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PART ULTGeneral
ULT-1 Scope. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 290ULT-2 Conditions of Service. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 290ULT-5 General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 290
DesignULT-16 General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 291ULT-17 Welded Joints. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 291ULT-18 Nozzles and Other Connections. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 291ULT-23 Maximum Allowable Stress Values. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 291ULT-27 Thickness of Shells. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 291ULT-28 Thickness of Shells Under External Pressure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 291ULT-29 Stiffening Rings for Shells Under External Pressure. . . . . . . . . . . . . . . . . . . . . . . . . . . . 296ULT-30 Structural Attachments. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 296ULT-56 Postweld Heat Treatment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 296ULT-57 Examination. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 296
FabricationULT-75 General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 296ULT-79 Forming Shell Sections and Heads. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 296ULT-82 Welding. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 296ULT-86 Marking on Plate and Other Materials. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 299
Inspection and TestsULT-90 General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 299ULT-99 Pressure Test. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 299
Marking and ReportsULT-115 General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 299
Pressure Relief DevicesULT-125 General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 301
FigureULT-82 Weld Metal Delta Ferrite Content. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 300
288
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
TablesULT-23 Maximum Allowable Stress Values in Tension for 5%, 8%, and 9% Nickel
Steels, Type 304 Stainless Steel, and 5083-O Aluminum Alloy atCryogenic Temperatures for Welded and Nonwelded Construction. . . . . . . . . . . . . 292
ULT-82 Minimum Tensile Strength Requirements for Welding ProcedureQualification Tests on Tension Specimens Conforming to QW-462.1. . . . . . . . . . . 297
289
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
PART ULTALTERNATIVE RULES FOR PRESSURE VESSELS
CONSTRUCTED OF MATERIALS HAVING HIGHERALLOWABLE STRESSES AT LOW TEMPERATURE
GENERAL
ULT-1 SCOPE
The alternative rules in Part ULT are applicable topressure vessels or vessel parts that are constructed ofmaterials for which increased design stress values havebeen established for low temperature applications. Whenapplied, these rules shall be used in conjunction withthe requirements in Subsection A and Part UW ofSubsection B. The requirements of Subsection C donot apply except when referenced in Part ULT.
ULT-2 CONDITIONS OF SERVICE
(a) Measures shall be taken to avoid stresses at anytemperature that are in excess of the maximum allowablestress applicable to that temperature. For example, themembrane stress at the maximum allowable workingpressure at 100°F (38°C) shall never exceed the maxi-mum allowable stress for 100°F (38°C). See ULT-27.
(b) Vessel use shall be restricted to fluids specificallyconsidered for the design of the vessel. The physicalcharacteristics of the contained fluid shall be such thata maximum operating temperature can be determinedfor the liquid phase at the maximum allowable workingpressure of the vessel. The safety relief valve settingthus controls the maximum operating temperature ofthe vessel for the specific fluid.
(c) The allowable stress at 100°F (38°C) shall beused for the design of vessel parts that are exposedto the static head of cryogenic fluid but are not actuallycontacted by the fluid, such as, as in a dead-end cylinderconnected to the bottom of a vessel that contains agas cushion.
(d) Insulation shall be applied external to the pressurevessel.
290
ULT-5 GENERAL
(a) Materials covered by this Part subject to stressdue to pressure shall conform to one of the specificationsgiven in Section II and shall be limited to those listedin Table ULT-23. The allowable stress values of TableULT-23 are limited to those materials which will be incontact with the cold liquid when subject to liquid head.
(b) Materials not covered by Part ULT may be usedfor vessel parts, provided such materials shall conformto one of the specifications in Section II and shall belimited to those materials permitted by another Part ofSubsection C. The maximum allowable stress for suchparts shall be determined at 100°F (38°C). All applicablerequirements of that Part of Subsection C shall be metincluding any required impact tests.
(c) The 5%, 8%, and 9% nickel steels listed in TableULT-23 shall be tested for notch ductility as requiredby UHT-5(d) and (e) and UHT-6. These ductility testsshall be conducted at the lowest temperature at whichpressure will be applied to the vessel or the minimumallowable temperature to be marked on the vessel,whichever is lower.
(d) For 5083 aluminum the provisions and require-ments of UNF-65 for low temperature operation apply.
