I" Kecord
DNE CALCULATIONS
-
TITLE-
I
flRUANII7ATINA
PRFPARiIN-
Bechtel Job
'
I
20652
47SA
c
R
RSEL R_
M(S)
sC 0033
__R
_6_73_/__O?
-I
-
I
17 1R
-
P-05711-
--
P-05711-A
/a°
___
.-
s
.. i
-
.
iq,4
Prepared
, ..
I
.
-~.
'B 2 0 4I13
..
3 o2
4
0
--B18 Woo , 90 0314 0 8 5 B-18 '90 050 1 080 B18 '90 0703 00P4 .
.-
barety -related ?
-
Yes
g
No U
Document design calculations
for pipe support referenced in calculations title.
. -
Reviewed
T
Approved
TV!)
3
-
-q
) SEE I
List all pages deleted bv this revision.
.
.I-
-
|~e- L)
List all pages changed by this revision.
These calculations contain unverified assumption(s)
4f~t
2..-2.4^°l ° Ar? s
12
List all pages added r- by this revision.
-J
Yes 0 No S
--
'~f
OR1ONiAL
_
ze
L6C
Yes S No D
Yesz|
No 0
Yes O
No ED
Abstract
This calculation verifies the structural adequacy of the subject pipe support.
Legibil ity evaluated and 8Wc peydfor , 9305280306 930522 PDR ADOCK 05000390 A PDR
p C
..
Statement of Problem --
Checked
-
o
N/A
ECN No. (or indicate Not Applicable)
-
r
0
UNIDDSYSTES
or DCN No.
S
6S
bIWc
RevisionO
1 *n
2
WB-DC-40-31.9
3.9
r,
r;,;1
Uarcb
O ±'O27co 2
8
RO
APPLICABLE DESIGN DOCUMENT(S)
SAR SECTION(S)
._
trr
I WBNW /TTh1
-rrr^ * ^~ssi= ^ L lv L-:a I 1711 1 A n Ench time thes calculations are issud. preparers must ensure that the original (RO) RIMS accession number Is filled in. Rev (for RIMS' use) RIMS accession number
70l. 7, 0 /1._
PLANT/UNIT
KEY NOUNS (Consult RIMS DESCRIPTORS LIST) Pie nO
/ BRANCH/PROJECT IDENTIFIERS
Date
.
System: 7+ Calculations for Pipe Support: 4-7A437/ - 7
Signature
Microfilm and store calculations in RIMS Service Center.
Microfilm and return calculations to: M7.th =: RIMS, SL 26 C-K 0
1/5/90
aUe
:J, -
OOR TL FLOOR DOC. CON(i
7t
H
Microfilm and destroy.
C /i-/
Address:
L-L.t-
VI
.d"
2U reOjZ1r
EN DES CALCULATIONS:-
CAL C5-
FORz
UNID SYSTEM(S)
ING ORGANIZATION
X-W
5tcy
APPLICABLE DESIGN DOCUMEN'TS
LO&-tp-
4-0-
I
Ac//. #4 BRANCH/PROJECT IDENTIFIERS
to)wm~3 ,0o
RO I
'
(FOR MEDS USE)
82 042 8E O065 ' * %
7F137PoJoo?
FoRl Llt
PIPE 5$c9-r
CALC5
rEOr A 60ovI
II.
fO -4-A4351 1---I- (Q l,3 FoL)u4
10697 (ENDES-7-78)
*Use revisjon log (form TVA 1
To
afe
Ac;rQvA-re
if more room is required .
REVISIO NLOG SYSTEM: 74 Title: CALCULATIONS FOR PIPE SUPPORT:
Sheet Ni0.
47A37olo67
1
DESCRIPTION OF REVISION
Revision No.
SUPPORT REQUALIFIED PER HAAUP
,/ - 4t-
Iu
I CALCULATION REPLACED IN ITS ENTIRETY
NAME (PRINT)
A NI-
~\.
-- AU MI .
j,&I
I
I
2
1
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MC-HIA
____
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11
/ SIGNATURE
57aK'
b ,~f-gTA
I
4.1
;Sfi-
NAME (PRINT)
IcUamF-2
TVA 10534 (EN DES-4-78)
AlA2
Ht-1.
I
_7IA,
M ftki6PALLJLATIW SUPPORTs tx, __3 kEVISED §NTS HiMi __ r-PLACE-D
4,9
N UP A
RGOUALIFIELD PEPR
.
INMALS
/ SIGNATURE
•OPPc'RT
r
,a
A
O
V "<".'kA I
;J*'I*
It G
0^/
Rev- O - o F
.
7-0 571/-,
THIS CALCULATION SUPPORTS DCN #
__
/
INITIALS
/
C4--
/ -f . -tTr /
C
/
'_
_
_
_
/__
.1
mom a
.
SYSTEM: i4 CALCULATIONS FOR-PIPE SUPPORT:
ITitle:
24_~
//w4g7
7
/
REVISION LOG Sheet No.
DESCRIPTION OF REVISION
oRevison
i.
Approved
SUPPORT REQUALIFIED PER HAAUP ADDED:________
at
f
Awe
/2AA/'
'"
AT74M,V
-JT4>J}g>
DELETED:
P-c57n /I
THIS CALCULATION SUPPORTS DCN#
..4S
/ INIALS
/ SIGNATURE
NAME .PRINT)
S4/41-1I
/
/
_
_
_
_
_
/
VP . (EN
IVA
OES1Q34G.7B)
10534 (EN DES-4 78)
_
_
_
/ ____
/
-
-2/ -6/e
A,
CALCULATION SHEET
JOBND
-N)
F-0
-
C.ALC,. NU.
20652
REV. NO.SHEET NO
4-74-437ol oo7
ORIGINATOR
DATE /23/"94
CHECKED o
DATE 5
P2
1 2
R
ORIGIATOR
DATE
4
3 4
SECTION
II
CHECKER DATE
J
/A
6'A ?1
N
0
REV.
-
I
a I I ~ O. ORIGINATOR DATE
I
CHECKER
'1.
DESCRIPTION
5
2 /24/V
-
DA
C2, SHEET NO.
Cover Sheet
.6
Revision Sheets
7
iL
Table of Contents
8 9
-
1.0
Purpose
1
1.1
Assumptions
1
12
1.2
Sources of Data/References
2-3
13
1.3
Calculations
3-
1.4
Conclusion
11'
3
iiL
4,4.17,OI5D
14
17 is
ATTACHMENT NO. -
19
_______
DESCRIPTION
SHEET NO.
A
Load Data Sheets
B
Pipe Support Configuration Data
A/1-
4-112-14513-
20
Unverified Calculation Assumption Form
21
,q/
22
HAAUP Open Item Transmittal
23 24 25
e-
civai
"lc/C/.
F, pps
o11
RE-QPUCr7 77 -
26
1 IAP
27
/I/
2B
rm
M,9F,.
s-o)
-I
-/
z
F1-F/0
o U7P4'
C(?R g/dP-RO63
F// -
Io
30 31 32
34 35 36
NOTE:
Total numbers of sheets in this calculation to be microfilmed including attachments -7 G 5 57. I
a&.VW Rw.
Wi
.e
I
.
I
CALCULATION SHEET ,EC20
.E
JOB NO.
SEP.27O ./A
CALC. NO.
ORIGINATOR
DATE
SHEET NO.
7 CHECKED
M
.A..
/ Rev
REV. NO.
47A 43 7
20652 *
-
h-4r
DATE
e
2
3
SECTION 1.0: PURPOSE
4
The purpose of this calculation is to establish the adequacy of the pipe support configuration at the Watts Bar Project per current design requirements.
6 7 8 9 10
SECTION 1.1:
ASSUMPTIONS
12
Assumptions are as noted below and/or as noted in the body of the 13
calculation.
14
17
18
1.
Coefficient of friction (i) = 0.3 (steel on steel)
2.
Concrete strength (f'c) = 3000 PSI (UNO)
3.
All carbon steel items (including tube) material properties are as follows: Yield stress of steel: Fy = 36.0 KSI (UNO)
19A.
20 21
B.
22
23 24 25 26 27 28 29 30 31
34 35 -36
C.
Modulus of elasticity of steel: E = 29,000 KSI (UNO) Shear modulus of elasticity of steel:
G
=
11,000 KSI (UNO)
(UNO)
{ .00006
NNATOR I DATE F CH-ECKER IDATE 1
Ji~~iRiG
CALCULATION SHH[ l
er n a JOB NU.
CALC. NO.
4-7A41-27
l90652 T
RIGINA OR
W
2
3
)
REV. NO.
SHEET NO.
0107
DATE
2
CHECKED
DATE
of a r / SqVlk
SECTION 1.2 SOURCES OF DJA.TA/REFERENCES
_R.
ORIGINATOR
0.
I
1
DATECHECKER DATE
X
1.
Load data sheets per Attachmint
X
2.
Pipe Support configuration data per attachment B.
X
3.
Piping Analysis Caic. No. Jt. No. L 15
X
4.
WB-DC-40-31.9, Rev. 10, "Criteria for Design of Piping Supports and Supplemental Steel in Category I Structures".
X
5.
WBEP 5.40, Rev. 3, and 5.40C, Rev. 0, "Procedure for Design of Supports for Category I Piping".
12
X
6.
Watts Bar Pipe Support Design Manual, Vol. 1 & 2, Rev. .. l\2
13
X
7.
Pipe Support Load Capacity Data Sheets Manual Revision 2. (RIMS No. B26 '89 1228 103)
/
8.
TVA Civil Design Standard DS-C1.7.1, Rev. 4, "General Anchorage to Concrete".
/_
9.
TVA General Construction Spec.
5 6
7 8 9 10 11
14
17 18
\J2
l
A-.
4
2-
-
024
G-32, Rev.
5/
,
13,
o
Rev.____
"Bolt Anchors
Set in Hardened Concrete".
19
X
10.
TVA Specific construction Spec. N3C-912, Rev. 5, "Support and Installation of Piping Systems in Category I Structures".
8/A
11.
Civil Design Standard DS-Cl.6.14, Rev. 0, "Design of Unistrut and B-Line Clamps for Piping and Tubing."
X
12.
AISC Manual, 7th Edition, Feb. 1969 with Supplements 1, 2, and 3.
X
13.
AISC Manual, 8th Edition, properties only).
N/A
14.
47A053-10 Pipe Strap Calculation Rev. 3 (RIMS No. B41 '88 0427 803).
/A
15.
AWS D1.1-81.
X-
16.
Blodgett, "Design of Welded Structures", 1966.
/
17.
WBEP 5.55C,
20 21 22
23 24 25 26 27 28
(for member dimensions and
29 30 31
Rev.01,"'Reconciliation of HAAUP Walkdown Data".
'34 35 36 GA-2706 Rev. 9189
.4
1
CALCULATION SHEET
I JOb -D liy NO.
-
20652
- A.
CAL;. NO.
REV. NO.
