = -151,1 dan m / -108,43 dan m K1 = 0,107 K = 0,19 = p.r / ts (p = 0,8 MPa) shear stress K 3 = 1,1707 Circumferential stresses b = b ts = 30 mm K 5 = 0,076 K 6 = 0,059 q =K 3.T/(r.ts) = 0,97 MPa 106,13 MPa [Min(0.8 f, 0.06 E ts/r)] f 5 = - K 5.Q/(b.ts) = -0,15 MPa f 5 f f 6 = -Q/(4ts.b ) - 3K 6.Q/(ts ) = -6,4 MPa f f Design of saddle Stress due to horizontal reaction on the saddle (BS/PD5500 G ) K 9 = 0,035 H = K 9 Q = 547 N A b = 1.196,4 mm S b = H / (/3 A b ) = 0,69 MPa (90% Leb) (16,9 MPa) Bending and compression stresses I zz = 77, mm 4 S zz = I zz /v = ,1 mm 3 I xx = 8, mm 4 S xx = I xx /v = ,3 mm 3 M zz = 0 dan m Sb z = M zz / S zz M xx = 15,19 dan m Sb x = M xx / S xx Sb z = 0 MPa (90% Leb) (16,9 MPa) Sb x = 0,79 MPa (90% Leb) (16,9 MPa) A = mm f b = 160,67 MPa Sb c = Ra V / A Sb c = 0 MPa (0.8 f b ) (18,53 MPa) max(sb z ; Sb x ) / (90% Leb) + Sb c / (0.8 f b ) 1 Stability of web plate [CODAP C9.3..7] [AD S3/ 6.1.1] h b = 381 mm l b = 66,9 mm e ba = 10 mm E b = MPa f b = 90% Leb = 16,9 MPa b = f b 10 3 / E b x = h b / l b K b = 1,613 = 0,575 Q max = l b e ba f b = ,5 dan Stresses in the bolts ( n b = ; S b = 5, mm ) Max. Tensile : bt = max{ 0 ; [ M zz / (I/v) / n b (Ra V + W S ) / n b / S b ]} = -6,8 MPa 100 MPa Max. Shear : bl = (Ra HL / n b )/ S b = 1,69 MPa 100 MPa AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

42 Maximum Allowable Working Pressure Maximum Allowable Working Pressure(Geometry). Type / Mark Diameter Thickness Max. allowable pressure Max. All. Ext. Pressure Hydrostatic pressure Operating Test Operating Test Operating Test (MPa) (MPa) (MPa) (MPa) (MPa) (MPa) 01[06] ,0 6,0,04 3,5864 / / 0,0000 0,0070 / 0[01] ,0 6,0 1,8899 3,057 / / 0,0000 0,0070 / 03[0] ,0 6,0 1,811,970 / / 0,0000 0,0070 / 04[01] ,4 6,3 3,6779 5,9406 / / 0,0000 0,0069 / 05[18] 30.03,0004 3,310 / / 0,0000 0,0000 / 07[1].01 / / / / / / / 07[1].01 / / / / / / / 09[18] ,6114 3,177 / / 0,0000 0,0000 / 10[01] ,4 7,9,0840 4,7073 / / 0,0000 0,0038 / 11[06] ,4 8,0 4, ,1358 / / 0,0000 0,0038 / Maximum Allowable Working Pressure (Nozzles). Neck Flange Hydrostatic pressure Tag Operating Test Operating Test Operating Test (MPa) (MPa) (MPa) (MPa) (MPa) (MPa) S 11, ,9478 0,8000 1,3000 0,0000 0,0000 / S1 0,560 33,11 0,8000 1,3000 0,0000 0,0070 / T 1,356,0698 0,8000 1,3000 0,0000 0,0038 / T1 1,356,0698 0,8000 1,3000 0,0000 0,0000 / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

43 Maximum Allowable Working Pressure (tubes of bundle). internal pressure External Pressure Operating Test Operating Test (MPa) (MPa) (MPa) (MPa) 16,951 34, ,5930 4,615 Maximum Allowable Working Pressure (compartment). Compartment maximum pressure Max. External Pressure Operating Test (shell) Shell (comp. 1) 0,800 MPa 1,90 MPa / Tube (comp. ) 1,00 MPa 3,160 MPa / / / / / Without any additional pressure due to hydrostatic height. AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

