sc celec bo 001 calculations caldera
DESCRIPTION
diseño de calderaTRANSCRIPT
psig at °F
Firetube Boiler 100 BHP
CUSTOMERSERVICIOS INDUSTRIALES Y CALDERAS
LOCATIONQuevedo - Ecuador
BOILER DESCRIPTION
PROJECT NUMBER: P2013-013-03
DESCRIPTIONMAWP: 165 373HEATING SURFACE: 704 sq-ftSTEAM CAPACITY: 5635 lb/hrYEAR BUILT: 2013RADIOGRAPHY: YESPOST-WELD HEAT TREATMENT: NONE
SIGNATURES
REV. DESIGNED BY REVIEWED BY ACCEPTED BY
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 1
Chapter Description
COVER SHEET
DESIGN CALCULATION INDEX
DESIGN REQUIREMENTS
BOILER SKETCH AND DIMENSIONS
MATERIAL SUMMARY
FITTING RATING SUMMARY
CYLINDRICAL SHELL UNDER INTERNAL PRESSURE
FURNACE DESIGN
FIRE TUBE DESIGN
TUBESHEET DESIGN
TUBE SHEET DIAGONAL AND STRAIGHT STAYS DESIGN
OPENINGS
HEATING SURFACE CALCULATION
STEAM CAPACITY CALCULATION
WEIGHT SUMMARY
16 LIFTING LUGS & SADDLES DESIGN / SELECTION
17 HYDROSTATIC TEST SUMMARY
18 WELDING JOINTS DESIGN
R REVISIONS RV
02 02
09 11
03 03
04 05
02 DESIGN CALCULATION INDEX
Sheet Nº.
01 01
05 06
06 07
07 08
08 09
10 12
11 13
12
15
13
14
20
18
18
24
14
19
23
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 2
03.01 General Information:
03.02 Owner:
03.03 Operator:
03.04 Country of Installation:
03.05 State/Province of Installation:
03.06 City of Installation:
03.07 Service:
03.08 Liquid Level:
03.09 Specific Gravity:
03.10 Item No.:
03.11 Diameter (in.):
03.12 Length, Tangent-to-Tangent (in):
03.13 Type of boiler: Vertical Horizontal Sphere
03.14 ASME Stamping Yes No
03.15 National Board Registration Required: Yes No
03.16 Special Service:
Not Applied Lethal (L) Direct Firing (DF) Unfired Steam Boiler (UB)
03.17 Overpressure Protection:
Rupture Disk Valve System Design Other Pressure switch
03.18 Operating Conditions:
03.19 Minimum Pressure Maximum Pressure psi
03.20 Minimum Temperature Maximum Temperature °F
03.20.01 Steam Capacity
03.21 Pressure and Temperature (Shell):
03.22 Internal Design Pressure: at °F
03.23 MAWP Internal: Same as Design Pressure
03.24 Minimum Design Metal Temperature (MDMT) ºF @ psi
03.25 Due to: Process Ambient Temperature Other
03.26 Pressure and Temperature (Furnace):
03.27 External Design Pressure: at °F
03.28 MAWP External: Same as Design Pressure
03.29 Minimum Design Metal Temperature (MDMT) ºF @ psi
03.30 Due to: Process Ambient Temperature Other
x
03 User's Design Requirements (Part 01)
Servicios Industriales & Calderas
Corporación Eléctrica del Ecuador (CELEC)
Ecuador
Los Rios
Quevedo
Steam generation
80%
1
P2013-013-01
60.79 (External)
(Shell)
x
x
x
150
194 ºF 365
x
100 psi
165
68
x
700
373
165
x
165 psi
x
5635 Lb/h
x
165 psi
68
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 3
03.31 Cyclic Service: Yes No
03.32 Design Life years
03.33 Fatigue Analysis? Yes No
03.34 Wind Loadings: Yes No
03.35 UBC IBC ASCE 7 None Other
03.36 Wind Speed: Exposure Category Elevation
03.37 Classification Category Topographic Factor
03.38 Seismic Loadings: Yes No
03.39 UBC IBC ASCE 7 None Other
03.40 PWHT Process Required Per Code
03.41 Other Loadings per PG-22
Temp. Gradients Deflagration Diff. Thermal Exp. None
03.42 Insulated: Yes No
03.43 By Manufacturer By Others
03.44 Type:
03.45 External Thickness Conductividad
03.46 Internal Thickness Density
03.47 Coating Specification:
03.48 Permitted Prior to Pressure Test Yes No
03.49 Vessel Support: Legs Skirt Lugs Saddles
03.50 Fireproofing: Yes No
03.51 Type: Rating (hr):
03.52 Corrosion Allowance:
03.53 Shell:
03.54 Heads/Tube Sheet:
03.55 Nozzles:
03.56 Supports:
03 User's Design Requirements (Part 02)
- - -
Cycles per - --
Int.: 0 in
-
x
x
x
x
x -
- -
- -
-
x
x -
-
-
x
x
x
x
x
- -
Int.: 0 in Ext.: 0 in
-
Int.: 0 in
-
x
-
Ext.: 0 in
Int.: 0 in
x
2 inch 0.033 W/(°C-m2)
in
Ext.: 0 in
Ext.: 0
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 4
04 BOILER SKETCH AND DIMENSIONS
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 5
- 16600 36000 1 1 Plate
16 Rear Cover SA-36 - 16600 36000 1 1 Plate
05.37
05.29
05.30
05.31
05.32
05.33
05.34
05.35
05.36
Item Spec. No.Type /
GradeP No.
Group
No.