(e) For 5%, 8%, and 9% nickel steel vessels, allstructural attachments and stiffening rings which arewelded directly to pressure parts shall be made ofmaterials of specified minimum strength equal to orgreater than that of the material to which they areattached.
(f) The weldments of Type 304 stainless steel shallbe Charpy impact tested as required by UG-84(h),except that the exemptions fo UHA-51 do not apply.These impact tests shall be conducted at the lowesttemperature at which pressure will be applied to thevessel or the minimum allowable temperature to bemarked on the vessel, whichever is lower. The applicable
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
ULT-5 PART ULT — LOW TEMPERATURE VESSELS ULT-28
minimum lateral expansion opposite the notch for allspecimen sizes shall be as required in UHT-6(a)(3)and (a)(4). All requirements of UHT-6(a)(3) and (a)(4)shall apply.
(g) For Type 304 stainless steel vessels, all structuralattachments and stiffening rings that are welded directlyto pressure parts shall be made of the same materialas the pressure part to which they are attached.
DESIGN
ULT-16 GENERAL
(a) The rules in the following paragraphs applyspecifically to the design of pressure vessels and vesselparts that are constructed of materials listed in TableULT-23 and shall be used in conjunction with therequirements for Design in Subsection A and Part UWof Subsection B.
(1) The thermal stresses resulting from the differ-ences between the base metal and the weld metal shallbe considered in the design.
(2) For vessels made of 5%, 8%, and 9% nickelsteels, the minimum thickness after forming of a sectionsubject to pressure shall be3⁄16 in. (4.8 mm) and themaximum thickness of the base metal at welds shallbe 2 in. (51 mm).
ULT-17 WELDED JOINTS
(a) All Category A, B, C, and D joints (UW-3) shallbe full penetration welds.
(b) The alignment of longitudinal joints in adjacentcylindrical sections or heads shall be displaced at leastfive times the thickness of the thicker material.
(c) In vessels of 5%, 8%, or 9% nickel steels, allCategory D joints shall be in accordance with Fig. UHT-18.1 or UHT-18.2 when the nominal shell thickness atthe opening exceeds 1 in. (25 mm).
(1) All joints of Category D attaching a nozzleneck to the vessel wall, and to a reinforcing pad ifused, shall be full penetration groove weld conformingto Fig. UHT-18.1 or Fig. UHT-18.2 or any of thesketches in Fig. UW-16 having full penetration welds.
(2) All joints of Category A shall be Type No.(1) of Table UW-12.
(3) All joints of Category B shall be Type No.(1) or (2) of Table UW-12.
(4) All joints of Category C shall be full penetra-tion welds extending through the entire section atthe joint.
291
(5) Joint alignment requirements of UHT-20 shallbe met.
(d) Butt welds with one plate edge offset [Fig. UW-13.1 sketch (k)] are prohibited anywhere in the vessel.
ULT-18 NOZZLES AND OTHERCONNECTIONS
(a) Nozzles shall not be located in Category A orB joints. When adjacent to Category A or B joints,the nearest edge of the nozzle-to-shell weld shall beat least five times the nominal thickness of the shellfrom the nearest edge of the Category A or B joint.
(b) The attachment of pipe and nozzle necks tovessel walls shall be by welded construction only.
ULT-23 MAXIMUM ALLOWABLE STRESSVALUES
Table ULT-23 gives the maximum allowable stressvalues at the temperatures indicated for materials con-forming to the specifications listed therein. Valuesmay be interpolated for intermediate temperatures (seeUG-23).
ULT-27 THICKNESS OF SHELLS
The minimum thickness of any vessel part shall bethe greater of the following:
(a) the thickness based on the MAWP at the top ofthe vessel in its normal operating position plus anyother loadings per UG-22, including the static head ofthe most dense cryogenic liquid to be contained. Thepermissible stress value shall be determined for theapplicable material in Table ULT-23 at the operatingtemperature corresponding to the saturation temperatureat MAWP of the warmest cryogenic fluid contained.The maximum allowable compressive stress shall bedetermined in accordance with UG-23(b) at 100°F(38°C) and the requirements of UG-23(c) shall be met.
(b) the thickness determined by using the permissiblestress value at 100°F (38°C) based on the MAWP atthe top of the vessel in its normal operating positionplus any other loadings per UG-22, except that nostatic head need be included.