474 437olo07 rv^sr
ADIDlKlATnD UOHIUINA I UK
I
.
t1-
t-A
DATE
i
2 - 2'
.
I
3-I
'--I
/ CHECKED
DATE
I
I
SHEET NO.
-
2/12 4/,?o
2/2 q/
SECTION 1.2: 2 3
X
18.
C!omputer
4
-
5
5<
6
Programs
BASEPLATE II, Version
IAP, Version
I
;I I L>4
ORIGNATOR
CONAN, Version
7
B8
%
-
ME150, FAPPS, Version
'DATE
CCKER DA E
S.v4z;
q
9
ME035, BASEPLATE, Version
-
10 -
I11
Other (Specify)
12 13
14
2K
19.
QIR CEB-WBN-88-002 R4 (RIMS No. B26 89 0922 101) Building Seismic Response Spectra and DBA Spectra for PAID Documents
17
,>
20.
Qualification for Use of E70 Electrode for Welds at WBNP (Ref. RIMS No. B26 881109021)
N/A
21.
Civil Design Guide, DG-C1.6.10, Rev. 0, "Design of Steel Members for Local Stresses".
N/4
22.
Civil Pipe Support Calculation N3-PS-002, Analysis for Concrete Bearing Stress check. RIMS # B26'89 0913 153
X
23.
QIR-CEB-WBN-89- 25
I/A
24.
Other
18 19 20 21 22 23 24 25 26 27 28 29 30 31
TIITT.ArTnS ~.-
SECTTON 13! -------
-.---.
/
"Footprint Load Transmittal"
(foIlf ,
Irows)
Based on a review of DCDTS, report #6140, dated -L-e Ye -, are there any open documents (ECN, DCN, etc.) applicable to this calculation? Yes X (See heet for listing) No NMvPei.5/44,, ,o hOAer -O deeps r 44Le.
3
Are there any non-generic HAAUP Open Items (i.e., CAQR's, PIR's, NCR's, SCN's, SCR's) against this support? (Exclude Construction Open Items) -
Yes
(See next sheet for listing)
X No 34
35
Note: For the resolution of generic open documents associated with the HAAUP program and related stress problem, see Block #8 of the DCN package cover sheet. GA-2706 Rev. 9/£
'Owtn
CALCULATION SHEET
Section 1.3:
(continued)
2 3
STRESS ANALYSIS LOADS AND MOVEMENTS:
4
* FORCES
(LBS)
DIR
5
NORMAL
10
UPSET
EMERG.
6
xX+
7
(* REF. NO.
1)
CALC DESIGN *MOVEMENTS (IN) LOADS (LBS) FAULTED THER MAX
\/
°12
a
_____ _
9
Y
10
~~~~0+__
-(OYrl A//Id -
-__
__
-17 29/-q
I11
-~
6
-
2
7
so1o383
3
I
c Og27
z
13
B
oJ 0o 8o)
+
12
o 293
-~~~
----
0030 jO.30°
14
17 18
;
77-/lf
COMMENTS:
CONSIDER FRICTION LOADING:
A
's Wv00O
(REF#_4 )
-YES
(SEE BELOW)
V-N/A (
S
19 20 21
CONIDR .WE.(REF#j15):
22 23
I X = m-£7 ' Based on
= Lh
y
/-
73
Z
YES 2
=
67
Peak Acceleration
24
(SEE BELOW) Acu, if Tab
-
NO
(SEE COMMENTS)
8+2 Fat Jcrcc~'i. Actual Accelerationl Fi.
pSO
dDt-
BLD>) {
25
CHECK GAPS
(REF.
#
10
):
-YES
26
(SEE BELOW)
'-~N/A
( 3P~o/A4'A4 fc
t
)e
DOES TOTAL GAP IN ANY RESTRAINED DIRECTION EXCEED N3C-912 REQUIREMENTS - YES (SEE COMMENTS BELOW) -- NO (THEREFORE OK)
27 28 29
CALCULATION ANALYSIS APPROACH
30
(SEE BELOW):
NAiPPLICABLE
-N/A
I 31 32
FAULTED LOADS OR LOADS GREATER THAN FAULTED LOADS WILL BE USED WITH NORMAL CONDITION ALLOWABLES (CONSERVATIVE) UNLESS OTHERWISE NOTED. COMMENTS:
I
35 .
36
I GA-2706 P.". 9189
2
SUPPORT LOAD COMPARISON SHEET The purpose of this sheet-is to document the acceptance of previously performed calc's (per attached sheets) based on revised loads.
3 4
A.
LOAD COMPARISON BETWEEN
5
6 7
RESTR. TYPE & DIR.
OPER. COND.
DESIGN REVISE LOAD LOAD (LB) (LB)
8
i
10
sNOW
W AraX AS oL D
UPSET
11
REMARK
-I29 -oI7M
NORM.
9
LOAD RATIO (REV/DES)
//
FAULT
12
' fgov
- .Oi'(6L1Do
bj
M/
NORM. 13
,
\
UPSET
iA
FAULT NORM. 17 18
UPSET
19
FAULT
20
Results:
21
ev
Load Increase (Continuation Sht. Req'd.) Load Decrease (OK)
22
B.
MOVEMENT EVALUATION FOR REVISED HANGER MOVEMENT.
23 24
1. FRICTION -_
Not Applicable Applicable (Explain)
25 26
2.
GAPS
3.
SWING ANGLE
4.
SPRINGS/SNUBBER SETTINGS
_d
Acceptable
Not Applicable
27 28 29
-
Not Applicable
Acceptable
/
30 31
34 35 36
Not Applicable
Y
Acceptable
Revision It of the stress hanger guidance REVIEW/COMPARISON RESULT: Previous pipe support has been reviewed and found to be acceptable. calculation as shown on succeeding sheets need not be revised to incorporate the revised loads and movements since sufficient margins exist.
CALCULATION SHEET
SECTION 1.3:
2
VariaTbl 6Spr
Lo&Z CltVCB 9uAL3Pn
11_3 4
t
(Continued) fRi
8sdoepi Ig) 8 S912,& (Nve74 t-yff)
Variable Spring Calculation (Based on one Spring)
I5
Spring Part No
6
Design Load (DL) 8 , Lower Component Weight (WL) = -Max. Movement (AMax.)'= + fo23in.,-o_117, Thermal Movement(Mvt.)= tr267in. Spring Working Range .5 7 # To as3 # - 0 C4
7 B
V i-5
Spring Total Range
, Size-_j
43 4- # To
Spring Rate(K) =
X/in.,
3 08
#
/ol,
9
10 11
When Mvt. is up:
_- Applicable
-
Not Applicable p-
Check Spring Working Range:
12
Hot Load (HL) = DL + WL 89 ' o lbs. Cold Load (CL) = HL + (K x Mvt.) = 9//
13
Check Spring Total Range (Top-Out or Bottom-Out): Max.- Load = CL -[K x (A Max)] = Min. Load = CL -[K x (+ A Max)] =
16
When Mvt. is down:
17
-
sD-c TvP.
CoLD -rE7'r7i/'a
0o3
cCL..
is!.
*i
U'D/o/
lbs. .
v- Appllicable
- Not Applicable
Check Spring Working Range:
19
Hot Load (HL) = DL + WL = _ a _ I Cold Load (CL) = HL - (K x Mvt.) =
lbs. 834
Max. Load = CL -[K x (A Max))= Min. Load = CL -[K x (+. L Max)]=
'Si 39
21
4'/
lbs.
18
20
lbs.
-_ -2 558 -
R F-F
CHA-PI6F6
/fqt C-0/ F- ;
V
-
lbs. Check Spring Total Range (Top-Out or Bottom-Out):
C -( .
-f 0 - - SD f
lo
= 2 - I °/e .
-- I
+ lbs.
5ss -lbs.
22 23
Check Spring Variability
24 25 26 27 28 29
Conclusion: Spring Variability < 25% Spring Within Working Range Spring Within Total Range
V Yes (OK) Yes (OK) -1fYes (OK)
30
'-
No (N.G.) No (See Below) A No (N.G.) I
31
Comments:
:
- CHj j CI)
MA)x. La,1 /) rY,i4.
A low
34 35 36
-
5rpzi.'Ui
-F /'"Wi/6 y
-Fk x -A
Lo
Ok/ZYV/? Cm-,1-Y p
mpax.U =
X+
•xc&E: ''X clz s
,tAhttE S
C-L
a8 /aIH/ F_ Lo,
2
/MIX ,Abt
-
=o3-F3Axo 1=C-L. I
o3z7
Avna
TOTAL AV/hLDA14A-R L
3S 1Lb 5
=5
2K
1oV6-E ,'.
W/1 La/-cc6
,-J1
4
.
"CALCULATION SHEET
d
A-
.
I
i
L.ALI.. N'.).
rsNU
1
474 -437
ORIGINATOR
IV
*EPC.270
I SHEET NO
/ oo 7 CHECKED
DATE
-2j - 9o
23 - /ue2 D)
REV. NO.
Pt". Of" (ED491
.
DATE
19rs /X
2124/90
1
2 SECTION 1.3:
(Continued)
at/ftgrlS171aw
5a'd"li WCT~r 5fP~id~
3
Variable Spring Calculation
4 S
(Based on one Spring)
Spring Part No VS / - A , Sizej9 Spring Rate(K) = 3o 8 #/in., Design Load (DL) 30 , Lower Component Weight (WL) = Max. Movement (A Max.) - + 1o33in.,-o.,i, Thermal Movement(Mvt.)=c267in. Spring Working Range s87 # To 953 # -O-D4 Spring Total Range 4 34 # To /o// #
6 7
a 9
When Mvt. is up:
10
I'WApplicable
11
Check Spring Working Range:
12
Hot Load (HL) -
83 o (K x Mvt.)
DL + WL
Cold Load (CL) - HL + *13
-
9/
lbs. 12
Not Applicable C c/ c.ot fJ77,V7 q i 2 - 7O X
lbs.
Check Spring Total Range (Top-Out or Bottom-Out): Max. Load = CL -[K x (Min. Load = CL -[K x (+
AMax)]= A Max)) =
q7 sS8
lbs. lbs.
,
i7.
°:°
to
C-.
ok
16
When Mvt. is down:
_jApplicable
17
-
Not Applicable
Check Spring Working Range: Hot Load (HL) DL + WL = 8 3 lbs. Cold Load (CL) = HL - (K x Mvt.) = 3/5 lbs. Check Spring Total Range (Top-Out or Bottom-Out): Max. Load - CL -tK x (a Max)]= lbs. Min. Load - CL -tK x (+ A Max))58 _ lbs.
18 l9 20
e c8A/6 iA c. 3- 8159o7 3 i,-C'f L67J /lf4A/U%
__3___
21
ur6
xif-r
cf.
22
23
Check Spring Variability
24 25
Variability =
Mvt. HL
26 27
27x3
(K)
x100
8
Conclusion: Spring Variability < 25% - Yes (OK) Spring Within Working Range. Yes (OK) Spring Within Total Range -__ Yes (OK)
28 29
No (N.G.)