44 Isolated Opening(s) Isolated opening S [ in operation Int.P. ] (Shell Outlet) AD 000-Merkblätter (07-01) B9 Nozzle without pad on Shell (No. ) Set In Pressure : p = 0,8 MPa Temperature : 104,4 C Shell Material :X CrNiMo Allowable stress : K/S = 13,67 MPa Joint efficiency : v = 0,85 Corrosion + tolerance : c 1A + c A = 0 mm Tolerance for seamless pipe : / Ext. Diameter : D a = 7 mm Nominal thickness : s e = 6 mm Nozzle Neck Material : X CrNiMo Allowable stress : K 1 /S = 13,67 MPa Corrosion : c 1S + c S = 0 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : d a = 60,3 mm Nominal thickness : s S =,77 mm DN 50 External Projection : 00 mm Internal Projection : 0 mm Schedule : 10 Inclination : 0 Eccentricity : 0 mm Flange Material : X CrNiMo Type : WN Rating : (DIN 401) 10 Height : 45 mm Pad Material : / Allowable stress : K /S = / Height : / Width : / Ext. Diameter : / Required thickness of the nozzle neck under internal pressure : s = d a p / ( K 1 /S v + p) = 0,18 mm s A = s e + h = 6 mm h = / D i = D a - (s e - c 1A - c A ) = 710 mm ( s S c 1S c S ) / ( s A c 1A c A ) b s = b max ( Di sa c1a ca )( sa c1a ca ) ; 3sA = 65,54 mm d i = d a - (s S - c 1S - c S ) = 55,45 mm Longitudinal Section : Theoretical reinforcement area Angle A = AL = 90 Ψ A ls ( di ss c1s cs)( ss c1s cs) = 14,8 mm 90 l S = 0.5 l S = / Available reinforcement area b r = 65,54 mm l Sr = 14,8 mm l Sr = / Reinforcement checking A P A 0 A 1 A Ap 1 (mm ) (mm ) (mm ) (mm ) σ p Aσ0 Aσ1 Aσ Area I = 6,69 MPa K / S = 13,67 MPa Area II / / / / / Cross Section / / / / / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

45 Isolated opening S [ in test Int.P. ] (Shell Outlet) AD 000-Merkblätter (07-01) B9 Nozzle without pad on Shell (No. ) Set In Pressure : p = 1,144 MPa Temperature : 0 C Shell Material :X CrNiMo Allowable stress : K/S = 14,9 MPa Joint efficiency : v = 0,85 Corrosion + tolerance : c 1A + c A = 0 mm Tolerance for seamless pipe : / Ext. Diameter : D a = 7 mm Nominal thickness : s e = 6 mm Nozzle Neck Material : X CrNiMo Allowable stress : K 1 /S = 14,9 MPa Corrosion : c 1S + c S = 0 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : d a = 60,3 mm Nominal thickness : s S =,77 mm DN 50 External Projection : 00 mm Internal Projection : 0 mm Schedule : 10 Inclination : 0 Eccentricity : 0 mm Flange Material : X CrNiMo Type : WN Rating : (DIN 401) 10 Height : 45 mm Pad Material : / Allowable stress : K /S = / Height : / Width : / Ext. Diameter : / Required thickness of the nozzle neck under internal pressure : s = d a p / ( K 1 /S v + p) = 0,16 mm s A = s e + h = 6 mm h = / D i = D a - (s e - c 1A - c A ) = 710 mm ( s S c 1S c S ) / ( s A c 1A c A ) b s = b max ( Di sa c1a ca )( sa c1a ca ) ; 3sA = 65,54 mm d i = d a - (s S - c 1S - c S ) = 55,45 mm Longitudinal Section : Theoretical reinforcement area Angle A = AL = 90 Ψ A ls ( di ss c1s cs)( ss c1s cs) = 14,8 mm 90 l S = 0.5 l S = / Available reinforcement area b r = 65,54 mm l Sr = 14,8 mm l Sr = / Reinforcement checking A P A 0 A 1 A Ap 1 (mm ) (mm ) (mm ) (mm ) σ p Aσ0 Aσ1 Aσ Area I = 89,65 MPa K / S = 14,9 MPa Area II / / / / / Cross Section / / / / / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