05 MATERIAL SUMMARY
08.1 Diagonal Stays 1 SA-516
1 1 Pipe
1 2 Plate
04
02
03
Product FormYield Point
Stress (psi)
SA-51601
05
08.2 Diagonal Stays 2 SA-516 Gr-70 38000
09
35000
Gr-70 38000
Stack SA-516 Gr-70 38000
17100
20000
Firetubes SA-192 - 26000 1 1 Tube13400
Plate
Furnace SA-516 Gr-70 38000 1 2 Plate
2
2 Plate
2 Plate
Maximum
Allowable
Stress (psi)
20000
20000
Gr-70
20000
Component
Boiler Shell 38000 1
Gr-70 38000 1
Rear Tubesheet SA-516 Gr-70 38000 1
20000
1 2 Plate
05.01
05.02
05.03
05.04
05.05
05.06
05.07
05.08
05.09
05.10
20000
20000
1 2 Plate
Front Tubesheet SA-516
07 Handhole (3x4x1/2x2) SA-106 Gr-B
05.19
05.20
Flange 4" SA-105 150# 36000
13 Legs SA-36 - 36000
Front Cover SA-36 -
17 16600
17100
16600
SA-106 Gr-B 35000
15 Steam Difusor SA-36
10 Pipe NPS-4, Sch. 40 SA-106 Gr-B 35000 1 1 Pipe17100
Plate
1 2 Fitting
12 Lugs SA-516 Gr-70 38000 1 2 Plate
19600
20000
11
14 Water Difusor SA-36 - 16600 36000 1 1 Plate
1
36000 1 1
1
1 1 Plate
06 Manhole (12x16x1x4) SA-675 Gr-70 35000 1 2 Bar
16600
19900
Beam Support SA-36
19
-
18 Pipe NPS-2, Sch. 40
05.11
05.12
05.13
05.14
05.15
05.16
05.17
05.18
05.21 20 BarHinges - - - --
1 Pipe
36000 1 1 Plate
05.24
05.25
05.26
05.27
05.28
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 6
06.20
06.19
06.18
06.17
06 FITTING RATING SUMMARY
NOZZLE ID SERVICE QTY MATERIALSCHEDULE /
CLASS
NOMINAL
DIAMETER
WALL
THICKNESS
FIGURE
PW-16.1
APPLICABLE
NPS-1 (NPT) 0.38 Skecth c
06.02 02 Control Level 1 SA-105 3000# NPS-1 (NPT)
06.01 01 Control Level 1 SA-105 3000#
0.38 Skecth c
06.03 03 Control Level 1 SA-105 3000# NPS-1 (NPT) 0.38 Skecth c
06.04 04 Warrick Control 1 SA-105 3000# NPS-2 (NPT) 0.5 Skecth c
NPS-1 (NPT) 0.38 Skecth c
06.06 06 Steam Outlet 1 SA-106 Gr-B Sch. 40 NPS-4
06.05 05 Surface purge 1 SA-105 3000#
0.237 Skecth c
06.07 07 Inlet Water 1 SA-105 3000# NPS-1 1/2 (NPT) 0.44 Skecth c
06.08 08 Inlet Water 1 SA-105 3000# NPS-1 1/2 (NPT) 0.44 Skecth c
NPS-1 1/2(NPT) 0.44 Skecth c
06.10 10 Safety Valve 1 SA-105 3000# NPS-1 1/2(NPT)
06.09 09 Safety Valve 2 SA-105 3000#
0.44 Skecth c
06.11 11 Drain 1 SA-105 3000# NPS-1 1/2 (NPT) 0.44 Skecth c
06.12 12 Drain 1 SA-105 3000# NPS-1 1/2 (NPT) 0.44 Skecth c
NPS-1 1/2 (NPT) 0.44 Skecth c
06.14 14 Manhole (12x16x1x4) 1 SA-675 Gr. 70 - -
06.13 13 Drain 1 SA-105 3000#
1 Skecth c
06.15 15 Handhole (3x4x1/2x2) 6 SA-106 Gr-B - - 0.5 Skecth c
06.16
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 7
Input:
07.01 Per PG-6
07.02 Maximum Allowable Working Pressure (PG-21) (See 03.22)
07.03 Working temperature
07.04 Maximum Allowable Stress Value at the Design Temperature of the Metal (PG-27.4.2)
07.05 Efficiency (see PG-27.4.1)
07.06 Inside Radius of Cylinder
07.07 Minimum Allowance for Threading and Structural Stability PG-27.4.3
07.08 Temperature Coefficient
07.09 Minimum Required Thickness (PG-27.2.2)
07.10 Thickness Chosen
#
07.11 Extreme fiber elongation (PG-20)
07.12 t =
07.13 Rf =
07.14 Ro = Write inf if cilinder is forming from a flat plate otherwise write Ro value.
07.15 % extreme fiber elongation = % 0.52
0.315 in
inf
30.18 in
in
t: 0.249 in
tch: 0.315 in
C: 0.000 in
y: 0.4 -
07 CYLINDRICAL SHELL UNDER INTERNAL PRESSUREASME Code Section I, Edition 2010, Addenda 2011
MATERIAL SA-516 Gr-70
psi
T: 373 ºF
R: 30.02 in
S: 20000 psi
E: 1.0 -
P: 165
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 8
Furnace Design (PFT-51)
When Do / t >= 10
08.01 08.01.01 Sy= psi
08.02 External Design Pressure (See 03.22)
08.03 Design Temperature (See PFT-50.1)
08.04 Modulus of Elasticity of Material at Design Temperature (Section II, Part D)
08.05 Total Length
08.06 Number of Stiffening Rings
08.07 Length between Stiffening Ring
08.08 Outside Diameter of Cylindrical Furnace
08.09 Selected Thickness for calculation Cylindrical Furnace
08.10 Ratio L/Do
08.11 Ratio Do/L#
08.12 Factor Determined from Fig. G (See Section II, Part D)
08.13 Allowable External Working Pressure for the Assumed Value of t (See PFT-51.1.2)
08.14 Factor Determined from the Applicable Material Chart in Section II, Part D, Fig. CS-2
08.15 Allowable External Working Pressure for the Assumed Value of t (See PFT-51.1.2)
08.16 Is A fall to the left of the applicable material/temperature line (Fig.CS-2, ASME Section II, Part D) if yes use Pa_A if No us Pa_B
08.17 Calculated Value of Allowable External Working Pressure
B: 7300 -
Pa_B 196 psi
Condition 1 No
Pa: 196 psi
A: 0.00072 -
Pa_A: 237 psi
L/Do: 4.52 -
Do/t: 49.61 -
Do: 24.80 in
t: 0.500 in
n: 0 in
L: 112.20 in
24500000 psiE:
Lt: 112.20 in
P:
T:
MATERIAL:
08 FURNACE DESIGNASME Code Section I, Edition 2010, Addenda 2011
SA-516
165 psi
700.0 ºF
Gr-70 38000
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 9
08 FURNACE DESIGNASME Code Section I, Edition 2010, Addenda 2011
08.18 Extreme fiber elongation (PG-20)
08.19 t =
08.20 Rf =
08.21 Ro = Write inf if cilinder is forming from a flat plate otherwise write Ro value.
08.22 % extreme fiber elongation = %
inf in
1.98
in
in
1/2
12.65
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 10
Input:
09.01 Per PG-13 09.01.01 Sy= psi
09.02 External Design Pressure
09.03 Design Temperature
09.04 Modulus of Elasticity of Material at Design Temperature (Section II, Part D)
09.05 Total Length (inside and between the tube sheets)
09.06 Outside Diameter of Tube
09.07 Minimum Required Thickness of Fire Tube
09.08 Ratio L/Do
09.09 Ratio Do/L
09.10 Factor Determined from Fig. G (See Section II, Part D)
09.11 Allowable External Working Pressure for the Assumed Value of t (See PFT-51.1.2)#
09.12 Factor Determined from the Applicable Material Chart in Section II, Part D
09.13 Allowable External Working Pressure for the Assumed Value of t (See PFT-51.1.2)
09.14 Is A fall to the left of the applicable material/temperature line (Fig.CS-1, ASME Section II, Part D) if yes use Pa_A if No us Pa_B
09.15 Calculated Value of Allowable External Working Pressure
09.16 No need calculation of the required cross-sectional for stay tubes per PFT-31.3
Conclusion:
09.17 Chosen pipe corresponds to a Pipe SA-192, Outer Diameter 2 1/2 in and thickness wall of 0,114 in
T: 700.0
NoCondition 1
Do/t: 21.93 -
A: 0.00290 -
112.20 in
t: 0.114 in
L/Do:
Do: 2.5 in
44.88 -
L:
09 FIRE TUBE DESIGNASME Code Section I, Edition 2010, Addenda 2011
SA-192 -
P: 165 psi
MATERIAL 26000
°F
E: 24500000 psi
Pa: 608 psi
Pa_A: 2160 psi
B: 10000 -
Pa_B 608 psi
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 11
10.01
10.02 Assumed Thickness
10.03 Maximum allowable stress for the tubesheet Table 1A of Section II, Part D
10.04 Design pressure
10.05 Tubesheets Constant (See PFT-31.2)
10.06 Longitudinal pitch
10.07 Diagonal pitch
10.08 Outside diameter of the tube
10.09 Required thickness of tubesheet due to Fire Tubes (PFT-31)
10.10
10.11Maximum allowable stress value for the tubesheet Table 1A of Section II, Part D
10.12Design pressure
10.13Tubesheets Constant
10.14Stay Diameter to be welded
15.15 Cross section for direct staybolt
10.16Maximum allowable stress value for stay @
10.17 Per PG-46.5 and PFT-27.4
10.18Staybolts pitch (see PG-49.1) (Deducted formula)
10.19 Minimum thickness of plate (See PG-46)
10.20 Chosen Pitch
10.21
10.22
10.23 Minimum thickness required tmax = MAX(t10.09;t10.22)
10.24 Thickness chosen
Pitch calculated according to
the chosen diam Stay
New minimum thickness of plate for chosen pitch in 10.