ULT-28 THICKNESS OF SHELLS UNDEREXTERNAL PRESSURE
(a) Cylindrical and spherical shells under externalpressure shall be designed by the rules in UG-28 using
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
Table ULT-23 2001 SECTION VIII — DIVISION 1
01
TA
BL
EU
LT
-23
MA
XIM
UM
AL
LO
WA
BL
ES
TR
ES
SV
AL
UE
SIN
TE
NS
ION
FO
R5%
,8%
,A
ND
9%N
ICK
EL
ST
EE
LS
,T
YP
E30
4S
TA
INL
ES
SS
TE
EL
,A
ND
5083
-OA
LU
MIN
UM
AL
LO
YA
TC
RY
OG
EN
ICT
EM
PE
RA
TU
RE
SF
OR
WE
LD
ED
AN
DN
ON
WE
LD
ED
CO
NS
TR
UC
TIO
N
5%N
icke
lS
teel
s,C
usto
mar
yU
nits
8%an
d9%
Nic
kel
Ste
els,
Cus
tom
ary
Uni
ts
Pla
tes:
SA
-645
2P
late
s:2
SA
-353
,S
A-5
53T
ype
I,an
dS
A-5
53T
ype
IIP
ipes
and
Tub
es:
SA
-333
Gra
de8
and
SA
-334
Gra
de8
For
ging
s:S
A-5
22W
elde
dC
onst
ruct
ion3,
4W
elde
dC
onst
ruct
ion3,
4
Tem
pera
ture
,1N
onw
elde
dT
empe
ratu
re,1
Non
wel
ded
°FC
onst
ruct
ion,
ksi
UT
S10
0ks
iU
TS
95ks
i°F
Con
stru
ctio
n,ks
iU
TS
100
ksi
UT
S95
ksi
−32
043
.138
.936
.9−
320
43.9
38.9
36.9
−30
039
.437
.936
.1−
300
42.6
37.9
36.1
−25
037
.036
.334
.6−
250
39.8
36.3
34.6
−20
036
.035
.033
.3−
200
37.3
35.0
33.3
−15
034
.533
.531
.8−
150
35.1
33.5
31.8
−10
032
.932
.130
.5−
100
33.2
32.1
30.5
−50
31.3
31.0
29.5
−50
31.6
31.0
29.5
027
.127
.127
.10
28.6
28.6
27.1
100
27.1
27.1
27.1
100
28.6
28.6
27.1
Typ
e30
4S
tain
less
Ste
el,
Cus
tom
ary
Uni
ts
Spe
cifi
edM
inim
umS
tren
gths
atR
oom
Tem
pera
ture
Max
imum
Allo
wab
leS
tres
s,ks
i,fo
rT
empe
ratu
res,
1°F
,N
otE
xcee
ding
Ten
sile
,Y
ield
,S
pec.
No.
Gra
deks
iks
i−
320
−30
0−
250
−20
0−
150
−10
0−
500
100
SA
-240
nonw
elde
d30
475
.030
.035
.535
.033
.431
.729
.727
.525
.320
.020
.0co
nstr
ucti
onS
A-2
40w
elde
d30
475
.030
.023
.623
.423
.122
.822
.422
.121
.820
.020
.0co
nstr
ucti
on
Tab
leco
ntin
ues
onfo
llow
ing
page
292
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
PART ULT — LOW TEMPERATURE VESSELS Table ULT-23
01
TA
BL
EU
LT
-23
MA
XIM
UM
AL
LO
WA
BL
ES
TR
ES
SV
AL
UE
SIN
TE
NS
ION
FO
R5%
,8%
,A
ND
9%N
ICK
EL
ST
EE
LS
,T
YP
E30
4S
TA
INL
ES
SS
TE
EL
,A
ND
5083
-OA
LU
MIN
UM
AL
LO
YA
TC
RY
OG
EN
ICT
EM
PE
RA
TU
RE
SF
OR
WE
LD
ED
AN
DN
ON
WE
LD
ED
CO
NS
TR
UC
TIO
N(C
ON
T’D
)
5083
-OA
lum
inum
Allo
y,C
usto
mar
yU
nits
Spe
cifi
edM
inim
umS
tren
gths
atR
oom
Tem
pera
ture
Max
imum
Allo
wab
leS
tres
s,ks
i,fo
rM
etal
Tem
pera
ture
,1°F
,N
otE
xcee
ding
Spe
c.T
ensi
le,
Yie
ld,
No.