46 Isolated opening S1 [ in operation Int.P. ] (Shell Outlet) AD 000-Merkblätter (07-01) B9 Nozzle without pad on Cone (No. 3) Set In Pressure : p = 0,8 MPa Temperature : 104,4 C Shell Material :X CrNiMo Allowable stress : K/S = 13,67 MPa Joint efficiency : v = 0,85 Corrosion + tolerance : c 1A + c A = 0 mm Tolerance for seamless pipe : / Ext. Diameter : D a = 461,741 mm Nominal thickness : s e = 6 mm Nozzle Neck Material : X CrNiMo Allowable stress : K 1 /S = 13,67 MPa Corrosion : c 1S + c S = 0 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : d a = 33,7 mm Nominal thickness : s S =,77 mm DN 5 External Projection : 00 mm Internal Projection : 0 mm Schedule : 10 Inclination : 0 Eccentricity : 0 mm Flange Material : X CrNiMo Type : WN Rating : (DIN 401) 10 Height : 38 mm Pad Material : / Allowable stress : K /S = / Height : / Width : / Ext. Diameter : / Required thickness of the nozzle neck under internal pressure : s = d a p / ( K 1 /S v + p) = 0,1 mm one-half apex angle : = 0,66 h = / Thickness : s A = s e + h = 6 mm D D i = e ( se c1a ca) cos di sin = 450,11 mm (Fig. ) di = d a - (s S - c 1S - c S ) = 8,85 mm cos ( s S c 1S c S ) / ( s A c 1A c A ) b s = b max ( Di sa c1a ca )( sa c1a ca ) ; 3sA = 5,31 mm Longitudinal Section : Theoretical reinforcement area Angle A = AL = 89,34 Ψ A ls ( di ss c1s cs)( ss c1s cs) = 10,87 mm 90 l S = 0.5 l S = / Available reinforcement area (Area II) Side Ψ A b r = 5,31 mm l Sr = 10,87 mm l Sr = / Available reinforcement area (Area I) b r = 5,31 mm l Sr = 10,87 mm l Sr = / Reinforcement checking A P A 0 A 1 A Ap 1 (mm ) (mm ) (mm ) (mm ) σ p Aσ0 Aσ1 Aσ Area I = 36,03 MPa K / S = 13,67 MPa Area II = 36,07 MPa K / S = 13,67 MPa Cross Section / / / / / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

47 Isolated opening S1 [ in test Int.P. ] (Shell Outlet) AD 000-Merkblätter (07-01) B9 Nozzle without pad on Cone (No. 3) Set In Pressure : p = 1,151 MPa Temperature : 0 C Shell Material :X CrNiMo Allowable stress : K/S = 14,9 MPa Joint efficiency : v = 0,85 Corrosion + tolerance : c 1A + c A = 0 mm Tolerance for seamless pipe : / Ext. Diameter : D a = 461,741 mm Nominal thickness : s e = 6 mm Nozzle Neck Material : X CrNiMo Allowable stress : K 1 /S = 14,9 MPa Corrosion : c 1S + c S = 0 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : d a = 33,7 mm Nominal thickness : s S =,77 mm DN 5 External Projection : 00 mm Internal Projection : 0 mm Schedule : 10 Inclination : 0 Eccentricity : 0 mm Flange Material : X CrNiMo Type : WN Rating : (DIN 401) 10 Height : 38 mm Pad Material : / Allowable stress : K /S = / Height : / Width : / Ext. Diameter : / Required thickness of the nozzle neck under internal pressure : s = d a p / ( K 1 /S v + p) = 0,09 mm one-half apex angle : = 0,66 h = / Thickness : s A = s e + h = 6 mm D D i = e ( se c1a ca) cos di sin = 450,11 mm (Fig. ) di = d a - (s S - c 1S - c S ) = 8,85 mm cos ( s S c 1S c S ) / ( s A c 1A c A ) b s = b max ( Di sa c1a ca )( sa c1a ca ) ; 3sA = 5,31 mm Longitudinal Section : Theoretical reinforcement area Angle A = AL = 89,34 Ψ A ls ( di ss c1s cs)( ss c1s cs) = 10,87 mm 90 l S = 0.5 l S = / Available reinforcement area (Area II) Side Ψ A b r = 5,31 mm l Sr = 10,87 mm l Sr = / Available reinforcement area (Area I) b r = 5,31 mm l Sr = 10,87 mm l Sr = / Reinforcement checking A P A 0 A 1 A Ap 1 (mm ) (mm ) (mm ) (mm ) σ p Aσ0 Aσ1 Aσ Area I = 51,83 MPa K / S = 14,9 MPa Area II = 51,89 MPa K / S = 14,9 MPa Cross Section / / / / / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