-No (See Below) No (N.G.)
30
comments:
:31
5S 6 Ar
>16
SE
CAc c:
b/,/;
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r
Sh
A-ar 7
'
1201
A
34 -c
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t f- 11e
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7
.
P U F
-T D
. I.-
j7- LI t
-
h
-
_ir j5
VF
rN/ ' 1v/I 7
SiC-C
101,04h, eg
"CALCULATION SHEET
JOB NO.
i 2 o652
47A 437o/ o°7
ORIGINATOR
I 1
REV. NO.
CALC. NO. DATE
/
1/~ 4fJV
1./
CHECKED
.2 -22 - 10
SHEET NO.
22
AYfA./A
IM-
7 DATE
4/ 0o
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- - / 3.(CONiK -.. )
Sec7/ o
2 3
.- .
.
.
- .
-...
tYL.
4 5 6
SlI/
7 '.1) CoSv)
8 9
-zV, iV I
3
I
10 11
29. 44''
12 13
LE G.END; *
A 16 17
CoI
Tor,q7.
-
-4---
- mcme-cA
OI-
PAP T
0-
5sc -rior/AL
18 19
rFPPS
144f/
MobE-L.
20 21
I- 2
M cme E-<
22
4-X 4x Y 4
T-5
TS 3
3
x3 V
23
Tw' T° W
24
rDrJC D C-7N 1 CAI
A S B 0 77/
25
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Frkqer M
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SHEET
CALC. NO.
IORIGINATOR, 2oc-'~;.
REV. NO.
4 7,4437 0 1oo07 DATE CHECKED
SHEET NO.
DATE
2
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35 .35 GA-2706 Rev. 9/89
CALCULATION SHEET
MA -
V. I
JOB NO.
CALC. NO.
20652
47
ORIGINATOR
r
Z X
2
Section 1.3:
3
EVALUATE STD. COMPONENTS:
4
(UNITS - INCHES/LBS.)
6
ITEM NO.
PART NO.
7
'4
133A
SHEET NO.
DATE
|w.Sr^/ea/2+/S 0
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ORIGrNATOR
DATE
CHECKER
1 I~6/ rY/1o -S
DESCRIPTION gO D P
/
1810
DATE
/jg
6
OK/ NG REF#
DESIGN LOADS
ALLOWABLE LOADS NORMAL=
81
co.k
8
7
UPSET =
9
FAULTED =
10
NA
12 12
ITEM NO. 5
PART NO.
SIZE
DESCRIPTION Valt6
5/2 A
jY Y/-
ALLOWABLE LOADS
DESIGN LOADS
OK/ NG REF#
NORMAL -
oUl
A
UPSET =
16
FAULTED =
17 18 19
20
ITEM NO.
PART NO.
SIZE
DESCRIPTION
ALLOWABLE LOADS
DESIGN LOADS
OK/ NG REF#
21 22
G
~
-
NORMAL
23
|
=
4
UPSET=
--
24
14
FAULTED=
25
-
-
26 27 28
ITEM NO.
PART NO.
SIZE
DESCRIPTION
ALLOWABLE LOADS
DESIGN Y&DS-- NG
REF#
29 30
I IL
bl1
S
-------- UPSET=
I;
FAULTED 3 34 35
36
COMMENTS:
-e
4
-
Tht.i
(2
- r
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(ED49)
10
CHECKED
(Continued)
SIZE
5/"
I
4-3 70/1W7
2-23-. v
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REV. NO.
DATE
2
5
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CALCULATION SHEET JO NO.
CALC. NO.
wI20652
4-7A4k37 .61,00-
ORIGINATOR
DATE
f4-5 1
3
REV. NO.
I
CHECKED
SECTION 1.4
DATE
CONCLUSION
ORIGINATOR
DATE
5,C7g Based
1//
-g-vq-
/62
4
SHEET NO.
on the
detailed
pe frmi
calculations
for..+larrL2 -
CHECKER DATE
+
D
4
5
configuration shown on the design documents attached,
6
following has been concluded:
the
7
8
A. Support meets current criteria requirements
9
10 11 T
B. Support meets current criteria requirements with
12
proposed modification.
13
¶6 17 18
NOTE:
The following open item(s)
have been addressed in the
preceeding detailed calculation per WBEP 5.55C
19
(See Attachment #___). 20
21
i- S c Los&V.
02 - 0
1-7L - H91
22 23 24 25
-no
'/tCz
"'
elf~
4$-~Ad
Z64'~eg) '49
7?r'
26 27 28 29 30 31
34 35
GA-2706 R.v
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CALCULATION SHEET JNO.
CALC. NO.
REV. NO.
20652
- -7A447 2a
ORIGINATOR
DATE
/
SHEET NO.
3
CHECKED
DATE
ad 6. a/
2
Section 1.4
(Continued)
3 CONCLUSION' 4
5
This support calculation has loads and movements per rev. 6 (reference sheet. A.3 ). 7 for overall compliance with criteria with emphasis on the
been subsequently evaluated for the -iZ of the stress calculation The calculation has been reviewed the requirements of the applicable following key attributes:
8
9 10
Load
increase factor= A0
1.
Member stresses
2.
Deflection
13
3.
Weld stresses
14
4.
Anchor bolt loads
5.
Base plate stresses
1
6.
Standard component allowables and settings
18
7.
Piping attachments welds and local stresses
8.
All other applicable requirements of the criteria
12
°
A/
18
19
2
21 22 23
Based upon the above evaluation, the support meets the current criteria requirement. The documentation of the above evaluation has been issued with the rev. 12of the stress calculation.
24 25 26 27 28 29
30
34 35 36 GA-2706 Rev. 9189
CLASS ;T PROCESSOR PLANT : WATTS BAR PIPING S IEM : RHR SPRAY NODE NAME * L15 SUPPORT DIR . Y SUPPORT TYPE: VS DESIGN TRAVEL DESIGN TRAVEL (LUG DESIGN LOAD 1729 L
JSN = AOWL
LOAD CASE -----------------
)8.52.53.
UNIT' -NIT
PAGE
103
1
A SHEET I OF 2 ANALYSIS PROBLEM ISOMETRIC DRAWING :: N3-74-02A B-47W432-205 SHT 2 REV RO SUPPORT ID : 47A437-1-7 1:03 IN
I
LUG ALLOW STRESS =
MAX PIPE MOVEMENT (IN.)z --X------ Y----- 7-7--1.034 J-3 .279 _.293 -.118 -387 -.299 '
90/04/0
16998 PSI
THERMAL PIPE MOVEMENT (IN.) ---
.
----
-:.010 -.054
-------
.268 -. 049
024 -..007
\T
LOAD (LB) + -
DW LOADING CONDITION -------------------NORMAL
It
-1729
D
LOAD (LB + -
-0
)
SUPPORT LOAD COMBINATIONS ------------------------------------------1729 VSALL =DW
i' Attachment No.-- A Calc. No. -47A437o7-o SheetNo. &L..-
=-Rev.ev.
13
I
I
I
CLASS W)ST PROCESSOR PLANT WATTS BAR PIPING SYSTEM * RHR SPRAY YNODE NAME L15 SUPPORT DIR : Y SUPPORT TYPEOe VS
JSN = AOWL
90/04/
08.52.53. UNIT : UNIT 1 SHEET 2 OF 2
PAGE
104
A AlIJALYSIS I., 30METRIC PROBLEM DRAWING :: N3-74-02A B-47W432-205 SHlT 2 REV RO StJPPORT ID : 47A437-1-7
CODELU PIPE LUGALLOWABLE STRESS LO STRESS EQUATION STRESS (PSI) (LB) (PSI) S 1301 1729 16998 L9U 1940 1729 20019 9E 2034 1729 30905 9F 4309 1729 39610 LIO 10155 1729 17919 Lii 11457 1729 34917 2SY 14384 1729 40615 L1 OA 0 1729 56399 TEST8 1301 1729 20658 L1 OT 8868 1729 19206 L1 T 10170 1729 36204 CODE
LU LODCMIA ON LUG---LOAD COMBINATIONS------VSALL =DW VSALL =DW VSALL =DW VSALL =DW VSALL =DW VSALL =DW VSAL =DW VSAL =DW VSAL =DW VSAL =DW VSAL =0W
AMtachlmsenit No.
A
Ca!c. No._______ ; Sheel No.4t-1
--.I
--
. . 'N.:
NSS 2 POST PROCESSOR
JSN = ARTZ 90/06/ A7.42.42. PAGE WATTS BAR UNIT 1 WPING SYSTEM : RHR SPRAY A 1 OF 2 NODE NAME : L15 Al 4ALYSIS PROBLEM SUPPORT DIR : Y I'3OMETRIC DRAWING :: N3-74-02A 47W432-205 SHT 2 REV RO SUPPORT TYPE: VS StJPPORT ID : 47A437-1-7 DESIGN TRAVEL (+) 1.03 IN DESIGN TRAVEL -. 11 IN LUG DESIGN LOAD 172q T. , A,A, x,. LUG ALLOW STRESS = 16998 PSI rqN'1'
-------
(+)
:
X
_.323 ()-387
LOAD CASE
MOVEMENT -------Y 1.034 -. 118
(IN.) -------z .320 -. 340
THERMAL PIPE MOVEMENT X ------------Y f+) .010 .268 -. 054 -. 049
(IN.) -------
LOAD (LB) +
--------------
DW
-
-1729
LOADING CONDITION
LOAD
(LB
+
NORMAL
-
0
SUPPORT LOAD COMBINATIONS
-1729 VSALL
=DW
-. t
z . 007
-. 024
104
OLASS 2 POST PROCESSOR NT WaIPING SYSTEM
: WATTS BAR : RHR SPRAY A
NODE NAME : L15 SUPPORT DIR : Y SUPPORT TYPE: VS CODE CODE PIPE STRESS STRESS EQUATION (PSI) -------8 L9U 9E 9F Li0 Lll 2SY L1OA TEST8 L1OT LilT
JSN = ARTZ
1301 1940 2034 4309 10155 i1457 14384 0 1301 8868 10170
90/06/ US SH
07.42.42.
PAGE
UNIT 1 2 OF 2
AlNALYSIS PROBLEM : N3-74-02A I'3OMETRIC DRAWING : 47W432-205 SHT 2 REV Ro StJPPORT ID : 47A437-1-7 LUG LOAD (LB) --------1729 1729 1729 1729 1729 1729 1729 1729 1729 1729 1729
LUG ALLOWABLE STRESS (PSI) 16998 20019 30905 39610 17919 34917 40615 56399 20658 19206 36204
LUG LOAD COMBINATIONS -------------------------------------VSALL =DW VSALL =DW VSALL =DW VSALL =DW VSALL =DW VSALL =DW VSALL =DW VSALL =DW VSALL =DW VSALL =DW VSALL =DW
105
JSN - jARTZ 90/06/15.