Allo
yT
empe
rT
hick
ness
,in
.ks
iks
i−
320
−30
0−
250
−20
0−
150
−10
0−
500
100
She
etan
dP
late
SB
-209
5083
O0.
051–
1.50
040
1815
.615
.314
.513
.813
.112
.512
.111
.411
.41.
501–
3.00
039
1714
.714
.413
.713
.012
.411
.811
.511
.111
.13.
001–
5.00
038
1613
.913
.612
.912
.211
.611
.110
.810
.710
.75.
001–
7.00
037
1513
.012
.712
.111
.510
.910
.410
.110
.010
.07.
001–
8.00
036
1412
.111
.911
.310
.710
.29.
79.
49.
39.
3
Rod
s,B
ars,
and
Sha
pes
SB
-221
5083
OU
pth
ru5.
000
3916
13.9
13.6
12.9
12.2
11.6
11.1
10.8
10.7
10.7
Sea
mle
ssE
xtru
ded
Tub
e
SB
-241
5083
OU
pth
ru5.
000
3916
13.9
13.6
12.9
12.2
11.6
11.1
10.8
10.7
10.7
Tab
leco
ntin
ues
onfo
llow
ing
page
293
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
Table ULT-23 2001 SECTION VIII — DIVISION 1
01
TA
BL
EU
LT
-23
MA
XIM
UM
AL
LO
WA
BL
ES
TR
ES
SV
AL
UE
SIN
TE
NS
ION
FO
R5%
,8%
,A
ND
9%N
ICK
EL
ST
EE
LS
,T
YP
E30
4S
TA
INL
ES
SS
TE
EL
,A
ND
5083
-OA
LU
MIN
UM
AL
LO
YA
TC
RY
OG
EN
ICT
EM
PE
RA
TU
RE
SF
OR
WE
LD
ED
AN
DN
ON
WE
LD
ED
CO
NS
TR
UC
TIO
N(C
ON
T’D
)
5%N
icke
lS
teel
s,S
IU
nits
8%an
d9%
Nic
kel
Ste
els,
SI
Uni
ts
Pla
tes:
SA
-645
2P
late
s:2
SA
-353
,S
A-5
53T
ype
I,an
dS
A-5
53T
ype
IIP
ipes
and
Tub
es:
SA
-333
Gra
de8
and
SA
-334
Gra
de8
For
ging
s:S
A-5
22W
elde
dC
onst
ruct
ion3,
4W
elde
dC
onst
ruct
ion3,
4
Non
wel
ded
Non
wel
ded
Tem
pera
ture
,1C
onst
ruct
ion,
UT
S68
9U
TS
655
Tem
pera
ture
,1C
onst
ruct
ion,
UT
S68
9U
TS
655
°CM
Pa
MP
aM
Pa
°CM
Pa
MP
aM
Pa
−19
626
023
422
3−
196
265
234
223
−18
423
822
921
8−
184
256
229
218
−15
622
321
920
9−
156
240
219
209
−12
921
721
120
1−
129
225
211
201
−10
120
820
219
2−
101
211
202
192
−73
199
194
184
−73
200
194
184
−46
189
187
178
−46
191
187
178
−18
163
163
163
−18
172
172
163
3816
316
316
338
172
172
163
Typ
e30
4S
tain
less
Ste
el,
SI
Uni
ts
Spe
cifi
edM
inim
umS
tren
gths
atR
oom
Tem
pera
ture
Max
imum
Allo
wab
leS
tres
s,M
Pa,
for
Tem
pera
ture
s,1
°C,
Not
Exc
eedi
ng
Spe
c.T
ensi
le,
Yie
ld,
No.