SA-36
t: 0.522
373 °F
in
d: 1.000 in
a: 0.785 in
S: 16600 psi
p:
t_ch: 0.500 in
p: 7.874 in
t: 0.482
t: 0.482 in
in
C:
8.522 in
pmax: 15.000 in
P: 165 psi
C: 2.2 -
TUBESHEET THICKNESS DUE TO STAYS
Material: SA-516 Gr-70
S: 20000 psi
d: 2.500 in
t: 0.151 in
pt: 3.310 in
pt': 3.310 in
P: 165 psi
C: 2.2 -
t_ass: 1/2 in
S: 20000 psi
10 TUBESHEET DESIGNASME Code Section I, Edition 2010, Addenda 2011
TUBESHEET THICKNESS DUE TO FIRE TUBES (PFT-31)
Material: SA-516 Gr-70
2.200 - Per PFT-27.3
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 12
11.01 SA-516 Gr 70 Per PG-13
11.02 Design pressure
11.03 Maximum allowable stress for stays
11.04 Maximum allowable stress for tubesheet
11.05 p: in Chosen Pitch (See 10.20)
11.06.01 Cross-section for direct stay (per PG-49 and PFT-26) a s =(1.1*P*p2) / (S S +1.1*P) (Deducted formula)
11.06.02 Direct Stay diameter
11.07 "L" and "l" ratio (per drawing: DWG-001) (Ratio per PFT-32.1)
11.08 Diagonal Stay diameter (Here considered PFT-32.1 or PFT-32.2)
11.09 Selected Stay diameter has to be greater then dds (see 11.08)
11.11 Cross section for diagonal stays selected (11.09)
11.12 Total area to be stayed (per drawing DWG-004)
11.13 Maximun load to be supported per one Staybolt. (See 11.08) (Here considered PFT-32.1 or PFT-32.2)
11.14 Total load to be suppprted by all staies Ft = P x At
11.15 Minimum stays n = Ft/Fs
11.16 Used stays
11.17 Net area to be stayed (Calculated)
11.17 Allowable Pressure
11.18 tthroat= Min per PW-19.4.1
11.19 L>= Min welded length per PW-19.4.1
11.20 L/2: Min choosen welded length per side of the stay
2.063 in
1.500 in
0.375 in
n_ch: 7 units
Paw: 174 psi
An: 499 sq-in
Ft: 83054 lb
n: 7 units
At: 503.36 sq-in
Fs: 12381 lb
d: 0.888 in
a: 0.6190 sq-in
dds: 0.888 in
L/l: 1.150 in
as 0.558 sq-in
7.874
ds: 0.84 in
11 DIAGONAL STAYS DESIGNASME Code Section I, Edition 2010, Addenda 2011
Material:
P: 165 psi
Ss: 20000 psi
St: 20000 psi
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 13
Vessel Data
15.01 Per PG-6
15.02 Maximum Allowable Working Pressure (PG-21)
15.03 Inside Radius of Cylinder (See 07.06)
15.04 Maximum Allowable Stress for Vessel (See 07.04)
15.05 Required Thickness of the Vessel (See 07.09)
15.06 Wall Thickness of the Vessel (See 7.10)
15.06.1 PG-32.1.1 K = P*D/(1.82*S*t)
15.06.2 PG-32.1.2 dmax = 2.75*[D*t*(1-K)]^(1/3)
Openings Data
15.06.3
15.07
15.08 Allowable Stress in Nozzle
15.09 Inside Radius of the Nozzle
15.10 Efficiency (See PG-27.4.1)
15.11 Temperature Coefficient (See PG-27.4.6)
15.12 Diameter of a Finished Opening
15.12.1 PG.32.1.4 (a)
15.12.2 PG.32.1.4 (b) PG-32.1.2 (see 15.06.2) (See example A-68 ASME Div. I)
15.12.3 dmax. Selected Max (15.42.2 & 15.42.3)
15.12.4 Per PG-32.1.4 (b) (See example A-68 ASME Div. I).
15.13
15.14 Nominal Thickness of Nozzle Wall
15.14.1 Per PG.32.1.3 Minimum distance center-to-center to be single opening
15.15 Limits of Compesation
15.16 Per PW-16.2
15.16.1 thickness of attached reinforcing
15.17 Per PW-16.2 (Throat)
15.17.1
15.17.2 Distance from the outside of the vessel to the projection of the nozzle inside the vessel
15.18
15.18.1
15.19 Factor from PG33 and Fig PG-33.3
15.20 Strength Reduction Factor
15.21
15.22
15.23
15.24
15.25
15.26
15.27 A 2-2 = 2*(t n -t rn )*(2 1/2*t n +t e )*f r1
15.28
15.28.1 A 3 = 2*t n *f r1 *h
15.29
15.29.1 A 4-3 = WL 32
*f r1
15.30
15.31
15.32 If 15.31 is "Yes" not need reinforcing element per Fig. PG-33.1
15.33 Note 1: Per PG32.1.4 , the component NPT-1 1/4, NPT-2 and NPT-3 no need to do calculations (See example A-68 ASME Div. I)
15.34 Note 2: Openings are sepated more than Ls=2*LC, so shall be considetared as Single Openings per PG-32.1.3
0.042
0.315
A1-2: 0.042
A: 0.436
A1:
tn: 0.380
3.694 3.694dmax.(b):
0.00618
0.380
A1-1:
te: 0.000 0.000
Area Available in Nozzle
Projecting Intward
0.000
3.694
0.354
1
Area Available in Nozzle
Projecting Outward
Area Available in Shell0.042
0.774 sq-in
0.774
0.263 in
0.315 sq-in
Required Thickness of Seamless Nozzle Wall
in
Area Available in outward Nozzle
Weld
Area Available in inward Nozzle
Weld
Area Required (fig. PG-33.1)
Strength Reduction Factor
in
in
sq-in
in
0.315
0.066 sq-in
in
sq-in
0.747
-
1.000