2 POST PROCESSOR
w ,
*
UNIl r i
WATTS BAR
w3-74-02A
*.
....
...*...
**
..
SUPPORT DESIGN DATA
*
07.42.42.
PACE
626
RHRSPRAY A
*
: *
P.....P
....
*T*.P ........ A
SOPPORT TYPE SUMMARY TABLE bMODE SUPPORT IlAE DIRECT R89
K89
SZ
RR
RR
COORDINATE SYSTEM WOGLO
NONGLO
X
DIRECTION COSINES Y 2
AXIS
-.8090 .0000 .5878
.0000 1.0000 .0000
-. 5878 .0000 -..8090
X
-..8090 .0000 .5878
.0000 1.0000 .0000
-. 5878 .0000 - .8090
X
Y 2 Y z
K93
SX
RR
NONGLO
-. 8090 .0000 .5878
.0000 1.0000 .0000
-. 5878 .0000 -. 8090
N Y
K93
SZ
RR
NONGLO
-..8090 .0000 .5878
.0000 1.0000 .0000
-. 5878 .0000 - .8090
X
2
Y z
K95
SX
RR
NONGLO
-. 8090 .0000 .5878
.0000 1.0000 .0000
-. 5878 .0000 - .8090
N Y 2
K95
SZ
RR
NONGLO
-. 8090 .0000 .5878
.0000 1.0000 .0000
-. 5878 .0000 - .8090
Y z
K99
SX
RR
NONGLO
-. 8090 .0000 .5878
.0000 1.0000 .0000
-. 5878 .0000 - .8090
N V 2 N
K99
Sz
RR
NONGLO
-. 8090 .0000 .5878
.0000 1.0000 .0000
-. 5878 .0000 - .8090
Y 2
L14
SX
RR
NONGLO
-. 8090 .0000 .5878
.0000 1.0000 .0000
-. 5878 .0000 - .8090
NI V 2
L14
SZ
RR
NONCLO
-. 8090 .0000 .5878
.0000 1.0000 .0000
-. 5878 .0000 - .8090
NI V 2
VS
GLOBAL
l15 1 7?
SX
SUPPORT TYPE
-CALCULATION SHEET JOB NO.
CALC. NO.
20652 *
47A 4-370 o7 7
ORIGINATOR
Y'
REV. NO.
DATE
..
2
1
CHECKED
2-23
SHEETNO.
DATE
.
,.
ATTACHMENT B PIPE SUPPORT CONFIGURATION DATA 1. s
£
Walkdown Data: Walkdown Package:
8
Drawing Number:
9
2.
74 -
HAAUP Pkg. 47A 43 2 -/
RAU/ 9 - 002
-7
Rev.:
;A
Applicable RFI's:
10
I
Information RFI's:
12
Feasibility RFI's:__
13
Constructability RFI's:
14
.3.
-214 0 _/ __
_
_
_
r/-
Reason and Description of Modification _
//A
17
19
20 21 22 23 24 WALKDoA/A
5
4.
Pipe Support Configuration iX* .
26
5.
Other Data:
V Sk6r7C1
.'t ./9
/J/s
See Sheet B2
A/b
27
29 30 31 32
~I
I es4
Pow. DM
:-
I
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I
t:
i.
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HAMUP PKG 74-WAAQPc4 r
WALK DOWN CHECKED BY
B
A3-&r 'a
w. CATALOG
NO. NOT STAMPED ON PART-VERIFIED BY COMPARISON OF CATALOG DIMENSIONS
I
'
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M7AIt -
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ii
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AS BUILT DATA 7 4~ AiH-AAUP PKG WALK DOWN BY CHECKED BY
7e
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saw m
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:
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ALDOWN OF AS-BUILT PIPIlG SYSTEMS
.DER
ISO. or Banger NO. Originated 'Date
4
THE SCOPE OF 5T
RA&UP
7A4!7-1-V.Pc l -
WA 353(EN O[3-T-fl1
Drfi Date
MV -
,
OQ.
.~l
DATE
CHECKER
-I==
I
ATTACHMENT:
DT
CALC:
- 413-,
4 7
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A 4 7c70/o
SHEETS-,
.0-3--,%
i I-1
ATTAcENDlT
DESCRIPTION:
ca'y,7.
Iccq,
A.:E
.
-
..
.-
-3
aFJS 7-
-
Al
.
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07 C ,
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rI
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. Aerachrnent40. Z) |Ca'i,c Ne i.-e , -'t I = I=
a r,3
m-Ss-c2.:=z:::z-
1
eCTVhIM
2
ICAL RIQUEST MEMO
a 4
F-Oa74 - e
S 8
Draving No. 47A 437 -1 - 7
7
Stress Cac. No.
a
M3 -74 -02A
L_-_15
Data Point No. _
_
S 10
Description: The folloving information is required for the local stress evaluation at the
:11
velded attachment. 13 14
1) Pipe Size (OD,
-
2)
is
Sch.) and Pipe Material
Design Pressure
_3_ w (o)T i
(Cl)ozrtn
f"lds
teD
fairA#rAj -
P16
4) Sif used in stress analvaim st atA pt mf
Prepared by:
V
Approved by:
36 as
a
a 21
27
U as
,/
.°
8-
FDES 3 r MAX sIT
|P .a~u
h
I~0'
--r-
1
f ~
--
K,
TMi
-
Date:
m--
GX 27 7-
11
,
--
,A I !X
au "
hm
-12 -I'70
SCE/Thickness -
C-)97n I XIP'2 ILv 1 I I I I
' if 7 I ... /- , I/ MAT = S,!, I,, -
tao
Date: -
Response: (7-, ) 1) OD L. o-(, <
2)
iA&A
w
-
,' ;;
_n I
- eV DI
-
-74. I
x1 Z
-
A)S ?--L
D a
Pr
d
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by:. 3by~e
13!"tr' =.
te: s .Data
, ,/h _1-47+
.
'1
IIr -
, I
I
TITLE: B47A43701007 JOB NUMBER: WBN - 1 INPUT FILE: FAPPSO-DAT
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1_OUT
DATE: 90-02-23 TIME: 17:39:23
SHEET 1 ME150 VERS.-
IX
9
M
z m *wS@
* * **********
******
** *************
FRAME ANALYSIS PROGRAM FOR PIPE SUPPORTS "FAPPS"
*
ME-150
*
ORIGINATOR:
g
, CHECKER:
VERSION TVA RELEASE DATE USER MANUAL REVIS!ON VALIDATION MANUAL REVISION
*
:9 :10-22-1989 :8 :8
*
TVA ENGINEERING SPONSOR
* * * *
IP ,
e /CK
DATE:
/
C):
-1
/D
"I.w ';u 0
>i mq
*
JOHN K. MCCALL, *W*******
CHIEF CIVIL ENGINEER
TVA ENGINEERING
*
SPECIALISTS ***************
*
*
JACK THOMISON, FRANK PICKERING,
PRINCIPAL CIVIL ENGINEER PRINCIPAL CIVIL ENGINEER
*
,*
*************
TVA PROGRAM SPECIALIST ******************
*
*
23 - 90
*************
.,6.
* *
2-
*
*. -. coi***-z**i* *
DATE:
*
* *
Kt) Cr 0
=
*
DEAN DEARING,
WT 60 211 A-K
(615) 632-3302
*
*******************************
co j:7 M =rB -o~l TI~k li
QLiL
.1t -
7
. ;
.,1.
~-
------
TITLE: B47A43701007 JOB NUMBER: WBN - 1 INPUT FILE: FAPPS1 DAT
INPUT DATA
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1 OUT
DATE: 90-02-23 TIME: 17:39:23
SHEET 2 ME150 VERS.-
9
TITLE: B47A43701007 JOB NUMBER: WBN - 1 lNPUT FILE: FAPPS1 DAT
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1_OUT
CODE DESIGN 0. 0. UNITS: KIPS,INCHDEGREES (EXCEPT NOTED) FY SU(M) SU(W) E G DENSITY 36.00 58.00 70.00 11200. .000285000 29000. FYCT FYCS SUCT SUCS .90 .52 .70 .42 STRUCTURAL PARAMETERS: NLS M NJ NJREL NJWEI LD NJEM&BP 6 3 4 0 3 0 NJSTF NJOSP 0 1 JO!NT COORDINATES-GLOBAL: JOINT X Y z (0=FREE,1=SUPPORT) S 1 0.000 2(?9440 80.375 0 2 0.000 25 9.440 51.000 0 3 0.000 25 ?.440 -12.000 4 0.000 ).000 0.000 MEMBER INFORMATION: MEMBER JJ JK BE -TA PART SECTION 1 1 2 1 1 2 2 3 0.0 2 2 3 2 4 0.0 PART INFORMATION: PART LY LZ KY KZ WRPBC WRPLEN 2.10 1 0.00 0.00 2.10 0. 0.00 2.10 2.10 2 0.00 0.00 0. 0.00 SECTION INFORMATION: SECTION TRY(1) TRY(2) TRY(3) TRY(4) TRY(5) 1 208 0 0 G 0 2 204 0 0 0 0 LOADING INFORMATION FOR LOADING SET # 1: NAME OF LOADING SET # SWE-X ALLOW. FACTOR:
1
1.000
DESIRED OUTPUT INFORMATION: DISP. FORC. REAC. STR. EM-BP
WELD
(1=YES,O=NO)
DATE: 90-02-23 TIME: 17:39:23
SHEET 3 ME150 VERS.- 9
TITLE: B47A43701007 JOB NUMBER: WBN - 1 !NPUT FILE: FAPPSI DAT
1. 0. RESULT-TYPE:
0.
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1_OUT
0.
0.
DATE: 90-02-23 TIME: 17:39:23
SHEET 4 ME150 VERS.-
9
0.
2
NUMBER OF LOAD-JOINTS: 0
DEAD WEIGHT CONSIDERATION(1=YES,0=NO): 1 .000
DEAD WEIGHT GLOBAL COEFFICIENT: x 1.00
Y 0.00
'A'Y***S*
* ** * *
z 0.00
******* * **** ** ***
***
LOADING INFORMATION FOR LOADING SET # 2: MAME OF LOADING SET " S JWE-Y
2
ALLOW. FACTOR: .000
DESIRED OUTPUT INFORMATION: D!SP. FORC. REAC. STR. 1.
0.
0.
0.
EM-BP
WELD
0.
(1=YES,O=NO)
0.
RESULT-TYPE: 2 NUMBER OF LOAD-JOINTS: 0
DEAD WEIGHT CONSIDERATION(1=YES,0=NO): 1.000 DEAD WEIGHT GLOBAL COEFFICIENT: x y z 0.00 1.00 0.00 LOADING INFORMATION FOR LOADING SET # 3: NAME OF LOADING SET #
3
SWE-Z
ALLOW. FACTOR: 1.000
DESIRED OUTPUT INFORMATION: DISP. FORC. REAC. STR. 1.
0.
0.
0.
EM-BP 0.