48 Isolated opening T [ in operation Int.P. ] (Channel Outlet) AD 000-Merkblätter (07-01) B9 Nozzle without pad on Shell (No. 10) Set In Pressure : p = 0,8 MPa Temperature : 104,4 C Shell Material :P65GH Allowable stress : K/S = 111,73 MPa Joint efficiency : v = 1 Corrosion + tolerance : c 1A + c A = 4,165 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : D a = 406,4 mm Nominal thickness : s e = 7,9 mm Nozzle Neck Material : P65GH Allowable stress : K 1 /S = 150,67 MPa Corrosion : c 1S + c S = 3,175 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : d a = 60,3 mm Nominal thickness : s S = 3,91 mm DN 50 External Projection : 00 mm Internal Projection : 0 mm Schedule : STD Inclination : 0 Eccentricity : 0 mm Flange Material : P65GH Type : WN Rating : (DIN 401) 10 Height : 45 mm Pad Material : / Allowable stress : K /S = / Height : / Width : / Ext. Diameter : / Required thickness of the nozzle neck under internal pressure : s = d a p / ( K 1 /S v + p) = 0,16 mm s A = s e + h = 7,9 mm h = / D i = D a - (s e - c 1A - c A ) = 398,89 mm ( s S c 1S c S ) / ( s A c 1A c A ) b s = b max ( Di sa c1a ca )( sa c1a ca ) ; 3sA = 38,88 mm d i = d a - (s S - c 1S - c S ) = 59,81 mm Longitudinal Section : Theoretical reinforcement area Angle A = AL = 90 Ψ A ls ( di ss c1s cs)( ss c1s cs) = 4,81 mm 90 l S = 0.5 l S = / Available reinforcement area b r = 38,88 mm l Sr = 4,81 mm l Sr = / Reinforcement checking A P A 0 A 1 A Ap 1 (mm ) (mm ) (mm ) (mm ) σ p Aσ0 Aσ1 Aσ Area I = 76,0 MPa K / S = 111,73 MPa Area II / / / / / Cross Section / / / / / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

49 Isolated opening T [ in test Int.P. ] (Channel Outlet) AD 000-Merkblätter (07-01) B9 Nozzle without pad on Shell (No. 10) Set In Pressure : p = 1,1478 MPa Temperature : 0 C Shell Material :P65GH Allowable stress : K/S = 5,38 MPa Joint efficiency : v = 1 Corrosion + tolerance : c 1A + c A = 4,165 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : D a = 406,4 mm Nominal thickness : s e = 7,9 mm Nozzle Neck Material : P65GH Allowable stress : K 1 /S = 5,38 MPa Corrosion : c 1S + c S = 3,175 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : d a = 60,3 mm Nominal thickness : s S = 3,91 mm DN 50 External Projection : 00 mm Internal Projection : 0 mm Schedule : STD Inclination : 0 Eccentricity : 0 mm Flange Material : P65GH Type : WN Rating : (DIN 401) 10 Height : 45 mm Pad Material : / Allowable stress : K /S = / Height : / Width : / Ext. Diameter : / Required thickness of the nozzle neck under internal pressure : s = d a p / ( K 1 /S v + p) = 0,14 mm s A = s e + h = 7,9 mm h = / D i = D a - (s e - c 1A - c A ) = 398,89 mm ( s S c 1S c S ) / ( s A c 1A c A ) b s = b max ( Di sa c1a ca )( sa c1a ca ) ; 3sA = 38,88 mm d i = d a - (s S - c 1S - c S ) = 59,81 mm Longitudinal Section : Theoretical reinforcement area Angle A = AL = 90 Ψ A ls ( di ss c1s cs)( ss c1s cs) = 4,81 mm 90 l S = 0.5 l S = / Available reinforcement area b r = 38,88 mm l Sr = 4,81 mm l Sr = / Reinforcement checking A P A 0 A 1 A Ap 1 (mm ) (mm ) (mm ) (mm ) σ p Aσ0 Aσ1 Aσ Area I = 109,08 MPa K / S = 5,38 MPa Area II / / / / / Cross Section / / / / / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