0.000 in
-
0.250 in
0.015
0.042
0.250
2.375
3.694
No need
calculation
tc DWG: 0.263 0.263 0.263
WL3: 0.000
1
h: 0.315
WL1: 0.354
0.315
0.000
0.250
fr1:
LC: 1.190
F:
A4-1: 0.125 0.125 0.125 sq-in
sq-in
A2:
0.048
in
A2-1: 0.592
A3: 0.239 0.277
1.000
0.592 0.682
0.000
1.000 1.000 1.000 -
CONDITION Yes Yes Yes -
SumA 0.998 1.133 1.280 sq-in1.001
A4-3: 0.000 0.000 0.000 sq-in
1.000 1.000
0.049 0.066 sq-in
0.560
sq-in
A2-2: 0.714 0.953 1.229
fr2:
1
0.354
2.980
trn: 0.00410 0.00672 0.00829
1.490
Ls: 2.380 3.240 4.000
1.620 2.000
tmin: 0.315 0.315 0.315
tc:
0.315
0.250
N07, N08, N09,
N10, N11, N12,
N13
1 1
y: 0.4 0.4
SA-105N
N01, N02,N03
NPT-1 1/4
20000
0.745
1
0.4
Rv: 30.02 in
Sv: 20000 psi
12 OPENINGSASME Code Section I, Edition 2010, Addenda 2011
MATERIAL SA-516 Gr-70
P: 165 psi
tr: 0.249 in
K: 0.873 -
dmax.: 3.694 in
t: 0.315 in
3.694 in
CONDITIONNo need
calculation
No need
calculation
No need
calculation
NPT-1 NPT-1 1/2 NPT-2 UNIT
dmax.: 3.694 3.694
N04
dmax.(a): 2.375 2.375 2.375
MATERIAL SA-105N SA-105N SA-105N
Sn 20000 20000 20000
Rn 0.495 0.810 1.000
Quantity 4 3 7 1
1.490
N01, N02,N03,
N05
Each
in
-
psi
in
E
-
3.694
0.440 0.500 in
d: 0.990 1.620 2.000 in
1 -
0.4
in
in
0.000
0.125
0.239
0.589
0.710
0.589
Yes
1
0.354
0.000
0.622
0.049
0.048
0.042
0.682
1.000
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 14
| 15.35 Manhole Size:
Vessel Inputs Nozzle Inputs
15.42.6
15.36 15.43
15.37 Maximum allowable working pressure 15.44 Allowable stress in nozzle
15.38 Allowable stress in vessel 15.45 Inside radius of the nozzle under consideration
15.39 Inside radius of cylinder 15.46 Inside diameter of the nozzle under consideration
15.40 15.47 do: Outside diameter
15.41 Required Thickness of the Vessel (See 07.09) 15.48 d or Rn + tn + t, use larger value PG-36.2.1 & 2
15.42 Thickness of the vessel wall 15.49
15.42.1 PG-32.1.1 K = P*D/(1.82*S*t) 15.50
15.42.2 dmax: PG.32.1.4 (a) dmax = 2.75*[D*t*(1-K)]^(1/3) 15.51 tn: Nominal thickness of nozzle wall
15.42.3 PG.32.1.4 (b) 15.52
15.42.4 Max (15.42.2 & 15.42.3) 15.52.1
15.42.5 15.52.2
Reinforcing Element
15.53 15.55 Allowable stress in reinforcing element
15.54 (see Fig. PG-33.2) 15.56 Out side diameter of reinforcing element
Area of Reinforcement Available (PG-33.3, Fig. PG-33.1)
Relations Inputs
15.57 Factor from PG-33 and Fig. PG-33.3
15.58 Sn /Sv 15.59 Sn /Sv or Sp/Sv 15.60 Sp/Sv
15.61 15.62 15.63
15.61.1 0.7xt min 15.61.2
Area of Reinforcement Required Area available in nozzle
15.64 A=(d+2tn)trF 15.68 A2a=2(tn – trn)(21/2tfr1)
Area available in shell 15.69 A2b=2(tn – trn)(21/2tn + te)fr1
15.65 A1a=(d-2tn)(t-Ftr) 15.70 Use smaller value
15.66 A1b=2t(t-Ftr) 15.71
15.67 Use larger value 15.72 Area available in welds
15.73 A41 A41=(WL1^2)fr2
15.74 A43 A43=(WL3^2)fr1
Results
15.75 A1+A2+A3+A41+A43
15.76 CONCLUSION 1 A1+A2+A3+A41+A43>=A, This is greater than the required area, so a reinforcing element is not necessary.
With reinforcing element added:
Area available in outer element weld Area available in element
15.77 A42=(WL2^2)fr3 15.78 A5=(Dp – d – 2tn)tefr3
15.79 CONCLUSION 2 Reinforcing element is not necesary.
12 OPENINGS (MANHOLE N14)ASME Code Section I, Edition 2010, Addenda 2011
For nozzle wall inserted through the vessel wall (PG-33.3, Fig. PG-33.1)
Material: SA-516 Gr-70 y: 0.4 Material: SA-675
12x16x1x4
Sv: 20000 psi Rn 6.000 in
Gr-70 y:
P: 165 psi
C: 0.000 in 14.000 in
Rv 30.02 in d: 12.000 in
t: 0.315 in C: 0.000 in
tr: 0.249 in Limit: 12.000 in
3.694 in 1 in
K: 0.873 - trn: 0.000 in
3.694 in h: 1 in Choosen
2.375 in h: 0.787 inPG-36.3 Maximum distance nozzle project
inwards from the outer surface of the vessel
wall
Condition: Need calculation
Material: SA-516 Gr-70 Sp: 20000 in
Ls: 24.000 inPG-32.1.3 Limit minimum distance to be single
opening.
F 1
fr1 1.00 fr2 1.00
te: 0 in
A 3.485 sq in A2a 1.567 sq in
fr3 1.00
WL1 0.354 in WL2 0.000 in WL3 0.354
tc min 0.250 in in
A1b 0.0416 sq in A3 1.567 sq in
A2b 4.975 sq in
A1a 0.6607 sq in A2 1.567 sq in
A42 0.000 sq in A5 0.000 sq in
A1 0.6607 sq in
0.124 sq in
0.124 sq in
Qty: 1 Each
4.04 sq in
in
Dp 0 in
Required thickness of a seamless nozzle. trn=0
per PG-33.3 for manhole and nozzle.