Gra
deM
Pa
MP
a−
196
−18
4−
156
−12
9−
101
−73
−46
−18
38
SA
-240
304
517
207
143
142
140
138
136
134
132
130
130
Tab
leco
ntin
ues
onfo
llow
ing
page
294
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
PART ULT — LOW TEMPERATURE VESSELS Table ULT-23
01
TA
BL
EU
LT
-23
MA
XIM
UM
AL
LO
WA
BL
ES
TR
ES
SV
AL
UE
SIN
TE
NS
ION
FO
R5%
,8%
,A
ND
9%N
ICK
EL
ST
EE
LS
,T
YP
E30
4S
TA
INL
ES
SS
TE
EL
,A
ND
5083
-OA
LU
MIN
UM
AL
LO
YA
TC
RY
OG
EN
ICT
EM
PE
RA
TU
RE
SF
OR
WE
LD
ED
AN
DN
ON
WE
LD
ED
CO
NS
TR
UC
TIO
N(C
ON
T’D
)
5083
-OA
lum
inum
Allo
y,S
IU
nits
Spe
cifi
edM
inim
umS
tren
gths
atR
oom
Tem
pera
ture
Max
imum
Allo
wab
leS
tres
s,M
Pa,
for
Met
alT
empe
ratu
re,1
°C,
Not
Exc
eedi
ng
Spe
c.T
ensi
le,
Yie
ld,
No.
Allo
yT
empe
rT
hick
ness
,m
mM
Pa
MP
a−
196
−18
4−
156
−12
9−
101
−73
−46
−18
38
She
etan
dP
late
SB
-209
5083
O1.
30–3
8.10
276
124
9291
8376
7270
6969
6938
.13–
76.2
026
911
787
8681
7470
6868
6767
76.2
3–12
7.00
262
110
8281
7972
6866
6666
6612
7.03
–177
.80
255
103
7776
7470
6665
6463
6317
7.83
–203
.20
248
9772
7169
6764
6362
6262
Rod
s,B
ars,
and
Sha
pes
SB
-221
5083
OU
pth
ru12
7.00
269
110
8281
7974
7068
6867
67
Sea
mle
ssE
xtru
ded
Tub
e
SB
-241
5083
OU
pth
ru12
7.00
269
110
8281
7974
7068
6867
67
NO
TE
S:
(1)
Str
ess
valu
esat
inte
rmed
iate
tem
pera
ture
sm
aybe
inte
rpol
ated
.(2
)M
inim
umth
ickn
ess
afte
rfo
rmin
gan
yse
ctio
nsu
bjec
tto
pres
sure
shal
lbe
3 ⁄ 16in
.(4
.8m
m),
and
max
imum
thic
knes
sof
the
base
met
alat
wel
dssh
all
be2
in.
(51
mm
).(3
)T
hem
inim
umte
nsile
stre
ngth
ofth
ere
duce
dte
nsio
nsp
ecim
enin
acco
rdan
cew
ith
QW
-462
.1sh
all
not
bele
ssth
an10
0ks
i(6
89M
Pa)
or95
ksi
(655
MP
a),
resp
ecti
vely
,at
room
tem
pera
ture
.C
hoic
eof
UT
Sde
pend
son
wel
ding
proc
ess
and
fille
rm
etal
used
inth
eco
nstr
ucti
on.
(4)
Wel
ded
cons
truc
tion
allo
wab
lest
ress
esap
ply
only
tobu
ttjo
ints
.
295
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
ULT-28 2001 SECTION VIII — DIVISION 1 ULT-82
the applicable figures in Subpart 3 of Section II, PartD at 100°F (38°C).
(b) Examples illustrating the use of the charts in thefigures for the design of vessels under external pressureare given in Appendix L.
ULT-29 STIFFENING RINGS FOR SHELLSUNDER EXTERNAL PRESSURE
Rules covering the design of stiffening rings aregiven in UG-29. The design shall be based on theappropriate chart in Subpart 3 of Section II, Part Dfor the material used in the ring at 100°F (38°C).
ULT-30 STRUCTURAL ATTACHMENTS
(a) See ULT-5(g) for limitations on material usedin permanent structural attachments in 5%, 8%, or 9%nickel steel vessels. See ULT-5(g) for limitations onmaterial used in permanent structural attachments inType 304 stainless steel vessels.
(b) The structural details of supporting lugs, rings,saddles, straps, and other types of supports shall begiven special design consideration to minimize localstresses in attachment areas.
(c) Attachments to 5%, 8%, or 9% nickel steelvessels shall be made using a weld procedure qualifiedto Section IX.
(d) Attachments to Type 304 stainless steel vesselsshall be made using a weld procedure meeting ULT-82.
ULT-56 POSTWELD HEAT TREATMENT
(a) For 5%, 8%, or 9% nickel steels, the provisionsof UHT-56, UHT-80, and UHT-81 apply.
(b) For 5083 aluminum, the provisions of UNF-56apply.