WELD
(1=YES,O=NO)
0.
RESULT-TYPE: 2
--...
i~::--
-
TITLE: B47A43701007 JOB NUMBER: WRN - 1 tNPUT FILE: FAPPS1-DAT
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1_OUT
NUMBER OF LOAD-JO!NTS: 0 DEAD WEIGHT CONSIDERATION(1=YES,0=NO): 1i000 DEAD WEIGHT GLOBAL COEFFICIENT: x Y z 0.00 0.00 1.00 LOADING !I'FORMAT!ON
FOR LOADING SET # 4:
NAME OF LOADING SET # NO RMAL ALLOW. FACTOR:
DESIRED
OUTPUT
DES?. FORC. 1. 7. RESULT-TYPE:
4
!WFORMATION: REAC. STR. 1.
EM-BP 0. .
WELD 1.
(1=YES,O=NO)
NUMBER OF LOAD-JOINTS: JOINT FX FY FZ 1 0.000 .940 0.000 DEAD WEIGHT CONSIDERATION(1=YES,O=NO): 1.000 DEAD WEIGHT GLOBAL COEFFICIENT: X Y Z 0.00 1.00 0.00
MX 0.000
LOADING INFORMATION FOR LOADING SET # 5: NAME OF LOADING SET # 5 UPSET ALLOW. FACTOR: 1.330 DESIRED OUTPUT INFORMATION: DISP. FORC. REAC. STR. 1. 1. 1. 1. RESULT-TYPE: 2 NUMBER OF LOAD-JOINTS:
EM-BP 0.
WELD 1.
(1=YES,O=NO)
MY 0.000
MZ 0.000
DATE: 90-02-23 TIME: 17:39:23
SHEET 5 ME150 VERS.-
9
,i,, w m
TITLE: B47A43701007 JOB NUMBER: WBN - 1 INPUT FILE: FAPPS1 DAT
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1_OUT
1
JOINT FX FY FZ 1 0.000 .899 0.000 DEAD WEIGHT CONSIDERATION(I=YES,0=NO):
MX 0.000
MY 0.000
MZ 0.000
000
DEAD WEIGHT GLOBAL COEFFICIENT: X Y Z 2.66 1.73 2.66 LOADING INFCRMATIOM FOR LOADING SET # 6: htAME OF LOADING SET # 6 FAULTED ALLOW. FACTOR: 7.500 DESIRED OUTPUT INFORMATION: DISP. FORC. REAC. STR. EM-BP 1.
1.
1.
1.
WELD
(1=YES,0=NO)
1.
0.
RESULT-TYPE: 2 NUMBER OF LOAD-JOINTS: I
JOINT FX FY FZ 1 0.000 .899 0.000 DEAD WEIGHT CONSIDERATION(1=YES,0=NO):
MX 0.000
1 .000
DEAD WEIGHT GLOBAL COEFFICIENT: x Y z 2.66 1.73 2.66 * END OF LOAD DATA ****** DISPLACEMENT CHECK INFORMATION: ALLDSX ALLDSY ALLDSZ (ALLOW. DISP.) .0625 .0625 .0625 JOI DSXCHK DSYCHK DSZCHK (1=YES,O=NO) 1
0.
1.
0.
WELD DESIGN INFORMATION: JOINT MEM(B) MEM(M) WELD-PLANE 3 2 0 2 2 3 1 1 4 3 0 2 **LE (LOCAL EFFECT EVALUATION):
BMTHK .500 .250 .500
PHI 0.00 0.00 0.00
MY 0.000
MZ 0.000
DATE: 90-02-23 TIME: 17:39:23
SHEET 6 ME150 VERS.- 9
TITLE: 847A43701007 JOB NUMBER: WBN - 1 INPUT FILE FAPP51 DAT
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1 OUT
DATE: 90-02-23 TIME: 17:39:23
7 SHEET ME150 VERS.- 9
NUMBER OF CONNECT!ONS: JOINT 2
MEM(B) 3
MEM(M1) 1
MEM(M2) 2
CONN-PLANE 1
PHI 0.00
K 0.00
*RESULTS*
UMITS: K;PSIMC!,CREES FOR TRY( 1) SECTION PRCPERTIES:
SiECT.NO.
NAME
AX SZ
1
T4X4X4
2
T3X3X4
3.540 4.000 EY=
0.0000
EY=
2.590 2.100 0.0000
AY AZ RZ RY 2.000 2.000 1.500 1.500 0.0000 EZ= 1.500 1.500 1.100
EZ=
1.100
IX B 13.184 4.000
IY D 8.000 4.000
IZ TF 8.000 .250
SY rw 44.000 .250
5.199 3.000
3.160 3.000
3.160 .250
2.100 .250
0.0000
)R JOINT# F(
1 DISPLACEMENT IN lTHE GLOBAL Y DIRECTION IS
.08926 WHICH IS GREATER THAN THE ALLOWABLE OF
.0625
Ft OR JOINT#
1 DISPLACEMENT IN ITHE GLOBAL Y DIRECTION IS
.08619 WHICH IS GREATER THAN THE ALLOWABLE OF
.0625
Ft)R JOINT#
1 DISPLACEMENT IN lTHE GLOBAL Y DIRECTION IS
.08619 WHICH IS GREATER THAN THE ALLOWABLE OF
.0625
***********
*P***
CODE CHECK PASSED * ** **** * ***
***** *
UNITS: KIPS,INCH,DEGREES
LL E 8
AlLL
I V/Y
J L4 Y'
LESS,771fr' 1
'toS/
p
TITLE: 847A43701007 JOB NUMBER: WBN - 1 INPUT FILE: FAPPSI DAT
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1 OUT
DATE: 90-02-23 TIME: 17:39:23
SHEET 8 ME150 VERS.- 9
MEMBER BUCKLING DATA:
HEM
LZ 92.375 92.375 58.887
LY 92.375 92.375 58.887
1
2 3
STRESS RESULTS
TN
JO!
1 2 1 2 1 2
NAME
NORMAL NORMAL UPSET UPSET FAULTED FAULTED
KZ 2.100 2.100 2.100
ABSOLUTE TERMS(+/-)
LOAD M-M
KY 2.100 2.A00 2.100
TYPE
- -:---------------------------STRESSES---------------------------:--INTERACTION VALUES----: STRESS BENDING BENDING WARPING SHEAR SHEAR SHEAR ALLOW. MAXIMUM MAXIMUM MARGIN AXIAL Y Z NORMAL Y Z TORSIONAL FACTOR NORMAL SHEAR FACTOR
ACTUAL ACTUAL ALLOW ACTUAL ACTUAL ALLOW ACTUAL ACTUAL ALLOW
0.000 0.000
0.000 0.000
8.929 .000 .022 11.409 .000 .022 11.409
ACTUAL ACTUAL ALLOW ACTUAL ACTUAL ALLOW ACTUAL ACTUAL ALLOW ACTUAL ACTUAL ALLOW ACTUAL ACTUAL ALLOW
.000
0.000 0.000
0.000 0.000
0.000 0.000
23.760 0.000 0.000 31.601 0.000 0.000 32.400
.470 .485 14.400 .450 .475 18.720 .450 .475 18.720
14.400 .000 .039 18.720 .000 .039 18.720
14.400 0.000 0.000 18.720 0.000 0.000 18.720
4.918 2.136 23.760 4.805 2.158 31.601 4.805 2.158 32.400
0.000 0.000 23.760 0.000 0.000 31.601 0.000 0.000 32.400
.233 .235 14.400 .237 .241 18.720 .237 .241 18.720
0.000 0.000 14.400 .024 .109 18.720 .024 .109 18.720
3.988 1.751 23.760 3.965 1.924 31.601
0.000 0.000 23.760 0.000 0.000 31.601
.144 .145 14.400 .164 .170 18.720
0.000 0.000 14.400 .020 .097 18.720
23.760 .000 .289 31.601 .000 .289 32.400
7.012 23.760 .000 6.790 31.601 .000 6.790 32.400
.824 .824 8.929 .853 .901 11.409 .853 .901 11.409
0.000 0.000 23.760 .286 2.387 31.601 .286 2.387 32.400
1.253 1.261 11.343 1.256 1.282 14.462
0.000 0.000 23.760 .108 2.353 31.601
1.000 1 .000
.000
.295
.033 .034
30.638 3.389
1.330 1.330
.000 .226
.024 .025
41.646 4.425
1.500 1.500
.000 .220
.024 .025
41.646 4.536
0.000 0.000 14.400 .068 .068 18.720 .068 .068 18.720
1.000 1.000
.299 .182
.016 .016
3.341 5.488
1.330 1.330
.236 .223
.016 .017
4.239 4.489
1.500 1.500
.232 .219
.016 .017
4.312 4.561
0.000 0.000 14.400 .112 .112 18.720
1.000 1.000
.278 .185
.010 .010
3.593 5.408
1.330 1.330
.216 .224
.015 .015
4.635 4.464
2 2 3 2 3 2 3
NORMAL NORMAL UPSET UPSET FAULTED FAULTED
3 2 4 2 4
NORMAL NORMAL UPSET UPSET
TITLE: B47A43701007 JOB NUMBER: WBN - 1 tNPUT FILE: FAPPS1-DAT
2 4
FAULTED FAULTED
ACTUAL ACTUAL ALLOW
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1_OUT
1.256 1.282 14.462
108 2.353 32. 400
OVERALL M!NIMUM STRESS MARGIN FACTOR=
|
3.965 1.924 32.400
0.000 0.000 32.400
~3.34087 |
.164 .170 18.720
.020 .097 18.720
.112 .112 18.720
1.500 1.500
. )/
-/-
2
- 2-
Z / Z+
UMITS-
DATE: 90-02-23 TIME: 17:39:23
9vo / ta
KIS,INCH,DEGREES
DISPLACEMEhRT CXECK RESULTS(GLO8AL) JOINT
DIRECTION
1
Y
ALLOW. .06250
ACTUAL .08926
I
o - -- ,
V. b . /) /'12.
UNITS: KIPS,INCH,DEGREES
FO-X
,-s, u
JOINT DISPLACEMENTSCIGLOBAL) JOINT 1
2
LOAD NAME SWE-X +/SWE-Y +/SWE-Z
+/-
NORMAL UPSET FAULTED SWE-X SWE-Y SWE-Z NORMAL UPSET
+/+/+/+/-
+/+/+/+/-
X DISP .03277 U.UUOUO 0.00000 0.00000 .08717 .08717 .01898
Y DISP +/+/-
+/+/-
+/+/+/0.00000 +/0.00000 +/0.00000 +/.05048 +/-
0.00000 +/.00098 +
.00002 +/.08926 +/.08619 +/.08619 +0.00000 +/-
.00040 +/-
FP-ut ~
a/z f/I
/)
.2g .w19
Z DISP
X ROT -
°0.00000°
. .00005 .00179 .00192
+
0.00000 +1 -
+/+/+/-
.00192 +0.00000 +/-
.00136 .00019 .18930 .18260
+/+/+/+/-
.18260+/ 0.00000 +/-
.00821 +/-
.00008 +/.00005 +/.00179 +/-
.08808 +/
.00835 +/-
.00191 +/-
.08499 +/-
.00007 +/-
-;,- I 3 -, .
