AS AÇÕES DO VENTO
Por: cavalc10 • 2/1/2017 • Trabalho acadêmico • 11.845 Palavras (48 Páginas) • 254 Visualizações
MEMORIAL DE CÁLCULO TANQUE TIER III
DADOS:
SOFTWARE DE CALCULO: AMETank 7.7
NORMA DE PROJETO: API 620
DIAMETRO INTERNO: 3820 mm
ALTURA DO CORPO: 8000 mm
TEMPERATURA MINIMA: 4 ºC
TEMPERATURA MAXIMA: 20 ºC
PRESSÃO DE OPERAÇÃO: 0,3 Kgf/cm ²
MATERIAL: ASTM A-36
TABLE OF CONTENTS
Summary of Design Data and Remarks
Tank Design Parameters
Roof Design
Top Member Design
Shell Design
Bottom Design
Site Ground Motion
Seismic Design
Wind Design Pressures
Wind Design
Anchorage Design
Normal and Emergency Venting (API-2000)
Capacities And Weight
Back
SUMMARY OF DESIGN DATA AND REMARKS
Overview
Job = 2014-12-10-23-44
Calculations Date = 10-Dec-2014
Manufacturing or Inspection Date =
Designer = Alan Cavalcante
Project =
Tag Number =
Plant = PURCHASER DESCRIPTION CITY AND STATE
Plant Location =
Site =
Design Basis = API-620 ()
Tank Nameplate Information
Pressure Combination Factor | N/A |
Design Standard | API-620 () |
Appendicies Used | L, R |
Roof | A36 : 0.25 in |
Shell (1) | A36 : 0.3752 in |
Shell (2) | A36 : 0.3752 in |
Shell (3) | A36 : 0.3126 in |
Shell (4) | A36 : 0.3126 in |
Shell (5) | A36 : 0.25 in |
Shell (6) | A36 : 0.25 in |
Bottom | A36 : 0.25 in |
Designer Remarks
Remarks or Comments
SHELL DESIGN
Shell Courses
Course # | Course Height (ft) | Material | Corrosion Allowance (in) | Joint Efficiency | Sd (lb/in^2) | Weight New (lbf) |
1 | 4.9213 | A36 | 0 | 0.7000 | 16000.0000 | 2965.8306 |
2 | 4.9213 | A36 | 0 | 0.7000 | 16000.0000 | 2965.8306 |
3 | 4.9213 | A36 | 0 | 0.7000 | 16000.0000 | 2470.9985 |
4 | 4.9213 | A36 | 0 | 0.7000 | 16000.0000 | 2470.9985 |
5 | 4.9213 | A36 | 0 | 0.7000 | 16000.0000 | 1976.1665 |
6 | 1.6404 | A36 | 0 | 0.7000 | 16000.0000 | 658.7244 |
Shell Courses (continued)
Course # | Weight CA (lbf) | t-min Erection (in) | t-min Internal Pressure (in) | t-min Seismic (in) | t-min External Pressure (in) | t-actual (in) |
1 | 2965.8306 | 0.1875 | 0.1050 | 0.0410 | 0 | 0.3752 |
2 | 2965.8306 | 0.1875 | 0.0906 | 0.0334 | 0 | 0.3752 |
3 | 2470.9985 | 0.1875 | 0.0763 | 0.0257 | 0 | 0.3126 |
4 | 2470.9985 | 0.1875 | 0.0620 | 0.0181 | 0 | 0.3126 |
5 | 1976.1665 | 0.1875 | 0.0477 | 0.0105 | 0 | 0.2500 |
6 | 658.7244 | 0.1875 | 0.0334 | 0.0027 | 0 | 0.2500 |
Back
TANK DESIGN PARAMETERS
D (Tank diameter) = 12.5328 ft
DL_added (Added dead load) = 0 psf
E (Tank Joinf efficiency) = 0.7
H_shell (Shell height) = 26.2467 ft
Liq_max (Maximum liquid level) = 26.2467 ft
Liq_min (Minimum liquid level) = 0 ft
Lr (Minimum roof live load) = 20.0 psf
Pg (Design pressure) = 4.2641 psi
Pv (Design vaccum) = 0.0 psi
S (Snow load) = 0.0 psf
SG (Specific gravity of content) = 1
T (Design temperature) = 4 degf
T_max_op (Max operating temperature) = 20 degf
T_min (Min design temperature) = 30 degf
V (Design wind velocity) = 125.0 mile/hr
site_ground_motion_input_mode (Site Ground Motion Input Mode) = asce7 mapped ss and s1
water_density (Water Density) = 62.37 lbf/ft^3
wind_method (Wind Method) = api 620 method
Product density
product_density = water_density * SG = 0.0361 * 1 = 0.0361 lbf/in^3
Test pressure API-620 7.18.3.4
Pt = 1.25 * Pg = 1.25 * 4.2641 = 5.3301 psi
API 620 Appendix R applied.
API 620 Appendix L applied.
Back
ROOF DESIGN
(Material) = A36
(Knuckle material) = A36
E (Joinf efficiency) = 0.7
Rc (Shell radius) = 6.2664 ft
Rs (Dish radius) = 10.0262 ft
c (Corrosion allowance) = 0 in
density_ins (Insulation Density) = 8 lbf/ft^3
t_act (Actual thickness) = 0.25 in
t_ins (Insulation thickness) = 0 in
t_knuckle (Knuckle actual thickness) = 0.25 in
Material density (density) = 0.2833 lbf/in^3
Maximum allowable tensile stress (Sts) = 16000.0 psi
As per API-620 Table 5-6, Erection Thickness (t_erection) = 0.1875 in
Corroded plates thickness
t_corr = t_act - c = 0.25 - 0 = 0.25 in
Geometry Calculations
Geometries
...