0.4
Sn 19900 psi
tc DWG 0.263
SERVICIOS INDUSTRIALES Y CALDERAS
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CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 15
| 15.80 Manhole Size:
Vessel Inputs Nozzle Inputs
15.87.6
15.81 15.88
15.82 Maximum allowable working pressure 15.89 Allowable stress in nozzle
15.83 Allowable stress in vessel 15.90 Inside radius of the nozzle under consideration
15.84 Inside radius of cylinder 15.91 Inside diameter of the nozzle under consideration
15.85 15.92 do: Outside diameter
15.86 Required Thickness of the Vessel (See 07.09) 15.93 d or Rn + tn + t, use larger value PG-36.2.1 & 2
15.87 Thickness of the vessel wall 15.94
15.87.1 PG-32.1.1 K = P*D/(1.82*S*t) 15.95
15.87.2 dmax: PG.32.1.4 (a) dmax = 2.75*[D*t*(1-K)]^(1/3) 15.96 tn: Nominal thickness of nozzle wall
15.87.3 PG.32.1.4 (b) 15.97
15.87.4 Max (15.42.2 & 15.42.3) 15.97.1#
15.87.5 15.97.2
Reinforcing Element
15.98 15.100 Allowable stress in reinforcing element
15.99 (see Fig. PG-33.2) 15.101 Out side diameter of reinforcing element
Area of Reinforcement Available (PG-33.3, Fig. PG-33.1)
Relations Inputs
15.102 Factor from PG-33 and Fig. PG-33.3
15.103 Sn /Sv 15.104 Sn /Sv or Sp/Sv 15.105 Sp/Sv
15.106 15.107 15.108
15.106.1 0.7xt min 15.106.2
Area of Reinforcement Required Area available in nozzle
15.109 A=(d+2tn)trF 15.113 A2a=2(tn – trn)(21/2tfr1)
Area available in shell 15.114 A2b=2(tn – trn)(21/2tn + te)fr1
15.110 A1a=(d-2tn)(t-Ftr) 15.115 Use smaller value
15.111 A1b=2t(t-Ftr) 15.116
15.112 Use larger value 15.117 Area available in welds
15.118 A41 A41=(WL1^2)fr2
15.119 A43 A43=(WL3^2)fr1
Results
15.120 A1+A2+A3+A41+A43
15.121 CONCLUSION 1 No need calculation and no need Reinforcing Element
With reinforcing element added:
Area available in outer element weld Area available in element
15.122 A42=(WL2^2)fr3 15.123 A5=(Dp – d – 2tn)tefr3
15.124 CONCLUSION 2 No need calculation and no need Reinforcing Element
PG-32.1.3 Limit minimum distance to be single
opening.
12 OPENINGS (HANDHOLE N15)ASME Code Section I, Edition 2010, Addenda 2011
3x4x1/2x2
For nozzle wall inserted through the vessel wall (PG-33.3, Fig. PG-33.1)
Qty: 6 Each
0.4
P: 165 psi Sn 17100 psi
Material: SA-516 Gr-70 y: SA-106
Rv 30.02
Gr-B y:0.4 Material:
Required thickness of a seamless nozzle. trn=0
per PG-33.3 for manhole and nozzle.
Dp 0 in
in d: 3.000 in
tc DWG 0.263 in
in
Sv: 20000 psi Rn
t: 0.315 in C: 0.000 in
tr: 0.249 in Limit: 3.000 in
1.500 in
C: 0.000 in 4.000 in
3.694 in 0.5 in
K: 0.873 - trn: 0.000 in
3.694 in h: 0.815 in Choosen
2.375 in h: 0.787 inPG-36.3 Maximum distance nozzle project
inwards from the outer surface of the vessel
wall
Material: SA-516 Gr-70 Sp: 20000 in
Condition: No need calculation Ls: 6.000 in
F 1
fr1 0.86 fr2 0.86
te: 0 in
A 0.996 sq in A2a 0.673 sq in
fr3 1.00
WL1 0.354 in WL2 0.000 in WL3 0.354
tc min 0.250 in
A2b 1.069 sq in
A1a 0.1321 sq in A2 0.673 sq in
1.69 sq in
A42 0.000 sq in A5 0.000 sq in
A1 0.1321 sq in
0.107 sq in
0.107 sq in
A1b 0.0416 sq in A3 0.673 sq in
SERVICIOS INDUSTRIALES Y CALDERAS
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CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 16
15.125 Steam Outlet:
Vessel Inputs Nozzle Inputs
15.132.6
15.126 15.133
15.127 Maximum allowable working pressure 15.134 Allowable stress in nozzle
15.128 Allowable stress in vessel 15.135 Inside radius of the nozzle under consideration
15.129 Inside radius of cylinder 15.136 Inside diameter of the nozzle under consideration
15.130 15.137 do: Outside diameter
15.131 Required Thickness of the Vessel (See 07.09) 15.138 d or Rn + tn + t, use larger value PG-36.2.1 & 2
15.132 Thickness of the vessel wall 15.139
15.132.1 PG-32.1.1 K = P*D/(1.82*S*t) 15.140
15.132.2 PG.32.1.4 (a) dmax = 2.75*[D*t*(1-K)]^(1/3) 15.141 Nominal thickness of nozzle wall
15.132.3 PG.32.1.4 (b) 15.142
15.132.4 Max (15.42.2 & 15.42.3) 15.142.1#
15.132.5 15.142.2
Reinforcing Element
15.143 15.145 Allowable stress in reinforcing element
15.144 (see Fig. PG-33.2) 15.146 Out side diameter of reinforcing element
Area of Reinforcement Available (PG-33.3, Fig. PG-33.1)
Relations Inputs
15.147 Factor from PG-33 and Fig. PG-33.3
15.148 Sn /Sv 15.149 Sn /Sv or Sp/Sv 15.150 Sp/Sv
15.151 15.152 15.153
15.151.1 0.7xt min 15.151.2
Area of Reinforcement Required Area available in nozzle
15.154 A=(d+2tn)trF 15.158 A2a=2(tn – trn)(21/2tfr1)
Area available in shell 15.159 A2b=2(tn – trn)(21/2tn + te)fr1
15.155 A1a=(d-2tn)(t-Ftr) 15.160 Use smaller value
15.156 A1b=2t(t-Ftr) 15.161
15.157 Use larger value 15.162 Area available in welds
15.163 A41 A41=(WL1^2)fr2
15.164 A43 A43=(WL3^2)fr1
Results
15.165 A1+A2+A3+A41+A43
15.166 CONCLUSION 1 Need a Reinforcing Element
With reinforcing element added:
Area available in outer element weld Area available in element
15.167 A42=(WL2^2)fr3 15.168 A5=(Dp – d – 2tn)tefr3
15.169 CONCLUSION 2 A1+A2+A3+A41+A42+A43+A5>=A, The design of Reinforcing Element is satisfactory
tc DWG 0.284 in
1.05 sq in
in
Dp 7.422 in
PG-32.1.3 Limit minimum distance to be single
opening.
PG-36.3 Maximum distance nozzle project
inwards from the outer surface of the vessel
wallChoosen
A42 0.099 sq in A5 0.920 sq in
A1 0.2347 sq in
0.107 sq in
0.107 sq in
A1b 0.0416 sq in A3 0.304 sq in
A2b 0.337 sq in
A1a 0.2347 sq in A2 0.293 sq in
A 1.120 sq in A2a 0.293 sq in
fr3 1.00
WL1 0.354 in WL2 0.315 in WL3 0.354
tc min 0.250 in
F 1
fr1 0.86 fr2 0.86
te: 0.315 in
Material: SA-516 Gr-70 Sp: 20000 in
Condition: Need calculation Ls: 8.052 in
3.694 in h: 0.750 in
2.375 in h: 0.787 in
Required thickness of a seamless nozzle. trn=0
per PG-33.3 for manhole and nozzle.