.00031 +/.00019 +/-
Y ROT .02712 +/0.00000 +/0.00000 +/0.00000 +/-
.07215 .07215 .02607 0.00000 0.00000 0.00000 .06935
+/+/+/+/+/+/-
+/-
O
2 3-90
Z / 24/ ?O
Z ROT .00441 0.00000 0.00000 0.00000 .01173 .01173 .00441 0.00000 0.00000 0.00000 .01173
.213 .221
SHEET 9 ME150 VERS.- 9
.015 .015
4.704 4.531
TITLE: B47A43701007 JOB NUMBER: WBN - 1 INPUT FILE: FAPPS1_DAT
FAULTED
.05048 +/-
+/-
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1 OUT
.00835 +/-
.00191 +/-
.08499 +/-
DATE: 90-02-23 TIME: 17:39:23
.06935 +/-
SHEET 10 ME150 VERS.- 9
.01173
UN'ITS: K!PS,!NCHDEGREES M--SER END-ACT!ONS IN LOCAL COORDINATE SYSTEM ------------------------------------FORCES ------------- :------------------MOMENTS-------------------: ME;MISER JO!NT LOAD NAME AXIAL SHEAR Y SHEAR Z TORSIONAL BENDING Y BENDING Z 1 I NORMAL 0.000 +/.940 +/'-I 0.000 4/0.000 4/ 0.000 +/.000 4/ 2 NORMAL 0.000 +/.970 +/0.000 4/0.000 4/ 0.000 +/28.048 4/ UPSET .000 +/.899 +/.000 4/ 0.000 4/ .000 +/.000 2 4/ UPSET .079 +/.950 +/.079 4/ 0.000 4/ 1.158 +/27.161 FAULTED 4/2 .000 +/.899 +/.000 4/0.000 4/.000 +/.000 FAULTED 4/.079 +/.950 +/.079 4/ 0.000 4/ 1.158 +/27.161 4/ NORMAL 2.919 +/.466 +/0.000 4/ 0.000 4/0.000 +/19.672 2 4/ NORMAL 2.919 +/.471 +/0.000 4/0.000 4/ 0.000 +/8.542 4/ UPSET 3 3.020 +/.473 +/.049 4/.480 4/ 1.143 +/19.222 4/ 2 UPSET 3.189 +/.482 +/.480 4/ .218 4/9.547 +/8.631 FAULTED 4/ 3 3.020 +/.473 +/.049 4/ .480 4/ 1.143 +/19.222 3 2 FAULTED 4/ 3.189 +/.482 +/.218 4/ .480 4/ 9.547 +/8.631 4/ NORMAL 3.245 +/.216 +/0.000 4/ 0.000 4/ 0.000 +/8.376 3 2 NORMAL 3.267 +/.218 +/4/ 0.000 4/ 0.000 4/ 0.000 +/3.678 4/ 4 UPSET 3.254 +/.246 +/.030 4/ .423 4/ .227 +/8.326 4/ 2 UPSET 3.321 +/.256 +/.146 4/ .423 4/ 4.942 +/4.041 4 FAULTED 4/3.254 +/.246 +/.030 4/.423 4/.227 +/8.326 FAULTED 4/ 3.321 +/.256 +/.146 4/ .423 4/ 4.942 +/4.041
UNITS: KIPS,INCH,DEGREES SUPPORT REACTIONS(GLOBAL) - -
-
-
- -
-
-
-
- -
-
-
-
TITLE: R47A.43701%CJ7 JOB NUMBERU W8W - I 3NPUT F!LE: FAPPS tD.AT
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1-OUT
DATE: 90-02-23 TIME: 17:39:23
SHEET 11 ME150 VERS.- 9
UNITS: KIPS,INCH,DEGREES WELD DESIGN: # t8
t,
JOINT 3
'442f
PLA7-E-
MEMBER 2
T4X4X4 WELDED TO 94--EL WELD PLANE = XY BASE METAL THK. = THETA Y = 90. THETA Z = 90.
7o
2
1C V
AWl/ AW2/ AW3
--- - - - - -
1
2
SW2/ SW3/ JW
C2/ C3
CLC
F1/ F2/ F3
FR
- - -.
Ml/ M2/ M3 - -
6.00 3.00 6.00
3.00 12.00 28.50
1.50 2.00
6.00 6.00 3.00
12.00 3.00 28.50
2.00 1.50
16.00 8.00 8.00
21.33 21.33 85.33
2.00 2.00
5 4.438 4 3.335
-
-
-
-
/-,
L<90 L=90 L>90 -
-
-
9 2 - 2 3 - I0
/,
z/z f /,? o
,,
.5000
MINIMUM SIZE FILLET PENE. WELD TYPE
Y.i
-
W<90 W=90 W>90 -
3.189 .482 .218
.480 9.547 8.631
3/16 -
2.919 .471 0.000
0.000 0.000 8.542
3/16 -
-
-
-
-
STRENGTH SIZE FILLET PENE.
S<90 S=90 S>90 -
-
-
-
L<90 L=90 L>90 -
-
-
-
W<90 W=90 W>90 -
-
-
RECOMMENDED SIZE FILLET PENE.
S<90 S=90 S>90 -
-
-
-
L<90 L=90 L>90 -
-
-
-
-
-
3/16 -
-
1/4
1/4
-
-
-
-
-
3/16 -
-
1/4 -
1/4 -
-
3/16 -
-
-
-
-
:
1/16
-
:
-
-
:
-
-
W<90 W=90 W>90 -
-
-
-
-
-
-
-
* 1/4
:
S<90 S=90 S>90 -
-
MARGIN FACTOR -
-
- -
-
-
-
1/4
-
-
-
-
1/4
1/4
-
-
-
-
-
-
-
-
1.055
1.080 ,
------------------------------------------------
5
3.189 .482 .218
1.055
3/16 -
.480 9.547 8.631
1/16 -
3/16
3/16
-
-
-
.*17
'/
4 v.2 17
V- 4
3.328
-
I
I^ -
AC'T7 &r U
V
;i
5
4-,tv /I 1,, 0 -W,~
Tt/CL ,E
/
C7 p
tV
S((f Ar4ce
eW/" (
5
ca Ivirre v,?
'
0 g
/<''< A-'V A (f 6 0 Po F-7 A r 6 57 ° - WE-L D Ci- X F1- c 711A ' ' ' -' ' ) -- o' I 8 7S x< eI,/ = / 7' °
) 25
- X 0 ./
^
o..27"
'
Vi
A /") "?--23 - 7 o
,
1z/f/l0
(lfe F /5)
TITLE: B47A43701007 JOB NUMBER: WBN - 1 INPUT FILE: FAPPS1-DAT
4
5
11.00 7.00 4.00
16.67 6.26 48.27
2.00 2.39
11.00 4.00
6.26 16.67 48.27
2.39 2.00
7.00
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1_OUT
5 2.696 5 2.790
.673
3.189 .482 .218
9.547 11.458
3/16 -
3.189 .482 .218
.907 12.374 8.631
3/16 -
DATE: 90-02-23 TIME: 17:39:23
-
3/16 -
-
-
3/16 -
-
3/16
-
-
-
-
3/16 -
-
-
* : 3/16
-
-
SHEET 12 ME150 VERS.- 9
3/16 -
-
1.302
-
-
3/16 -
3/16 -
-
:
-
3/16 -
3/16 -
-
1.258
-
UNITS: KIPS,INCH,DEGREES WELD DESIGN:
JOINT 2
MEMBER 3
T3X3X4 WELDED TO T4X4X4 WELD PLANE = XZ BASE METAL THK. = THETA Y = 90. THETA Z = 30.
0.0000
MINIMUM SIZE FILLET PENE. WELD TYPE
AW1/ AW2/ AW3
SW2/ SW3/ JW
C2/ C3
CLC FR
Fl/ F2/ F3
M1/ M2/ M3
L<90 L=90 L>90
W<90 W=90 W>90
GENERAL NOTES FOR WELD 1) MINIMUM AND MAXIMUM WELD CHECKS ARE BASED ON ONLY MEMBER
1
2
4.00 2.00 4.00
1.33 12.00 37.34
1.00 3.00
8.00
12.00
1.50
8.00
5.33
2.00
4 1.858 4
1.809 2.919 0.000
0.000 0.000 8.376
1.809
0.000
2.919
0.000
-
3/16
S<90 S=90 S>90
STRENGTH SIZE FILLET PENE. L<90 L=90 L>90
W<90 W=90 W>90
RECOMMENDED SIZE FILLET PENE.
S<90 S=90 S>90
L<90 L=90 L>90
W<90 W=90 W>90
S<90 S=90 S>90
MARGIN FACTOR
3 THICKNESSES -
-
3/8
: :
-
-
-
-
-
1/8
:
-
-
PP 3/8 PP 1/8
-
-
.
-
-
-
:
-
3/8 1/8
-
-
-
-
13/16
3/16
L--.
--
3/16
-
3/16
-
3/16
-
1.003
:: 4'I
<
1.473
-
cl",l _j2'F72
lrW
.-- -
SIeoA/
.cLXr .A
,
0 , Ic- .
Y -
, /'' *)
m,97,4
P07?aI l
- '23-v
Z/ 2 V/ 9
iL
TITLE: B47A43701007 JOB NUMBER: WBN - 1 INPUT FILE: FAPPS1-DAT
4.00 -
--
3
4
-
28 67 -
-
-
-
18.00 12.00 6.00
21.00 3001 121.53
13.00 10. 0 3 COO 3.100 11.00O 6.00 5.00
16.50 11.46 60.02
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1 OUT
1.833 -
-
1.50 3.00
0.000 -
-
-
-
-
8.376 -
-
-
-
-
-
-
-
DATE: 90-02-23 TIME: 17:39:23
-
-
-
4
1.809 0.000 3/8 5/16 2.919 0.000 3/16 3/16 1/16 1/16 .451 0.000 8.376 1/8 1/16 ---------------------------------------------------------------1.50 4 1.809 0.000 3/8 3/8 3.08 2.919 0.000 3/16 3/16 1/8 1/8 1.080 0.000 10.324 1/8 1/8
3.55
1.93 3.00
21.00 69.88
SHEET 13 ME150 VERS.- 9
4
1.809 2.919 0.000
1.186
2.720 1.686 8.376
3/16 -
3/16 -
3/8 1/8
1/8 -
1/8 -
3/8 1/8
pP- 3/8 3/16 -
3/16
-
3/16 -
3/16 -
Pp 1/8
3/16 -
PP 3/8 PP 1/8
1.725
3/16 -
PP 3/8 PP 1/8
1.572
4.133
UNITS: KIPSINCHDEGREES WELD DESIGN:
JOINT 4
MEMBER 3
s CV. WELDED TO *AUX.-STEC[-
T3X3X4 WELD PLANE = XY THETA Y = 90.
