flange design mmcobc 1.1 2010
TRANSCRIPT
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DESIGN OF CIRCULAR STEEL FLA T-FACE FLANGE W ITH METAL-TO-METAL CONTACT OUTSIDETHE BOLT CIRCLE - INTEGRAL TYPE FLANGE WITH SELF-SEALING GASK ETREFERENCE DRAWINGS: =DESIGN CONDITIONS:
DESIGN CODE =
[CLASS 1 ASSEMBLY / CATEGORY
DESIGN TEMPERATURE = C
DESIGN PRESSURE P = MPa
FLANGE MATERIAL DATA:FLANGE MATERIAL =
DESIGN TENSILE STRENGTH @ AMBIENT Sf = MPa
DESIGN TENSILE STRENGTH @ DESIGN TEMP. Sf = MPa
HUB MATERIAL: =
DESIGN TENSILE STRENGTH @ AMBIENT Sn = MPa
DESIGN TENSILE STRENGTH @ DESIGN TEMP. Sn = MPa
MODULUS OF ELASTICITY @ OPERATING TEMP. EI = MPa
BOLT/STUD DATA:MATERIAL =
PROOF STRENGTH Fy = MPa
DESIGN TENSILE STRENGTH @ AMBIENT Sa = MPa
DESIGN TENSILE STRENGTH @ DESIGN TEMP. Sb = MPa
MODULUS OF ELASTICITY @ OPERATING TEMP. E = MPa
NOMINAL DIAMETER db = mm
AREA Ab/n = mm
NO. OF THREADED ENDS (BOLT = 1 STUD = 2) =
FLANGE DIMENSIONS (REFER FIG. Y-3.2 FOR NOTATION):OUTSIDE DIAMETER A = mm
INSIDE DIAMETER B = mm
BOLT CIRCLE DIAMETER C = mm
THICKNESS OF HUB @ SMALL END go = mm
THICKNESS OF HUB @ BACK OF FLANGE g1 = mm
HUB LENGTH (h > 0) h = mm
NO. OF BOLTS n =
BOLT HOLE DIAMETER D = mm
OUTSIDE DIAMETER OF SPACER (=A, IF NONE) = mm
GASKET DATA:MATERIAL =
DIAMETER = mm
GASKET FACTOR m =
MIN DESIGN SEATING STRESS y = MPa
OUTSIDE DIAMETER = mm
INSIDE DIAMETER = mm
DIA. @ LOCATION OF GASKET LOAD REACTION G = 0.0 mm
BOL T-FORCES / MOMENT ARMS (REFER FIG. Y-3.2 FOR NOTATION):HYDROSTATIC END-FORCE H = 0 N
H'STATIC END FORCE ON AREA I/S OF FLANGE HD = 0 N
GASKET LOAD HG = 0 N
HYDROSTATIC END FORCE HT = 0 N
MOMENT ARM hD = 0.0 mm
MOMENT ARM hG = 0.0 mm
MOMENT ARM hT = 0.0 mm
ASME BPVC SECT. VIII - DIV. 1 [2
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SUGGESTED TRIAL VAL UES:FLANGE THICKNESS ta = #DIV/0! mm
BOLT AREA Ab' = #DIV/0! mm
SUGGESTED TRIAL FLANGE THICKNESS t = #DIV/0! mm
SUGGESTED TOTAL AREA OF BOLTS Ab = #DIV/0! mm
SUGGESTED AREA OF BOLT Ab/n = #DIV/0! mm
RADIAL DIST. FROM B.C.D. TO BEARING CIRCLE hC = 0 mm
SELECTED VALUES:SELECTED FLANGE THICKNESS t = mm
SELECTED AREA OF BOLT Ab/n = 0 mm
RADIAL DIST. FROM B.C.D. TO BEARING CIRCLE hC = mm
hCmax = 0 mm
THICKNESS OF SPACER ts = mm
THICKNESS OF WASHERS, ETC = mm
MISCELLANEOUS CALCULATIONS:g1/go = #DIV/0!
ho = 0.0
h/ho = #DIV/0!
K = #DIV/0!
T = #DIV/0!
U = #DIV/0!
Y = #DIV/0!
Z = #DIV/0!
F = #DIV/0!