dmax: 3.694 in tn: 0.237 in
K: 0.873 - trn: 0.020 in
in
t: 0.315 in C: 0.000 in
C: 0.000 in 4.500 in
tr: 0.249 in Limit: 4.026
Rv 30.02 in d: 4.026 in
Sv: 20000 psi Rn 2.013 in
12 OPENINGS (Steam Outlet N06)ASME Code Section I, Edition 2010, Addenda 2011
NPS-4 Sch 40
For nozzle wall inserted through the vessel wall (PG-33.3, Fig. PG-33.1)
Qty: 1 Each
SA-106 Gr-B y: 0.4
P: 165 psi Sn 17100 psi
Material: SA-516 Gr-70 y: 0.4 Material:
SERVICIOS INDUSTRIALES Y CALDERAS
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CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 17
16.01 Tubesheet diameter
16.02 Firetube Hole Diameter
16.03 Furnace Hole Diameter
16.04 O.D. Stiffener Ring. If there is not then N/A
16.05 I.D. Stiffener Ring. If there is not then N/A
16.06 O.D. Furnace Diameter
16.07 O.D. Firetube Diameter
16.08 O.D. Wetback Inspection Door ring. If there is not then N/A
16.09 In side Length between Tubesheets
16.10 Wetback Inspection Door Length. If there is not then N/A
16.11 Stiffener Ring Thickness. If there is not then N/A
16.12 Total Holes in Front Tubesheet for Firetubes
16.13 Total Holes in Rear Tubesheet for Firetubes
16.14 Total of Stiffener Rings
16.15 Total Firetubes
16.16 Complete tubesheet Area
16.17 Steam Area in Tubesheet Autocad DWG-004
16.18 Holes Area in Front Tubesheet by Firetubes
16.19 Hole Area in Front Tubesheet by Furnace
16.20 Holes Area in Rear Tubesheet by Firetubes
16.21 Area occupied by Wetback. (If boiler is wet back, areas come from drawings)
16.22 Area Stiffener Rings
16.23 Heating surface in Front Tubesheet
16.24 Heating surface in Rear Tubesheet
16.25 Heating Surface in Firetubes
16.26 Heating Surface in Furnace
16.27 Heating Surface in Wetback Component 2
16.28 Heating Surface in Wetback Component 3
16.29 Heating Surface in Wetback Component 4
16.30 Heating surface in Wetback Inspection Door
16.31 HEATING SURFACE
17.01 Boiler Heating Surface
17.02 Constant for Boiler Heating Surface (Table A-44)
17.03 Steam Capacity
17.05 Valved quantity
17.06 Minimum flow (pounds/hr per valve)Flow/valve 2817
n: 2
sq-ft
14 STEAM CAPACITY COMPUTATIONASME Code Section I Division 1, Edition 2010, Addenda 2011
0 sq-ftA6:
SC: 5635 pounds/hr
sq-ft
SCBHS 8 pnds/hr*sq-ft
BHS: 704.3
A4: 60.16 sq-ft
HT: 704.3
A7: 0 sq-ft
A8: 0.0 sq-ft
A5: 0
13 HEATING SURFACE COMPUTATIONASME Code Section I, Edition 2010, Addenda 2011
sq-ft
Ats: 2831 sq-in
Ast: 503 sq-in
102 un
n3: 0 un
501 sq-in
A3:
d1: 60.04 in
d2: 2.5 in
d3: 25.05 in
501 sq-in
Ahf: 493 sq-in
A1: 13 sq-ft
A2: 13 sq-ft
d4:
619 sq-ft
N/A in
d5: N/A in
n4: 102 un
N/A in
int: N/A
d6: 24.8 in
L: 111.2 in
d7: 2.5 in
d8: N/A in
L1:
Asr: 0 sq-in
Ahr:
sq-in
Ahft:
n1: 102 un
n2:
Awb: N/A
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 18
Welding material (aprox 1%)
Accesories (1%)
Total Material Weight
Water Weight (full)
Material + Water Weight (full)
18.21 7383.89
3.33
Steam Difsor
9.802.45
1
1
6
91.00
1
1
3.33
18.48
18.22 14924.02
33.99 135.96
50.00 100.00
50.00 50.00
4
2
SA-3618.16 15
18.19
18.20
1
18.48
4
31.54 31.54
5
2
3.27 16.35
6.26 12.52
91.00
7.00 42.00
339.82
2923.32
1275.36
252.7403 Front Tubesheet SA-516 252.741
339.82
28.66
1
102
18.02
Total Weight (lb)
2090.0618.01 01 Boiler Shell SA-516
Item Component Spec. No.Type /
Grade
2090.06
1275.36
Weight per Unit
(lb)QTY
1
102 Furnace SA-516
18.05 05 Firetubes SA-192
18.04 04 Rear Tubesheet SA-516
18.03
18.07 07 Handhole SA-106
18.06 06 Manhole SA-675
18.09 08.2 Diagonal Stays 02 SA-516
18.08 08.1 Diagonal Stays 01 SA-516
18.12 11 Flange 4" SA-105
18.11 10 Pipe NPS-4, Sch. 40 SA-106
18.10 09 Stack SA-516
Gr-70
-
Gr-B
-
18.13 12 Lugs SA-516
Gr-70
Gr-70
Gr-70
Gr-70
Gr-B
-
-
15 WEIGHT SUMMARY
Gr-70
-
Gr-70
Gr-70
Gr-70
18.15 14
18.14 13
Water Difusor SA-36
Legs SA-36
73.92
7540.12
18.18 73.92
18.17 SUB-TOTAL 7392.28
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 19
19.00 Material:(considered only for design)
Dimensions: Conditions:
19.01 A 19.07 Q:
19.02 B: 19.08 Sy: SA-106
19.03 R1: 19.09.01 Ssh: (Ssh=0,4*Sy)
19.04 D1: 19.09.02 St: (St=0,6*Sy)
19.05 0,25A 19.09.03 Sb: (Sb=0,66*Sy)#
19.06 1,5A 19.09.04 Qty: #
Thickness Due to Bending: Strobe angle
19.10 t1: 19.10.01 q = °
Thickness Due to Shear:
19.11 t2:
Thickness Due to Tension:#
19.12 t3:
Thickness Calculated:
19.13 t: t=MAX(t1,t2,t3)
Thickness Choosed:
19.14 tch: Thickness choosed for lug
Welded Joins (PRESSURE VESSEL HANDBOOK, EUGENE MEGYESY)