V,
BASE METAL THK. = THETA Z = 60.
>' H'
M. I .5000
z - 23-
a/ z4/I6>
MINIMUM SIZE FILLET PENE.
STRENGTH SIZE FILLET PENE.
WELD TYPE
: :
RECOMMENDED SIZE FILLET PENE.
AW1/ SW2/ C2/ CLC F1/ M1/ L<90 W<90 SC90 L<90 W<90 S<90 . L<90 W<90 S<90 MARGIN AW2/ SW3/ C3 F2/ M2/ L=90 W=90 S=90 L=90 W=90 S=90 : L=90 W=90 S=90 AW3 JW FR F3 M3 L>90 W>90 S>90 L>90 W>90 S>90 : L>90 W>90 S>90 FACTOR -------------------------------------------------------------------------------------------------------------------------------4.00 1.33 1.00 5 3.004 2.837 3/16 3/16 5/16 1/4 : 5/16 1/4 1 2.00 6.93 1.73 1.882 4.492 : 1.014 4.00 13.33 4.859 .146 4.041 3/16 3/16 3/8 5/16 3/8 5/16 ----------------------------------------------------------------
--------------------------
TITLE: 847A43701007 JOB NUMBER: WBN - 1 INPUT FILEt FAPPS1 DAT
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1 OUT
4.62 6.93 1.50 5 3.004 2.837 4.62 1.78 1.15 1,882 4.492 2.31 12,44 3.664 .146 4.041 -------------- ------ ----------------12.93 i3.39 1.50 5 3.004 2.837 3 6.93 14.39 1.73 1.882 4.492 6.00 45.01 .934 .146 4.041 -----------------------------------------------------8.77 10.6 1.50 5 3.004 2.951 4 5.77 4.19 1.94 1.882 4.492 3.0 23. 3s 2.384 .146 6.391 2
8.46 3.46 5.00
5
3.29 10.66 24.26
1.76 1.73
5 2.939
3.004 1.882 .146
4.270 6.780 4.041
3/16
3/16
-
1/4
1. 14
DATE: 90-02-23 TIME: 17:39:23
-
:
1/4
3/16 3/16 3/16
3/16 3/16 3/16
-
-
M
3/16 3/16 3/16
3/16 3/16 3/16
-
3/16 3/16 3/16
3/16 3/16 3/16
-
1/16 6 1/8
-
-
: 3/16 : 3/16 : 3/16
3/16 3/16 3/16
-
3/16 3/16 3/16
1/8 3/16 3/16
-
: 3/16 : 3/16 : 3/16
3/16 3/16 3/16
-
-
3/16 3/16 1/4
3/16 3/16 3/16
-
: : :
3/16 3/16 3/16
-
3/16 3/16 1/4
MEMBERS: 3
LOAD CASE
LOAD NAME
ALLOW. FACTOR
fab/ fam
fbyb/ fbym
fbzb/ fbzm
Fl
1.3 .8 1.3
0.0 0.0 .1
4.0 4.9 4.0
1.8
4
NORMAL
1.00
5
UPSET
1.33
1.8
1.277
2.741
-
'
.-----
LOCAL EFFECT EVALUATION:
BRANCH: B= MAIN : B=
-
1/16 r/=16 I 1/16
UNITS: KIPS,INCH,DEGREES
T3X3X4 CONNECTED TO T4X4X4 CONN. PLANE = XZ THETA Y = 90. THETA Z = 30. 3.000 D= 3.000 TF= .250 TW= .250 4.000 D= 4.000 TF= .250 TW= .250 K=
1/4
0
-.------------------------------------------------
JOINT 2
SHEET 14 ME150 VERS.- 9
0.000 M12
M3
/--ACTING---/--ALLOWABLE--/MARGIN VP F VP F FACTOR
0.0
8.4
2.0
N/A
10.0
N/A
4.97
5
8.3
2.0
N/A
13.0
N/A
6.48
1.074
1.006
o
k'.
i6 Ml,9
. /
2-2-
2/2'9/90
TITLE: 847A43701007 JOB NUMBER: WBN - 1 INJPUT FILE: FAPPS1 -DAT
6
FAULTED
1.50
CALCULATION NO. 47A43701007 ATTACHMENT NO. OUT FILE: FAPPS1 OUT
.9 1.3 .9
.3 .1 .3
4.8 4.0 4.8
1.8
.5
8.3
OVERALL MINIMUM LOCAL EFFECTS MARGIN FACTOR(w/o stiffeners):
49
THE FOLLOWING FILES WERE USED FOR CONSTANTS FOR STEEL TABLE FOR SHAPE MENU FOR BASE PLATE W/ANCHORS FOR EMBED PLATES FOR STD. FRAME CONSTANTS FOR ME150 BANNER ********
FROM YOUR PROJECTFILE=$USER.WBNFAPPS =:NVE.KXL!BDC.WBN FAPPS.FAPPSCONST =:NVE.KXLIBDC.WBN FAPPS.AISCTAB =:NVE.KXLIBDC.WBN-FAPPS.AISCMEN =:NVE.KXL!8DC.WBN FAPPS.FAPPSBP =:NVE.KXLIBDC.WBN FAPPS.FAPPSEMB =:NVE.KXLIBDC.WBN-FAPPS.STD =$SYSTEM.APPLICATIONS.ME15O.VER_9.BANNER
2.0
-
N/A
DATE: 90-02-23 TIME: 17:39:23
13.0
N/A
SHEET 15 ME150 VERS.-
9
6.48
J: .
.9
M,
g
zlzl-lqo
******* ***********
PROGRAM EXECUTION FINISHED ****
** * ******** ***
PROGRAM EXECUTION ************
***
****
*
FINISHED ** ***
** **
... ,
, o,
, r, ., .1.. ... ... r : ; 7.
: ! ; .: . :.;.;I
-. : .- - : ,
; -f
CALCULATION SHEET
2 2 4 5 6 7
a 9 10 11
ATTACHMFENT
F
12 13 14
INTEGRAL WELDED ATTACHKNT EVALUATION
le 17 le 10 20 21 22 23 24
as 27
20 at
/
ATTACHMENT
'
F
CALCULATION SHEET
P
JOB NO.
CALC. NO.
REV. NO.
18 968 DATE
4Ae,
CHECKED
I 2/1IS/ 8 p9
SHEET NO.
V
77oo
47A 4370
ORIGINATOR
2
UECPC2706 ft.. 8/86 (EO49)
DATE
1 <
lldks~isq
REF
InteQral Welded Attachment Evaluation
Lug height
3
h=
4
f '12/2/
h-IJPz,
5 6
3>.P.
7
10
Fk
DESIGN DATA: Pipe Size: Design Temp:
11
ITEM
(Units: Lbs., In., Deg. F., PSI) B Sch.: 4O Material: SA31 Cold L40 Hot mo° Pipe OD: S 625" LENGTH
12 13
ATTACHMENT
I
(2L 2 ) WIDTH (2L 1 )
7II6
Weld Size and Type
15
bevvepe luspec Loads at surface of pipe
SC
3-t
e
(C.G.
,
i8 19
.
-
MAT'L REF.4
2-1490
30ML'L316AL
---
SEC. 5.I
A2
I
Sy (Weld) = AcKu
L. 1'
L' k, Wt
- -Applicable Not Applicable
Friction Load: QP Q 1, =
LOAD CASE
I-
0_3z_ SY
|5o700
of lua):
Friction Force
In
i-
TP34O
t:
SH
I'S700
I/I
aI
14
-17
LIT
M L = Q2 -* 3/1+/" L C-\ckmp\
8 9
_
Q2 =
Q1
Q2
IRFLDCE
MLML
W W
-ITPER.S
MT
s~g
NC8
865
6L49
C7a6S-
NC9U
E6S-
6L
2z0514
NC9F
865
64
20 21 . 22 23
NC10
-865
24
26
27 28
IAP OUTPUT EVALUATTON:
1. 2.
31 32
6
(Code Case N-318-3)
NC1l-
3z2Z 7
CHECK PARAMETERS:
29 30
F
86c
2SY
25
3.
For 2-sided Fillet or Partial Penetration Welds: L2 (= ) >3L1 ( ) OK N.G. a)
Circum. Separation = 6'Z7>
b)
Long. Separation=
All Other Parameters: 7 Acceptable As Is
6"
>
l,
(=_1 16), 6
E' (= 7i~E"),
-_AcceptableBased
V NA OK /-OK
-N.G. -N.G.
on Modif ied
Conservative Dimensions.
36
PIPE LOCAL STRESSES ACCEPTABLE FOR ALL EQUATIONS: LUG IS STRUCTURALLY ADEQUATE: YES NO
/ Yes
INo
SHT. S/to
ATTACHMENT
_
_
CALCULATION SHEET JOB NO.
BEPC.2706
CALC. NO.
18968
L. 7A
ORIGINATOR
DATE
REV. NO.
SHEET NO.
4
F13
o 100c7
437
CHECKED
DATE
.kl 2
r
INTEGRAL WELDED ATTACHMENT
EVALUATION
Structural
4
P
/ squA \*S
(continu ed)
2
3
Rw. 8/86tED9)
Adequacy Of The Lug Attachment
5
6 7
S
2L2
in
8
9
r\±
10
M
11 12 13
14
PARAMETERS
14
V
2L 2~
inches, 2L 1=
16
S = (2 L2 ) (2L,) 2/6
17
3/14
iCi4ES (MOM EWT ARM )
inches, H-='/
/
.inches,
Sy=
21 4qC)-
Psi
in3
=
192
ST= abd2
20
= 0.208(2L2 ) (2L1 ) 2
21
Av=0.67(H
* 2L 1 )
22
Ah=O. 67 (2L
1
) (2L 2 )=
23
Ab=
3/4 =
7S-
25
MOMENTS
26
3
:n
=
*
in 0 in2
67,
in2
(Contact Area)
& STRESSES
N/A
MN/SN <0.6SY;
Mt4=Q1H-=
Pd/A
.=Q2H= ML
6 W9
Ml T=QiL 2=
F/A
in-lb
27
28
ML/SL <°.6S Y;
29
19 47
-
in-lb
TORSIONAL STRESSES:
30
MT/ST <0.4SY;
I
t/A
31
in-lb
SHEAR STRESSES: Q2/Ah
34
4
S;
&
&859b
/bl= 2cR1
-2
Q1/Av
<0.4S
85
35~~~~
Be>X:-i5=@/^b
=
865/3,-
=
Z30'1
<-
0
35
36
Notes:
*
Desiqn of Welded Structures hy 1~Rl~nein -
-
_-
-
-
1-
--
-.
:t;
a=0.208
for b/d=1.0
E174 2.L 15
07 4 Z LA
jATT~EPACHMNT: CALC: 47,-C43?c/o7 HE ;_- - SHEET:
IIIIIIIIII
AAAAAAAA
£
REV.