50 Isolated opening T1 [ in operation Int.P. ] (Channel inlet) AD 000-Merkblätter (07-01) B9 Nozzle without pad on Shell (No. 10) Set In Pressure : p = 0,8 MPa Temperature : 104,4 C Shell Material :P65GH Allowable stress : K/S = 111,73 MPa Joint efficiency : v = 1 Corrosion + tolerance : c 1A + c A = 4,165 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : D a = 406,4 mm Nominal thickness : s e = 7,9 mm Nozzle Neck Material : P65GH Allowable stress : K 1 /S = 150,67 MPa Corrosion : c 1S + c S = 3,175 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : d a = 60,3 mm Nominal thickness : s S = 3,91 mm DN 50 External Projection : 00 mm Internal Projection : 0 mm Schedule : STD Inclination : 0 Eccentricity : 0 mm Flange Material : P65GH Type : WN Rating : (DIN 401) 10 Height : 45 mm Pad Material : / Allowable stress : K /S = / Height : / Width : / Ext. Diameter : / Required thickness of the nozzle neck under internal pressure : s = d a p / ( K 1 /S v + p) = 0,16 mm s A = s e + h = 7,9 mm h = / D i = D a - (s e - c 1A - c A ) = 398,89 mm ( s S c 1S c S ) / ( s A c 1A c A ) b s = b max ( Di sa c1a ca )( sa c1a ca ) ; 3sA = 38,88 mm d i = d a - (s S - c 1S - c S ) = 59,81 mm Longitudinal Section : Theoretical reinforcement area Angle A = AL = 90 Ψ A ls ( di ss c1s cs)( ss c1s cs) = 4,81 mm 90 l S = 0.5 l S = / Available reinforcement area b r = 38,88 mm l Sr = 4,81 mm l Sr = / Reinforcement checking A P A 0 A 1 A Ap 1 (mm ) (mm ) (mm ) (mm ) σ p Aσ0 Aσ1 Aσ Area I = 76,0 MPa K / S = 111,73 MPa Area II / / / / / Cross Section / / / / / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

51 Isolated opening T1 [ in test Int.P. ] (Channel inlet) AD 000-Merkblätter (07-01) B9 Nozzle without pad on Shell (No. 10) Set In Pressure : p = 1,144 MPa Temperature : 0 C Shell Material :P65GH Allowable stress : K/S = 5,38 MPa Joint efficiency : v = 1 Corrosion + tolerance : c 1A + c A = 4,165 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : D a = 406,4 mm Nominal thickness : s e = 7,9 mm Nozzle Neck Material : P65GH Allowable stress : K 1 /S = 5,38 MPa Corrosion : c 1S + c S = 3,175 mm Tolerance for seamless pipe : 7/8 (1.5%) Ext. Diameter : d a = 60,3 mm Nominal thickness : s S = 3,91 mm DN 50 External Projection : 00 mm Internal Projection : 0 mm Schedule : STD Inclination : 0 Eccentricity : 0 mm Flange Material : P65GH Type : WN Rating : (DIN 401) 10 Height : 45 mm Pad Material : / Allowable stress : K /S = / Height : / Width : / Ext. Diameter : / Required thickness of the nozzle neck under internal pressure : s = d a p / ( K 1 /S v + p) = 0,14 mm s A = s e + h = 7,9 mm h = / D i = D a - (s e - c 1A - c A ) = 398,89 mm ( s S c 1S c S ) / ( s A c 1A c A ) b s = b max ( Di sa c1a ca )( sa c1a ca ) ; 3sA = 38,88 mm d i = d a - (s S - c 1S - c S ) = 59,81 mm Longitudinal Section : Theoretical reinforcement area Angle A = AL = 90 Ψ A ls ( di ss c1s cs)( ss c1s cs) = 4,81 mm 90 l S = 0.5 l S = / Available reinforcement area b r = 38,88 mm l Sr = 4,81 mm l Sr = / Reinforcement checking A P A 0 A 1 A Ap 1 (mm ) (mm ) (mm ) (mm ) σ p Aσ0 Aσ1 Aσ Area I = 108,71 MPa K / S = 5,38 MPa Area II / / / / / Cross Section / / / / / AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