(c) For Type 304 stainless steel vessels, the provi-sions of UHA-32 apply
ULT-57 EXAMINATION
(a) All butt joints shall be examined by 100% radiog-raphy, except as permitted in UW-11(a)(7).
(b) All attachment welds, and all welded joints sub-ject to pressure not examined by radiography or ultra-sonic testing, shall be given a liquid penetrant examina-tion either before or after hydrotest. Relevant indicationsare those which result from imperfections. Any relevant
296
linear indication greater than1⁄16 in. (1.6 mm) shall berepaired or removed.
When a pneumatic test is required by ULT-99(b),these liquid penetrant examinations shall be performedprior to pneumatic test.
(c) For 5083 aluminum, the requirements of UNF-91 apply.
FABRICATION
ULT-75 GENERAL
The rules in the following paragraphs apply spe-cifically to the fabrication of pressure vessels and vesselparts that are constructed to this Part and shall be usedin conjunction with the requirements for fabrication inSubsection A and Part UW of Subsection B.
ULT-79 FORMING SHELL SECTIONS ANDHEADS
The requirements and limitations of UNF-77 applyfor 5083 aluminum, and of UHT-79 for 5%, 8%, or9% nickel steel.
ULT-82 WELDING
(a) A separate welding procedure qualification shallbe made, as prescribed in Section IX, Part QW, exceptthat the procedure qualification tests on tension speci-mens conforming to QW-462.1 and prescribed in QW-451 shall be four in number, two of which when testedat room temperature shall meet the minimum tensilestrength requirements for room temperature as listedin Table ULT-82 and two of which when tested at orbelow the vessel minimum allowable temperature shallmeet the minimum tensile strength requirements forthat test temperature as listed in the applicable table,except that the requirements for the two tests at vesselminimum allowable temperature shall not be appliedto procedure qualification for 5083 aluminum weldedwith 5183 aluminum filler metal.
(b) For 5%, 8%, or 9% nickel steels, the provisionsof UHT-82, UHT-83, UHT-84, and UHT-85 apply.
(c) For Type 304 stainless steel vessels, the followingprovisions apply.
(1) The welding processes that may be used arelimited to gas metal arc, gas tungsten arc, and sub-merged arc.
(2) Filler metal is limited to SFA-5.9, AWS Classi-fications ER308L and ER308L(Si). The filler metal
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
PART ULT — LOW TEMPERATURE VESSELS Table ULT-82
TA
BL
EU
LT
-82
MIN
IMU
MT
EN
SIL
ES
TR
EN
GT
HR
EQ
UIR
EM
EN
TS
FO
RW
EL
DIN
GP
RO
CE
DU
RE
QU
AL
IFIC
AT
ION
TE
ST
SO
NT
EN
SIO
NS
PE
CIM
EN
SC
ON
FO
RM
ING
TO
QW
-462
.1
SA
-353
,S
A-5
53T
ypes
Ian
dII
,S
A-3
33G
rade
8,S
A-6
45,
SA
-334
,S
A-5
22,
Cus
tom
ary
Uni
tsC
usto
mar
yU
nits
5083
-OA
lum
inum
Allo
y,C
usto
mar
yU
nits
Wel
ded
Con
stru
ctio
nW
elde
dC
onst
ruct
ion
Min
imum
Ten
sile
Str
engt
h,ks
i,fo
rM
etal
Tem
pera
ture
,1°F
,N
otE
xcee
ding
Tem
p.,1
Spe
c.°F
UT
S10
0ks
iU
TS
95ks
iU
TS
100
ksi
UT
S95
ksi
No.
Thi
ckne
ss,
in.
−32
0−
300
−25
0−
200
−15
0−
100
−50
010
0
−32
013
612
913
612
9S
heet
and
Pla
te−
300
133
126
133
126
−25
012
512
112
512
1S
B-2
090.
051–
1.50
055
.253
.348
.243
.841
.440
.440
4040
1.50
1–3.
000
53.8
5247
42.7
40.4
39.4
39.1
3939
−20
012
211
612
211
63.
001–
5.00
052
.550
.745
.841
.639
.438
.438
.138
38−
150
117
111
117
111
5.00
1–7.
000
51.1
49.3
44.6
40.5
38.3
37.4
37.1
3737
−10
011
210
711
210
77.