V = #DIV/0!
f = #DIV/0!
e = #DIV/0!
d = #DIV/0!
L = #DIV/0!
B1 = #DIV/0!
SHAPE FACTOR a = #DIV/0!
SHAPE FACTOR = #DIV/0!
BOLT HOLE ASPECT RATIO AR = #DIV/0!
rB = #DIV/0!
Jp = #DIV/0!
Js = #DIV/0!
CALCULATED STRAIN LENGTH OF BOLT l = 0.0 mm
ELASTICITY FACTOR rE = #DIV/0!
F' = #DIV/0!
FLANGE MOMENT DUE TO FLANGE-HUB INTERACTION:Ms = #DIV/0! N-m
SLOPE OF FLANGE A T DIAMETER B TIMES E:EqB = #DIV/0! MPa
SLOPE qB = #DIV/0! rad
= #DIV/0! deg
CONTACT FORCE BETWEEN FLANGES AT hC:HC = #DIV/0! N
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BOL T LOAD AT OPERATING CONDITIONS:REQUIRED BOLT-FORCE Wm1 = #DIV/0! N
BOLT AREAS:REQUIRED BOLT-AREA Am = #DIV/0! mm
TOTAL BOLT-AREA Ab
= 0 mm
OPERATING BOL T STRESS:OPERATING BOLT STRESS sb = #DIV/0! MPa
DESIGN PRESTRESS IN BOLTS:DESIGN PRESTRESS IN BOLTS Si = #DIV/0! MPa
PERCENTAGE OF YIELD STRESS = #DIV/0! %
TYPE OF LUBRICANT =
NUT FACTOR (TORQUE CO-EFFICIENT) =
BOLT PRELOAD = #DIV/0! kN
BOLT TORQUE = #DIV/0! N-m
RADIAL FLANGE STRESS AT B OLT CIRCLE:SR = #DIV/0! MPa
RADIAL FL ANGE STRESS AT INSIDE DIAMETER:SR = #DIV/0! MPa
TANGENTIAL FLA NGE STRESS AT INSIDE DIAMETER:ST = #DIV/0! MPa
LONGITUDINAL HUB STRESS:SH = #DIV/0! MPa
(SH+SR)/2 = #DIV/0! MPa
(SH+ST)/2 = #DIV/0! MPa
ALLOW ABL E FLANGE DESIGN STRESSES:BOLTS:
Sb = 0.0 MPa
FLANGE:
SR = 0.0 MPa
ST = 0.0 MPa
SH = 0.0 MPa
(SH+SR)/2 = 0.0 MPa
(SH+ST)/2 = 0.0 MPa
DESIGN SUMMARY:FLANGE STRESSES Sact/Sall = #DIV/0!
BOLT STRESS sb/Sb = #DIV/0!
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A = #DIV/0! C 1 = #DIV/0! E
C = #DIV/0! C 2 = #DIV/0! E
C 3 = #DIV/0! E
C 4 = #DIV/0! E
C 5 = #DIV/0! E
C 6 = #DIV/0! EC 7 = #DIV/0!
C 8 = #DIV/0!
C 9 = #DIV/0!
C 10 = #DIV/0!
C 11 = #DIV/0!
C 12 = #DIV/0!
C 13 = #DIV/0!
C 14 = #DIV/0!
C 15 = #DIV/0!
C 16 = #DIV/0!
C 17 = #DIV/0!
C 18 = #DIV/0!
C 19 = #DIV/0!
C 20 = #DIV/0!
C 21 = #DIV/0!
C 22 = #DIV/0!
C 23 = #DIV/0!
C 24 = #DIV/0!
C 25 = #DIV/0!
C 26 = #DIV/0!
C 27 = #DIV/0!
C 28 = #DIV/0!
C 29 = #DIV/0!
C 30 = #DIV/0!
C 31 = #DIV/0!
C 32 = #DIV/0!
C 33 = #DIV/0!
C 34 = #DIV/0!
C 35 = #DIV/0!
C 36 = #DIV/0!
C 37 = #DIV/0!
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1 = #DIV/0!
2 = #DIV/0!
3 = #DIV/0!
4 = #DIV/0!
5 = #DIV/0!
6 = #DIV/0!