52 Summary [01] [0] [06] [13] [18] [1] [4] [39] Shell Cone Korbbogen Type Head Welding Neck Flange Body Flange Tubesheet Spacing Back Flange Summary of nozzles [ Location and Dimensions ]. Location Dimensions Flange Loc. Ori. Inc. Exc. Neck Reinforcement Projectio NPS DN Rating Typ. ( ) ( ) Diam. Thk. Sch. Type (a) (b) n (DN) S 1.855,0 70,00 0,00 0,00 60,30, (50) / / / 00, [13] S ,0 90,00 0,00 0,00 33,70, (5) / / / 00, [13] T 3.445,8 90,00 0,00 0,00 60,30 3,910 STD (50) / / / 00, [13] T ,8 70,00 0,00 0,00 60,30 3,910 STD (50) / / / 00, [13] (a),(b) : Pad = thickness, Width ; Self Reinforcing = Height, over thickness ; Internal Plate = thickness, Height Tag NB : The external projection and the height of over thickness of a self is measured on axis of the nozzle. Summary of nozzles [ Type, Adjacent Openings, Goose and Material ]. Tag Set-in (+) Set-on(-) Operati ng Goose hydrostatic height Material Adjacent openings Radius Loc. Operating Test Neck Pad Flange X CrNiMo X CrNiMo S (+) CS None / / 0,00 0,0 / S1 (+) CS None / / 0,00 X CrNiMo X CrNiMo ,0 / T (+) TS None / / 0,00 390,6 P65GH / P65GH T1 (+) TA None / / 0,00 0,0 P65GH / P65GH Nozzle Type A = Process, H = manhole, E = With Blind Flange, L = Instrument, AP = Boot, XT = transition by head, CA = Shell Inlet, CS = Shell Outlet, TA = Channel Inlet, TS = Tubeside Outlet. Summary of nozzles [ Type, Weight and Local Loads ]. Tag Loc. Operating Mass Shell Nozzle Flange Longitudinal Shear Load Circumferential Shear Load Radial Load Local Loads Longitudinal Moment Circular Moment Torsional moment No. (kg) (kg) (dan) (dan) (dan) (dan m) (dan m) (dan m) S 0[01] CS 0,6, S1 03[0] CS 0,4 1, T 10[01] TS 0,9, T1 10[01] TA 0,9, Nozzle Type A = Process, H = manhole, E = With Blind Flange, L = Instrument, AP = Boot, XT = transition by head, CA = Shell Inlet, CS = Shell Outlet, TA = Channel Inlet, TS = Tubeside Outlet. Flange Weight With blind flange if present. AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