001–
8.00
049
.748
43.4
39.4
37.3
36.4
36.1
3636
−50
108
103
108
103
095
9510
095
Rod
s,B
ars,
and
Sha
pes
100
9595
100
95S
B-2
21U
pth
ru5.
000
53.8
5247
42.7
40.4
39.4
39.1
3939
Sea
mle
ssE
xtru
ded
Tub
e
SB
-241
Up
thru
5.00
053
.852
4742
.740
.439
.439
.139
39
Typ
e30
4S
tain
less
Ste
el,
Cus
tom
ary
Uni
ts
Min
imum
Ten
sile
Str
engt
h,ks
i,fo
rM
etal
Tem
pera
ture
,1°F
,N
otE
xcee
ding
Spe
c.N
o.−
320
−30
0−
250
−20
0−
150
−10
0−
500
100
SA
-240
82.7
82.1
80.9
79.7
78.5
77.4
76.2
75.0
75.0
Tab
leco
ntin
ues
onfo
llow
ing
page
297
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
Table ULT-82 2001 SECTION VIII — DIVISION 1
TA
BL
EU
LT
-82
MIN
IMU
MT
EN
SIL
ES
TR
EN
GT
HR
EQ
UIR
EM
EN
TS
FO
RW
EL
DIN
GP
RO
CE
DU
RE
QU
AL
IFIC
AT
ION
TE
ST
SO
NT
EN
SIO
NS
PE
CIM
EN
SC
ON
FO
RM
ING
TO
QW
-462
.1(C
ON
T’D
)
SA
-353
,S
A-5
53T
ypes
Ian
dII
,S
A-3
33G
rade
8,S
A-6
45,
SA
-334
,S
A-5
22,
SI
Uni
tsS
IU
nits
5083
-OA
lum
inum
Allo
y,S
IU
nits
Wel
ded
Con
stru
ctio
nW
elde
dC
onst
ruct
ion
Min
imum
Ten
sile
Str
engt
h,M
Pa,
for
Met
alT
empe
ratu
re,1
°C,
Not
Exc
eedi
ng
Tem
p.,1
UT
S68
9U
TS
655
UT
S68
9U
TS
655
Spe
c.°C
MP
aM
Pa
MP
aM
Pa
No.
Thi
ckne
ss,
mm
−19
6−
184
−15
6−
129
−10
1−
73−
46−
1838
−19
693
888
993
888
9S
heet
and
Pla
te−
184
917
869
917
869
−15
686
283
486
283
4S
B-2
091.
30–3
8.10
381
368
332
302
285
279
276
276
276
38.1
3–76
.20
371
359
324
294
279
272
270
269
269
−12
984
180
084
180
076
.23–
127.
0036
235
031
628
727
226
526
326
226
2−
101
807
765
807
765
127.
03–1
77.8
035
234
030
827
926
425
825
625
525
5−
7377
273
877
273
817
7.83
–203
.20
343
331
299
272
257
251
249
248
248
−46
745
710
745
710
−18
655
655
689
655
Rod
s,B
ars,
and
Sha
pes
3865
565
568
965
5S
B-2
21U
pth
ru12
7.00
371
358
324
294
279
272
270
269
269
Sea
mle
ssE
xtru
ded
Tub
e
SB
-241
Up
thru
127.
0037
135
832
429
427
927
227
026
926
9
Typ
e30
4S
tain
less
Ste
el,
SI
Uni
ts
Min
imum
Ten
sile
Str
engt
h,M
Pa,
for
Met
alT
empe
ratu
re,1
°C,
Not
Exc
eedi
ng
Spe
c.N
o.−
196
−18
4−
156
−12
9−
101
−73
−46
−18
38
SA
-240
570
566
558
550
541
534
525
517
517
NO
TE
:(1
)S
tren
gth
valu
esat
inte
rmed
iate
tem
pera
ture
sm
aybe
inte
rpol
ated
.
298
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
01
ULT-82 PART ULT — LOW TEMPERATURE VESSELS ULT-115
shall conform to the SFA specified percentage composi-tion limits.
(3) A determination of delta ferrite of each lot offiller metal shall be made by the use of the chemicalanalysis from (c)(2) above, in conjunction with Fig.ULT-82. Additionally, for submerged arc welds, adetermination of delta ferrite shall be made in conjunc-tion with Fig. ULT-82, by the use of the chemicalanalysis of lots of electrode and flux used for productionwelds. The acceptable delta ferrite shall not be lessthan 6 FN nor greater than 14 FN.