PPPPPPPPP
IIIIIIIIII AAAAAAAAAA PPPPPPPPPP II AA AA PP PP II AA AA PP PP II AA AA PPPPPPPPPP
II AAAAAAAAAA PPPPPPPPP II AAAAAAAAAA PP II AA AA PP IIIIIIIIII AA AA PP IIIIIIIIII AA AA PP TENNESSEE VALLEY AUTHORITY
INTEGRAL ATTACHMENT ANALYSIS PROGRAM TVA SOFTWARE ID: 262402 VERSION 1 JUNE 17,
1988
/
TVA INTEGRAL ATTACHMENT ANALYSIS PROGRAM jiLE: PROB: N3-74-2A SUPP: 47A437-1-7 LYSIS = N-318-3
PAGE D.P. L15 DATE: 15 DEC 89
TIME:
5:07 PM
PROGRAM CAPABILITIES: 1) RECTANGULAR LUG ATTACHED TO STRAIGHT PIPE PER ASME CODE CASE N-318-3 2) HOLLOW CIRCULAR ATTACHMENTS ON STRAIGHT PIPE PER ASME CODE CASE N-392
PROGRAM LIMITATIONS: THIS PROGRAM ONLY ANALYZES THE LOCAL STRESSES INDUCED INTO THE PIPE AND THE INTEGRAL FILLET WELD IF USED. QUALIFICATION OF THE INTEGRAL ATTACHMENT IS BEYOND THE SCOPE OF THIS PROGRAM. USER IS RESPONSIBLE FOR ANY OVERLAPPING STRESS OCCURING BECAUSE OF LUG SPACING OR OTHER STRESS RISERS LOCATED ON THE PIPE.
ATFACo;viEN__: CALC:
47>T43-7
SHEETiLX--
-s
, /0107RE °
,RV
1
_
PAGE
- TVA INTEGRAL ATTACHMENT ANALYSIS PROGRAM LE: PROB: N3-74-2A SUPP: 47A437-1-7 LYSIS = N-318-3
*
D.P. DATE:
L15 15 DEC 89
TIME:
*
GEOMETRY DATA
* *
PIPE SHELL INFORMATION PIPE SIZE
PIPE SCH
8
MATERIAL ID
(INCHES, PIPE DIA
USER MATL
ATTACHMENT INFORMATION ATTACHMENT LENGTH WIDTH 2.0000
PSI,
WALL THK
8.625
.5000 USER MATL
ALLOW STR & MTL TEMP SC/TC SH/TH SY/TH
.3220
18800. 40.
PSI,
DEGREES F)
(INCHES,
MATERIAL ID
DEGREES F)
17900. 190.
25500. 190.
ALLOW STR & MTL TEMP SC/TC SH/TH SY/TH -----
------
------
15700. 40.
15700. 190.
21490. 190.
WLD MAT PROPERTIES BASED ON A ROUNDED TEMPERATURE OF 100 F
WELD INFORMATION WELD TYPE
LEG SIZE
(INCHES,
PSI)
SY WLD THROAT
KL
50000.
3.6
--------F 3S-FILLET
.1875
2
5:07 PM
TVA INTEGRAL ATTACHMENT ANALYSIS PROGRAM ;LE: PROB: N3-74-2A SUPP: 47A437-1-7 y LYSIS = N-318-3
PAGE D.P. L15 DATE: 15 DEC 89
TIME:
5:07 PM
* *
*
LOAD DATA
*
APPLIED ATTACHMENT LOADS AND STRESS RESERVE MARGINS LOAD CASE
Q1 (LB) MN (IN-LB)
Q2 (LB) ML (IN-LB)
W (LB) MT (IN-LB)
RESERVE STR (PSI)
-----
NC8
.0 .0
865.0 649.0
.0 .0
17265.0
NC9U
.0 .0
865.0 649.0
.0 .0
20514.0
NC9F
.0 .0
865.0 649. 0
.0 .0
41153.0
0
.0 .0
865. 0 649. 0
.0 .0
15005.0
NC9E
NC1OA NC11
32271.0
ABSOLUTE VALUES OF MAXIMUM LOADS OCCURING SIMULTANEOUSLY Q1A (LB)
Q2A (LB)
WA (LB)
MNA (IN-LB)
MLA (IN-LB)
MTA (IN-LB)
--------
.0
865.0
.0
.0
649.0
.0
A ACHE lENT: CALC: 4-7 44-2 7o/,0
SHEET:
EN-TE. --
REV.
3
1
.
TVA INTEGRAL ATTACHMENT ANALYSIS PROGRAM LE: PROB: N3-74-2A SUPP: 47A437-1-7 O LYSIS = N-318-3
PAGE D.P. L15 DATE: 15 DEC 89
TIME:
5:07 PM
* *
ANALYSIS RESULTS
* *
CALCULATED ATTACHMENT-SHELL GEOMETRY PARAMETERS PARAMETER
VALUE
LIMIT
----------
BETA2 BETA2 BETA1*BETA2
DO/T SQRT(RM/T)
.060 .241 .015 26.786 1.156
0.500 0.500 0. 075 100. 000
MINIMUM ATT SEPERATION
INTERMEDIATE EQUATION PARAMETERS PARAMETER
VALUE
PARAMETER
10.279 2. 664 1.307
VALUE
BT BL BN
6.853 1.776 .872
ATTACHMENT AND WELD SECTION PROPERTIES FOR STRESS CALCULATIONS /---- ATT SECTION PROP----/
AL (IN**2)
ZLL (IN**3)
-------
ZLN (IN**3) -------
1. 000
CALCULATED WELD GAP (IN)
.333
.083
SKEW WELD ANGLE (DEGREES) ---------
.0073
/----WELD SECTION PROPERTIES ----- / AW ZWD ZWL ZWT (IN**2) (IN**3) (IN**3) (IN**3) -------
94.5730
-------
.552
-------
.196
-------
.128
.220
EFFECTIVE THROAT (IN) .1227
ArtACHNIENT:
_-
CALC: -4-74E 7 ° /. °L7 REV SEET:
4
L
TVA INTEGRAL ATTACHMENT ANALYSIS PROGRAM
E
LE:
PROB: N3-74-2A
SUPP: 47A437-1-7
K|LYSIS = N-318-3
PAGE D.P. L15 DATE: 15 DEC 89
TIME:
5
5:07 PM
*
*
ANALYSIS RESULTS
*
*
STRESS SUMMARY OF CODE CASE N-318-3 ANALYSIS CODE CASE EQUATION
NC8 NC9U NC9E NC9F NC10 NC1OA NC11
SML
SPL/2
5188.3 5188.3
TOTAL STRESS
RESERVE STRESS
--------
--------
5188.3 5188. 3
17265.0 20514.0
12451.4
5188.3 12451.4
41153.0 15005.0
12451.4
17639.7
32271.0
5188. 3 5188. 3
(PSI)
SML FOR NC11 = SML FROM NC8 M FOR NC11 = SPL FROM NC10
P.
N-318-3 EQUATION
EQN EQN EQN EQN
5 6 7 8
STRESS
6917. 5 1730.0 6440.4 3133.9
ALLOW
53725.0 21490.0 42980.0 21490.0
1.. ~CIVIL/ MCELOICAL RBOUEBT NMEMO
-
2
CMRM
3 4
-
i
I+
No.
- 1
5 6 7
8
1 4
Drawing No.
A2 4 371- 1- 7 rht 3 -74 - -A
Stress Calc. No. Data Point No.
9 10
Description: The following information is required for the local stress evaluation at the
11
12
welded attachment.
13
1)
Pipe Size (OD, Sch.) and Pipe Material
2)
Design Pressure
14 1s
3)
TMAX
4)
1B
(Hot)/ TMIN (Cold)3operating temp. including faulted condition.
Sif used in stress analysis at data Pt of welded attaahment.
19
Prepared by:
20
Approved by:
(r
Response:
,,
Date:__________ -
-Date:-
21 22 23
1) OD
24
t2,)
-
a
' 4 31;
MAT
SCH/Thickness = TP3DL
SC
-),
SH lio
-
I1~
I
I,
SY -
-
2-.-f
25 26 27
2B
15c
L 2)
1)ES
3)
rMAX
_
4)
SIF -
V1-
=
90
p
TMW
f f TMIN fi
°
-
29 a0
DApproved
u
21 2
Prepared by:.
-~,
Disapproved
v
-Date:
33
Approved by: .
z-r
-
Lead Stfess Engineer
Date:
.//-
V -i57 .
C0; , {-
)
I
V
. '.
. ATTACHMENT:
G
CALC: 1744+37 0/ 007 SHEET: r
.L
REV. __/
TENNESSEE VALLEY AUTHORITY WBN HAAUP Joii.3 .1)8-63
UNVERIFIED CALCULATION ASSUMPTION
JC2A N(O,
4-7A 4-3 7 00 7 (SUPPORT MARK NO.)
OPE,£il, CLOSE D,
2 - 23 E-
-
-
o
(SEQ.
- q9 (DATE)
BYI:
- fo
Y ..
NO.)
PATE
i7 lol/
-BY
1, I
(DATE) REV.
IORIGINATOR
%
|
DETAILED DESCRIPTION:
,
DATE I CHECKER
DATE
I/7i
The Non Standard Component Item listed in this calculation (Item/s No. 6 ) has been sent to Bechtel Plant Design Staff for evaluation and is not cualified in this calculation.
REQUIREMENTS TO CLOSE: Approval of the above mentioned Non Standard Component based on analysis Rerformed by Bechtel Plant Design Staff.
Note:
Authorization by TVA is rea'd to perform.
Ref. Analysis
CLOSED PER FOLLOWING DOCUMENTATION/CALCULATION:
7'/lj z4
/d eoteo
/pe
4&
- r6p-ko
. ffeF -
t1
3f
,
.
;
a 1.,il
--
,,
I i
.I.
I
.
1..
I
I
-
I
.
. .
r-.
,
(/Iw
.
.
R00 72 58
-CX.
wFm
CO1GOM STRESS PROD-,O
T
MAxnck=L
A.-
zmDRmwX~ II
ML PM R
U
No0.
.24
BILL O? HAlO.MO IT2o (SIE ATCUD sxf=)
TY SW R
6
o
lo. 7Sl-624160
981423
TASKt LOAD RATE THE CLAMP SHOWN ON THE ATTACKED SKETCR.
-r; PM Ta
I
B E C H T E L
C02amt Gl-BIP
L.P/A's
MPRAm: -
ATR:.
.
-
/?e F
S
d-er1M
4
-A
•-
67
f
.
RiZSVa=LSS 0P ENGXnG EVAL B E R a
LOAD RATING NORMAL: I cD4 UPSET: e FAULTED :±_L4 .
N p A, T
0 N
-%
-NG ;'. E~rENG APPROVA
Le" ,L
^~
_~4
Q&UjAZ
I
-~
-=