53 Summaries of bundle. Baffles and Support Plates. Transverse : No = / Thickness = / Diameter = / Holes = / Total weight = / Material = / Locations : / Support : No = / Thickness = / Diameter = / Holes = / Total weight = / Material = / Locations : / Longitudinal : No = / Thickness = / Width = / Total length = / Total weight = / Material = / (Location, length) : / Partition Plates. Front box Total weight = 10,5 kg Material = SA516GR60 Rear box Total weight = / Material = / Impingement plate, tubes by-pass and sealing strips. Plate : No = / Thickness = / length = / Material = / Total weight = / Tubes : No = / Thickness = / Diameter = / Material = / Total weight = / Sealing Strips : No = / Thickness / Width / Material = / Total weight = / Sliding Rails. Quantity = 0 Height / Diameter = / Material = / Type = / Width = / Total weight = / Tie Rods, spacers and Dummy Tubes. Bar Stays : No = / Diameter = / Total weight = / Material = / Spacer : Thk. = / Diameter = / Total weight = / Material = / Dummy Tubes No = / Diameter = / Total weight = / Material = / Miscellaneous. / No = / Thickness = / Total weight = / Material = / Summary of bends. Row Number Circumferential Weight Thickness Bending radius Straight Length of bends Length 1 9 6, kg,11 mm 38,10 mm.500,00 mm 5.119,69 mm 8 6,3 kg,11 mm 65,60 mm.500,00 mm 5.06,08 mm 3 7 6,4 kg,11 mm 93,09 mm.500,00 mm 5.9,46 mm 4 4 6,6 kg,11 mm 10,59 mm.500,00 mm 5.378,84 mm Total number of bends = 8 Length ( thk =,11 mm ) = 146,3 m Total weight = 178,3 kg AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

54 Summary of Forged Items and Relevant Accessories. Flange dimensions Tag Type (1) C C T () External Diameter Internal Diameter Bolt Circle Flange thickness Hub length Cylindrical extension length Hub thickness shellside Hub thickness flangeside Nubbins width Stub Thickness , , , , , (1) Flange Type : P = slip-on (loose), C = integral with hub, T = lap-type joint (loose), R = slip-on (integral), G = Integral with hub, swing bolts O = optional (corner joint), F = compression flange, S = backing flange.. () Flange face : 0= flat face unconfined, 1= male-female semi-confined, = tongue and groove, 3= tongue and groove + nubbins. Bolting Tag (3) no. [n B] Designation Friction Friction Thread Bolt Load Bolt torque Diameter Bolts length coefficient coefficient pitch [F BO nom / n B] [M t,nom] in nut in thread [ p t] (N) (N mm) [ n] [ t] 5.01 / M (4) 1.65,15 0,1 0,1 (3) Bolt Type : 1,,4,6 : ISO (1 et 4 : Pitch 3 mm for Ø > M4) (1 et 6 : Tensile Stress Area ;,4 : Root Area) 3 : UNC, Root Area 5 : ISO, Reduced Area (DIN 510) (4) Bolt torque according to EN Appendix D : M t,nom = k B F BO nom / n B k B = p t /() + t d t /(cos) + n d n / (5) Bolt torque according to EN Appendix G.8.4 : (6) Bolt torque according to GOST R Appendix J : Gaskets d t = pitch diameter of the thread d n = mean diameter in the nut (friction) = half angle of thread Partition rib Ring Diameter Width Thickness Tag width Outer Width Internal Width Thickness 5.01 / , ,5 / Tubesheets No. 1 (a) Side Shellside Machining Shell support Stress Relief But joint Partition Tube External Flange Face Thickness extension or radius Slope extension groove depth Extension Diameter Tube Shellside 5 Tube 5 (a) Floating Tubesheet for a floating head exchanger , Standard Flanges. Type / Mark Norm Diameter Nominal Rating Material Group [13] S DIN 401 DN X CrNiMo [13] S1 DIN 401 DN 5 10 X CrNiMo [13] T DIN 401 DN P65GH [13] T1 DIN 401 DN P65GH Temperature ( C) Pressure (MPa) Max. allowable pressure (MPa) 104,4 C 0,8 0,8 test 1,144 1,3 104,4 C 0,8 0,8 test 1,151 1,3 104,4 C 0,8 0,8 test 1,148 1,3 104,4 C 0,8 0,8 test 1,144 1,3 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

55 Summary of Geometry. Type Tag Diameter Height / Length Thickness Angle Mass Flanges Internal base rating ( ) (kg) Specifi c Gravity Material 01[06] ,0 36, 50,0 6, ,4 8,00 X CrNiMo [01] ,0.550,0.600,0 6, ,3 8,00 X CrNiMo [0] ,0 547, ,8 6, ,00 X CrNiMo [01] NPS 16 33, ,8 6,350 0,1 8,00 X CrNiMo [18] ,7 67,0 3.47,8 0, , 8,00 X CrNiMo [4] space -,0 3.45,8 07[1] ,9 33,0 3.78,8 0, ,00 X CrNiMo [4] space -,0 3.76,8 09[18] ,6 67, ,8 0, ,8 7,85 P65GH 10[01] 5.06 NPS 16 04, ,8 7, ,9 7,85 P65GH 11[06] ,4 156, ,8 8, ,85 P65GH Angle : half angle at apex for a concentric cone ; maximum angle between cone an cylinder for an eccentric cone. Material : (N) = normalized NB : Italic line indicates an element without pressure.. AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