19.15 Length of the weld
19.16 Allowable load on Weld (factor)
19.17 Load on Fillet Weld
19.18 Fillet Weld Leg Dimension
19.19 Thickness choosed for base material, boiler sheel (see 07.10)
19.20 Minimum thickness between 19.14 & 19.19
19.21 Minimum Fillet Weld Size per "t min" plate, (see fig PW-16.2 a)
19.22 Minimum Fillet Weld Size per "t min" plate, (see fig PW-16.2 a)
19.23 Minimum Full penetration Size per "t min" plate, (see fig PW-16.2 b)
19.24 The field supervisor could select the weld size, 19.22 if fillet weld, 19.23 if full penetration.
45
0.315 in
leg: 0.3018 in
t min: 0.315 in
leg: 0.357 in
4 Each
Throat: 0.2500 in
W: 1.184 kips/in
w: 0.123 in
Aw: 10.13 in
f:
t:
9.6 kips/sq-in
0.162 in
0.567 in
0.50 in
6.75 in
0.567 in
0.243 in
1.25 in 22800 psi
1.13 in 25080 psi
4.00 in 38000 psi
2.25 in 15200 psi
16 Lifting Lugs DesignPRESSURE VESSEL DESIGN MANUAL, DENNIS MOSS / PRESSURE VESSEL HANDBOOK, EUGENE MEGYESY
SA-516 Gr. 70
4.50 in 12000.0 lb
6*Qx*B
t1 =
A2*Sb
Qx
t2 =
(A - D1) * Ssh
Q
t3 =
(A - D1) * St
Q
Aw W =
Aw = 2* (A + t)
SERVICIOS INDUSTRIALES Y CALDERAS
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CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 20
Dimensions Conditions
19.20 Length 19.27 W: Total weight (including full water)
19.21 Radius of Shell (out) 19.28 Q: Load on one saddle (Q=Qt/4, See 18.42)
19.21.1 19.29 P: Design Pressure (See 03.22)
19.22 deg Saddle Contact Angle 19.30 Temp: Operating Temperature (See 03.22)
19.23 deg Angle between center line and load 19.31 E: Circ Joint Efficiency
19.24.0 Long wear plate (pag. 102 EUGENE MEGYESY 10 th ed.) Materials4
19.24.1 Wide wear plate (pag. 102 EUGENE MEGYESY 10 th ed.) 19.32 Shell Material
19.24.2 19.33 Allowable Shell Stress
19.24.3 19.34 Yield Point
19.24.4 19.35 Modulus or elarticity
19.24.5 Lever arm of load, inch.
19.25 Corroded Shell Thickness
19.26 Corroded Head Thickness
K Factors (Page 103-104):
19.36 19.38 19.40 19.42
19.37 19.39 19.41 19.43
Stress Limits:
19.44 S1t: S1= Q/t2 [cosa(-K1 + 6K2)+H/R VR/t (-K3 + 6K4)] Longitudinal Stress
19.45 S2t: S2= Q/t2 [cosa(-K5 + 6K6)+H/R VR/t (-K7 + 6K8)] Cincumferntial Stress
19.46 S1c: S1= Q/t2 [cosa(-K1 - 6K2)+H/R VR/t (-K3 - 6K4)] Longitudinal Stress
19.47 S2c: S2= Q/t2 [cosa(-K5 - 6K6)+H/R VR/t (-K7 - 6K8)] Cincumferntial Stress
19.48 S: S= PR/2t The stress due to internal pressure
19.49 SL : SL = Sa x E Limit of the stress value of the girth seam
19.50 S1t+S : /S1t+S/ < SL, is proper the support selection
19.51 S1c+S : /S1c+S/ < SL, is proper the support selection
19.52 S2t+S : /S2t+S/ < SL, is proper the support selection
19.53 S2c+S : /S2c+S/ < SL, is proper the support selection
19.53.1 Note: - The analysis was made considering the shell only 2 support points (or 4 legs).
- The shell is built on 3 support points (or 6 legs).
in5.912B:
5.2844C:
18285.27 psi
-3187.56 psi
20000.00 psi
17347.00 psi
-4856.09 psi
-12816.38 psi
-11147.84 psi
7960.28 psi
10324.99 psi
0.020000 K5: 0.006250
0.002000
9386.72 psi
K7: 0.004000
K2: 0.004000 K4: 0.031250 K6:
K3:
K8: 0.031250
th: - in
K1: 0.020000
psi
ts: - in
t: 0.315
4.55H:
3.1087D:
in
Sy: 38000 psi
E: 29000000
SA-516 Gr 70
Sa: 20000 psi
2A: 18.9 in
Theta: 120 373 ºF
a : 36 1 -
Qty: 2 Pair 165 psi
1543.812
16 Saddles Design (Part 01)HANDBOOK EUGENE MEGYESY (Tenth Edition) and Dennis Moss
L: 141.62 in 14924.0
R: 30.39 in 3731.0 lb
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 21
Dimensions Conditions
19.54 Height of the support 19.67 W: Total weight (including full water)
19.55 Long of the support base 19.68 Q: Load on one base (Q=W/4, See 11.27)
19.56 Wide of the support base 19.69 P: Design Pressure (See 03.22)
19.57 Support thickness 19.70 Temp: Operating Temperature (See 03.22)
19.71 E: Circ Joint Efficiency
Properties Materials
19.58 Inertia 19.72 Support Material
19.59 Inertia 19.73 Allowable Shell Stress
19.60 Radius 19.74 Yield Point
19.61 Radius 19.75 Elasticity modulus
19.62 Net Area#
19.63 Gross Area
19.64 Buckling length (in this case Lp=0.5L)
19.65 Lb Buckling load Fp = (π E I) / Lp2
19.66 Conclusion 1: Fp>Q 'No Buckling failure'
Centric compression analysis
19.76 l : mechanical slenderness
19.77 w : buckling coefficient
19.78 g : safety factor
19.79 s : Work stress
19.80 sad : Allowable stress
19.81 Qmax: Maximum load allowable per support
19.82 Conclusion 2: Qmax>Q 'Selected support is correct'
19.83 This analysis was performed considering a uniform section for support. This will be the most critical condition for support.
19.84 Note: - The analysis was made considering the shell only 2 support points (or 4 legs).
- The shell is built on 3 support points (or 6 legs).
6.5558
5.61
1.04
60490.38 Lb
1110.23
psi
Fp:
Ag: 13.987
2.00
10113101.68
psi
18000.00 psi
Sy: 36000 psi
Lp: 7.685
E: 29000000
in2
in2
in
ry: 1.3696
S-A36 -
An: 3.495
Sa: 16600 psi
rx: 1.4889 in
Ix: 7.7475 in4
in4
in
Iy:
t: 0.25 373 ºF
1 -
in
A: 3.94 in 3731.0 lb
B: 3.55 in 165 psi
16 Saddles Design (Part 02)HANDBOOK, NICOLAS LARBURU (thirteenth Edition)
L: 15.37 in 14924.0
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 22
Maximum Allowable Working Pressure (PG-21)
Working temperature
Maximum Allowable Working Pressure at Test Temperature
Note 1: per A-22.8
Note 2:
No, Design is Satisfactory20.40 37 Handhole SA-106 Gr-B 35000 17100 17100 248
ºF
Pt: 248 psi
20000
248
248
248
248
St (A-22.8)
[MASV at test
temperature]
(psi)
248
248
248
248
Po (A-22.8)
[MAWP at
design
temperature]
(psi)248
224
248
248
229
20000
No part of the boiler shall be subjected to a general membrane stress greater than 90% of its yield strength (0.2% offset) at
test temperature.