ULT-86 MARKING ON PLATE ANDOTHER MATERIALS
For 5%, 8%, or 9% nickel steel the requirements ofUHT-86 apply. For the use of other markings in lieuof stamping, see UG-77(b).
INSPECTION AND TESTS
ULT-90 GENERAL
The provisions for inspection and testing in Subsec-tions A and B shall apply to vessels and vessel partsconstructed of materials covered by this Part, exceptas modified herein.
ULT-99 PRESSURE TEST
The vessel shall be hydrostatically pressure tested atambient temperature in the operating position for aminimum of 15 min, using the following requirementsof (a) or (b), whichever is applicable.
(a) Except for vessels covered by (b) below, a hydro-static test shall be performed in accordance with UG-99, except that the ratio of stresses is not applied, andthe test pressure shall be at least 1.4 times the designpressure at 100°F (38°C).
(b) When the test procedure in (a) above will causea nominal membrane stress greater than 95% of specifiedminimum yield strength or 50% of specified minimumtensile strength of the material in any part of the vessel,the hydrostatic test may be conducted at a pressurethat limits the nominal membrane stress at such partto the lesser of those values. When these conditionslimit the hydrostatic test pressure to a value less than110% of the maximum allowable working pressure at100°F (38°C), a pneumatic test in accordance withUG-100 shall also be conducted, except that the ratioof stresses is not applied.
299
(c) Vessels which are to be installed in the verticalposition may be tested in the horizontal position pro-vided all components of the vessel are hydrostaticallytested for a minimum of 15 min at a pressure not lessthan 1.4 times the design pressure at 100°F (38°C)plus the equivalent of the head of the test liquid inthe operating position.
MARKING AND REPORTS
ULT-115 GENERAL
The provisions for marking and reports in UG-115through UG-120 shall apply to vessels constructed tothis Part, with the following supplements to the markingand Manufacturer’s Data Reports:
(a) The vessel markings shall be in accordance withUG-116 except:
(1) the letters ULT shall be applied below the USymbol;
(2) the following markings shall be used insteadof those in UG-116(a)(3) and UG-116(b)(1)(a):
Maximum Allowable Working Pressure: psi at 100°FMinimum Allowable Temperature: Minus °F
Service Restricted to Operatingthe Following Temperature
Liquid Minus °FLiquid Minus °FLiquid Minus °FLiquid Minus °F
NOTES APPLICABLE TO MARKINGS:(1) Minimum allowable temperature is the temperature of the
coldest cryogenic liquid which will be admitted to or stored withinthe vessel.
(2) Operating temperature for the cryogenic liquid is its saturationtemperature at MAWP. All liquids that may be contained in thevessel shall be listed.
(b) On the Manufacturer’s Data Report, under Re-marks, show the additional marking notations from (a)above.
(c) Unless the requirements of (c)(1) and (2) beloware met, for 5%, 8%, and 9% nickel steels, the useof nameplates is mandatory for shell thicknesses below1⁄2 in. (13 mm); nameplates are preferred in all thick-nesses.
(1) The materials shall be limited to aluminum asfollows: SB-209 Alloys 3003, 5083, 5454, and 6061;SB-241 Alloys 3003, 5083, 5086, 5454, 6061, and6063; and SB-247 Alloys 3003, 5083, and 6061.
(2) The minimum nominal plate thickness shallbe 0.249 in. (6.32 mm), or the minimum nominal pipethickness shall be 0.133 in. (3.38 mm).
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
Fig. ULT-82 2001 SECTION VIII — DIVISION 1
FIG
.U
LT
-82
WE
LD
ME
TA
LD
EL
TA
FE
RR
ITE
CO
NT
EN
T
300
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services
ULT-125 PART ULT — LOW TEMPERATURE VESSELS ULT-125
PRESSURE RELIEF DEVICES
ULT-125 GENERAL
The provisions of UG-125 through UG-136 shallapply to vessels constructed to this Part; the vesselshall be equipped with a safety relief valve suitablefor low temperature service and installed to remain atambient temperature except when relieving.
301
COPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling ServicesCOPYRIGHT American Society of Mechanical EngineersLicensed by Information Handling Services