56 Summary of Weights, Capacities and Painting Areas. Designation Mass (kg) Lifted Erected Operating Test Shutdown Shells 93 X X X X X Cones 48 X X X X X Heads 48 X X X X X Shell flanges 53 X X X X X Skirts Support saddles 78 X X X X X Anchor boxes Fireproofing Man holes Nozzles 1 X X X X X Piping Support Ring Trays Liquid on trays Packing Helicoidal plates Inner lining Insulation supports Insulation (Vessel) Insulation (Piping) Coil Liquid in Coils Stiffening rings Piping Clips Structural Clips Ladders Platforms Tubesheets 37 X X X X X Tubes and Tie Rods 178 X X X X X Baffles and Support Baffles 11 X X X X X Floating head flange Backing device Operating Internals Test Lifting Erection Operating External loads Test Lifting Erection Compartment Shell (comp. 1) Tube (comp. ) / Capacity (m 3 ) 1,150 0,098 / Operating 0 0 / Liquid Mass (kg) Test / Total Test / / / Mass (kg) Area (m ) NB : New weight. Vessel Operating 758 Lifted 758 Erected 758 Shutdown 758 Vessel Tag 8,3 Support 1,6 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

57 Summary of saddles. H EYV M K T FB EXA < 0 a F EXF EXF EXA > 0 F a EXA = 0 F a Standard : APVessel Number of saddles = Fixed saddle No. = Saddle No 1 (left) Location = mm Stiffness = / H = 561 mm Welded Diameter =7 mm T = 10 Mass = 39 kg Bolts : Diameter = 0 mm ( Hole Diameter = 3 mm ) Base Plate Ribs Wear Plate Web E B L C G EXV EYV K / Saddle No (right) Location =.600 mm Stiffness = / H = 561,93 mm Welded Diameter =73,86 mm T = 10 Mass = 39 kg Bolts : Diameter = 0 mm ( Hole Diameter = 3 mm ) Base Plate Ribs Wear Plate Web E B EYV EXV L C G EXV EYV K / Summary of Foundation Loads D B C DB L EXF EXA G Ra V : Vertical reaction in dan seismic load Ra HT : Horizontal reaction (cross) in dan () vertical downside and horizontal longitudinal to the right Ra HL : Horizontal reaction (longitudinal) in dan () vertical downside and horizontal longitudinal to the left Am T : Circumferential bending moment in dan m () vertical upside and horizontal longitudinal to the right Am L : Longitudinal bending moment in dan m () vertical upside and horizontal longitudinal to the left () vertical downside and horizontal cross Stacked vessels : loads for the whole. () vertical upside and horizontal cross Support No E D D M M F F E FB FB EXF EXA G EXF EXF EXA EXA E G a a (Corroded Weight) (New Weight) Operation Int.P. Wind Normal Lifting Ra V Ra HT 0 0 Ra HL Am T 0 0 Am L 0 0 Ra V Ra HT 0 0 Ra HL 0 0 Am T 0 0 Am L 0 0 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

58 (New Weight) (Corroded Weight) Erected During test Ra V Ra HT 0 0 Ra HL 0 0 Am T 0 0 Am L 0 0 Ra V Ra HT 0 0 Ra HL 0 0 Am T 0 0 Am L 0 0 (Corroded Weight) Shutdown Wind Normal Ra V Ra HT 0 0 Ra HL Am T 0 0 Am L 0 0 (Corroded Weight) During test P = 0. Ra V Ra HT 0 0 Ra HL 0 0 Am T 0 0 Am L 0 0 AutoPIPE Vessel (Microprotol) procal V prodia V Bentley Systems, Inc.

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