20.19
20.01
20.02
20.03
20.2
No, Design is Satisfactory
No, Design is Satisfactory
No, Design is Satisfactory
No, Design is Satisfactory
No, Design is Satisfactory
248
248
248
MAWP: 165 psi
T: 373
20000
20000
20000
13400
38000
20000
17100
17100
17100
17100
20000
20000
20000
20000
20000
20000
20000
17100 17100
20000
20.36 33 Explosive Cover SA-516
20.39 36 Rear Cover SA-516 Gr-70
38000 2000020.38 35 Water Difusor SA-516 Gr-70
38000
20000
20.35 32 Radial Stiffeners SA-516 Gr-70
20.37 34 Water Difusor SA-516 Gr-70
38000
16600 16600 248
248
248
248
248
248
248
38000
17100 17100
28 Reduction NPS-8 to NPS-6, Sch. 40 SA-234 WPB
35000
Gr-70
38000
20000
20000 20000
20000
17100
17100
17100
17100
20000
20000
20000
20000
16600
20.30 27 Pipe NPS-6, Sch. 40 SA-106 Gr-B
35000
No, Design is Satisfactory20.34 31 Front Inspection Door SA-516 Gr-70
38000
No, Design is Satisfactory
No, Design is Satisfactory
No, Design is Satisfactory
No, Design is Satisfactory
No, Design is Satisfactory
No, Design is Satisfactory
No, Design is Satisfactory
No, Design is Satisfactory
No, Design is Satisfactory
20.31
16600
20.29 26 Elbow, NPS-6, Sch. 40 SA-234 WPB
35000
No, Design is Satisfactory
20.33 30 Hinges SA-516 Gr-70
3800020.32 29 Front Cover SA-516 Gr-70
35000
No, Design is Satisfactory
No, Design is Satisfactory
16600
20.28 25 Pipe NPS-6, Sch. 40 SA-106 Gr-B
3800020.16 12 Lugs SA-516 Gr-70
20.15 11 Flange 4" 150# SA-105 -
35000
36000
248
17100 17100 248
16600
20.14 10 Pipe NPS-4, Sch. 40 SA-106 Gr-B
36000
No, Design is Satisfactory
No, Design is Satisfactory
20.13 09 Stack SA-516 Gr-70
3600020.12 08.2 Diagonal Stays 2 SA-516 Gr-70
3600020.11 08.1 Diagonal Stays 1 SA-516 Gr-70
3500020.10 07 Handhole SA-106 Gr-B
35000
12400 No, Design is Satisfactory
20.09 06 Manhole SA-675 Gr-70
Firetubes SA-192 -
20000 No, Design is Satisfactory
2600020.08 05
20000 No, Design is Satisfactory
20000 No, Design is Satisfactory3800020.07 04 Rear Tubesheet SA-516 Gr-70
3800020.06 03 Front Tubesheet SA-516 Gr-70
17 HYDROSTATIC TEST SUMMARYASME Code Section I, Edition 2010, Addenda 2011
Item Component Spec. No.Type /
Grade
Sy [Yield Point
Stress] (psi)
3800020.05 02 Furnace SA-516 Gr-70
3800020.04 01 Boiler Shell SA-516 Gr-70
So (A-22.8)
[MASV at the
design
temperature]
(psi)
Po is greater than
0,9Sy? (CONDITION
PER PG-99.1)
18100 No, Design is Satisfactory
No, Design is Satisfactory
20.18 14 Water Difusor SA-36 - 36000 16600 16600 248 No, Design is Satisfactory
20.17 13 Legs SA-36 - 36000 16600 16600 248
No, Design is Satisfactory20.19 15 Steam Difusor SA-36 - 36000 16600 16600 248
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 23
18.01.02 Tubesheet Thickness 18.02.02 Tubesheet Thickness
18.01.03 Shell Thickness 18.02.03 Shell Thickness
18.01.04 Tc1 = 0,7*Tt 18.02.04 Tc2 = 0,7*Tt
18.03.02 Tubesheet Thickness 18.02.02 Tubesheet Thickness
18.03.03 Shell Thickness 18.02.03 Shell Thickness
18.03.04 Tc =1/4 min 18.02.04 Tc2 = 0,7*Tt
18.04.02 18.05.02
18.05.03 " lenght per side
18.05.04 Choosen welded
in
18.03.01 SHELL-TUBESHEET
(PFT-11.4.3)
Tc 0.25 in Tc2 0.35
in
Ts 0.375 in Tf 0.375 in
Tt 0.5 in Tt 0.5
Lw 3.00 in
Lw 5.00 in
(PW-19.2 & PW-19.3) (PW-19.4.1)
Per PW-19.3 The ends of stays inserted through the sheet
shall not project more than 3⁄8 in. (10 mm) beyond surfaces
exposed to products of combustion.
- Fillet welds shall be not less than 3⁄8 in. (10 mm) size and
shall continue the full length of each side of the portion of
the stay in contact with the shell.
- Lw = lenght welded
18.04.01 TUBESHEET - DIAGONAL STAYS 18.05.01 CYLINDRICAL SHELL DIAGONAL STAYS
Tc2 0.35 in
(PFT-11.3.4)
Tt 0.5 0.5 in
Tf 0.375 in
1.5
18.02.01 FURNACE-TUBESHEET
18 WELDING JOINTS DESIGNASME Code Section I, Edition 2010, Addenda 2011
in
Ts 0.375 in
18.01.01 SHELL-TUBESHEET
Tc1 0.35 in
(PFT-20.2.3)
Tt
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 24
05
18 Changed value on the row 19.02 & 19.09.04 20 J. CATTAN
19 Added row 19.10.01, 19.11, 19.13, 19.15, 19.17, 19.18 20 J. CATTAN
19 REVISIONS
REVISION ITEM DESCRIPTION SHEET BY REV. BY ACCEPTED
02 Changed material on the row 05.06 06 J. CATTAN
01 Changed operarion condition 01 J. CATTAN
04 Changed material on the row 06.14 07 J. CATTAN
05 Changed stay diameter, row 11.09 13 J. CATTAN
03 Changed size of nozzle N04, row 06.04 07 J. CATTAN
07 Changed "L" value , row 11.19 13 J. CATTAN
06 Changed "Paw" value , row 11.17 13 J. CATTAN
09 Changed values on the row 15.17.2 14 J. CATTAN
08Changed size of nozzle N04, and all de corresponding
values14 J. CATTAN
11Change values on 15.44; 15.58; 15.59; 15.68; 15.69; 15.70;
15.71; 15.73; 15.74; 15.7515 J. CATTAN
10 Changed material on the row 15.43 15 J. CATTAN
13 Changed material on the row 11.01 13 J. CATTAN
12 Changed material on the row 05.09 06 J. CATTAN
15Changed value on the row 16.12, 16.13, 16.15, 16.18,
18.20, 18.25, 16.31, 17.1, 17.3, 17.518 J. CATTAN
14 Changed value on the row 11.03, 11.08, 11.09 13 J. CATTAN
17 Changed value on the row 18.17 to 18.22 19 J. CATTAN
16Changed material on the row 18.06, 18.07, 18.08, 18.09,
18.1019 J. CATTAN
20 Changed material on the row 20.09, 20.11, 20.12, 20.13 23 J. CATTAN
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-01 SHEET No. 25
05
07 Added row 19.10.01, 19.11, 19.13, 19.15, 19.17, 19.18 20 J. CATTAN
20 J. CATTAN
05 Changed material on the row 20.09, 20.11, 20.12, 20.13 23 J. CATTAN
06 Changed value on the row 19.02 & 19.09.04
02Changed value on the row 16.12, 16.13, 16.15, 16.18,
18.20, 18.25, 16.31, 17.1, 17.3, 17.518 J. CATTAN
01 Changed operarion condition 01 J. CATTAN
19 REVISIONS
REVISION ITEM DESCRIPTION SHEET BY REV. BY ACCEPTED
03 Changed quantity value on the row 18.05 19 J. CATTAN
04Changed material on the row 18.06, 18.07, 18.08, 18.09,
18.1019 J. CATTAN
SERVICIOS INDUSTRIALES Y CALDERAS
Quevedo - Ecuador
CONTRACT 2012 CEP 132
PROJECT No.: P2013-013-03 SHEET No. 25