CIS EVA(SideWall) 6320 Sdwl 01

7/25/2019 CIS EVA(SideWall) 6320 Sdwl 01

1/29

MAXIMUM STRESS & DEFLECTION RESULTS SUMMARY

ITEM : Methanol Injection Skid (A!"#$%

PROJECT NO. N'A

Description Max Bending stress Result Max Deflection Result

nit psi in !!

SIDE ALL (#% )*+*,! $--."# NAME/ "."#$ "*.** ection 2 t'$ (need%ori&ontal stiffener $#+"56 #*,."* NAME/ '.()* ).", O.7

+ertical stiffener NAME/ NAME/ NAME/ ,N-ME NAME/ NAME/

SIDE ALL ($% REF8 REF8 NAME/ ,RE/0 REF8 REF8

%ori&ontal stiffener REF8 REF8 NAME/ ,RE/0 REF8 REF8

+ertical stiffener REF8 REF8 NAME/ ,RE/0 REF8 REF8

9OTTOM ALL N'A N'A NAME/ ,N1- N'A N'A

%ori&ontal stiffener N'A N'A NAME/ ,N1- N'A N'A

+ertical stiffener N'A N'A NAME/ ,N1- N'A N'A

ROOF ALL N'A N'A NAME/ ,N1- N'A N'A

%ori&ontal stiffener N'A N'A NAME/ ,N1- N'A N'A

+ertical stiffener N'A N'A NAME/ ,N1- N'A N'A

N1!!2


2/29

TA9LE OF CONTENT:A;E

( T3RP*'2 : 4IDE 5-66 7(8 DE4I9N C-6C6-TION ) $ -

2 TR:6,$ < SIDE ALL (#% STIFFENER LOCATION # *

" T3RP*'2 : 4IDE 5-66 7(8 %ORIONT-6 4TI//ENER C-6C6-TION # !

) T3RP*'2 : 4IDE 5-66 7(8 +ERTIC-6 4TI//ENER C-6C6-TION # 5

; T3RP*'2 : 4IDE 5-66 728 DE4I9N C-6C6-TION ) " #,

# TR:6,$ < SIDE ALL ($% STIFFENER LOCATION # ##

< T3RP*'2 : 4IDE 5-66 728 %ORIONT-6 4TI//ENER C-6C6-TION # #$

$ T3RP*'2 : 4IDE 5-66 728 +ERTIC-6 4TI//ENER C-6C6-TION # #)

* T3RP*'2 : BTM 5-66 DE4I9N C-6C6-TION # #-

(' TR:6,$ < 9TM ALL STIFFENER CALCULATION # #*

(( T3RP*'2 : BTM 5-66 %ORIONT-6 4TI//ENER C-6C6-TION # #!

(2 T3RP*'2 : BTM 5-66 +ERTIC-6 4TI//ENER C-6C6-TION # #5

(" T3RP*'2 : ROO/ 5-66 DE4I9N C-6C6-TION # #"

() TR:6,$ < ROOF ALL STIFFENER CALCULATION # #6

(; T3RP*'2 : ROO/ 5-66 %ORIONT-6 4TI//ENER C-6C6-TION # $,

(# T3RP*'2 : ROO/ 5-66 +ERTIC-6 4TI//ENER C-6C6-TION # $#

A::ENDIX

(< # $$

($ 4ECTION-6 4TI//ENER PROPERTIE4 C-6C6-TION 7Botto! 5all8 # $)

(* T-B6E O/ RO-R= /ORM6- $ $- $*

N=>?e4o1 @ae3

4ECTION-6 4TI//ENER PROPERTIE4 C-6C6-TION74ide 5all(>2 and Roof 5all8


3/29

SIDE ALL (#% DESI;N CALCULATION (:a4t #%

TAN7 NO. < T!)$-

:ROBECT < 7RA7EN F:SO

Design

Tan? %eig@tA % $' in 2'"2 !! Pressure arg psig ?P-

Tan? 5idt@A 5 *).)* in 2)'' !! Top '.'; '.=> 9endin 3t4e33+ (qb2)/ t2

4

a

4

4

4


4/29

SIDE ALL (#% DESI;N CALCULATION (:a4t $%

TAN7 NO. < TR:6,$

:ROBECT < E:CIC OF BDA ;AS 9ALANCIN; EACUATION (EA%

Tan? %eig@tA % $' in 2'"2 !!

Tan? 5idt@A 5 *).)* in 2)'' !!

Tan? 6engt@A 6 a0 (@t$% 3.3"8 in

(@t$% )*+*,! psi

-s per Ta?le ##.- Ca3e No.#d

!1s2

?g1!"

7 liFg%7!ax8'.=> 9endin 3t4e33+ (qb2)/ t2

4

a

4

4

4


5/29

SIDE ALL (#% DESI;N CALCULATION RESULTS

TAN7 NO. < TR:6,$

:ROBECT NO. E:CIC OF BDA ;AS 9ALANCIN; EACUATION (EA%

T@erefore A Consider Gorst condition of part ( and part 2

At Center,

Ma0i>=> De1lection >a0 (@t#% >a0 (@t$%

(.


6/29

SIDE ALL (#% STIFFENER LOCATION

TAN7 NO. < TR:6,$



7/29


8/29

REACTION FORCE DESI;N CALCULATION

TAN7 NO. < TR:6,$


Calc of nifor! distriuted load 758 t@at act upon @ori&ontal > Lertical stiffener

A is giLen K eloG for!ula

5 R !ax 7Plate 3(8 R !ax 7Plate 328 12

5 Rp( Rp2 12

G@ere R is calc ased on Roar? /or!ulaA Tale ((.) Case No.(a

%EI9%T sd Gall (

( (''' (''' #,,, @)

2 (''' ;'' 5*, @"

" (''' """ *,, @2

) (''' 2;' $*, @(

; (''' 2'' $*,

LEN;TK

# #*,, #*,,

2 #*,,


9/29

SIDE ALL (#% KORIONTAL STIFFENER CALCULATION (Majo4 3ti11ene4%

TAN7 NO. < TA!)$,

SEAATER 9UFFER TAN7

Maxi!u! ending !o!ent occurs at t@e point G@ere dM1dx ' and s@ear force is &eroA

t@at isA at t@e !iddle of t@e ea!.

6 2''' !!


10/29

SIDE ALL (#% ERTICAL STIFFENER CALCULATION

TAN7 NO. < TR:6,$

:ROBECT < S7O :i@eline3 & Facilitie3 Rej=enation :4oject < 9A:9

6 2'"2.' !! $'.'' in

,RE/0 l1in ($''.' !! a0 '.''("'* x 56)

55a

6

5


11/29

SIDE ALL ($% ERTICAL STIFFENER CALCULATION ( >ino4 3ti11ene4%

TAN7 NO. < TA!)$,

SEAATER 9UFFER TAN7

;.


12/29

,.,,,! 61"#' ,.,6!* in O.7

The4e1o4e the 3ie =3ed i3 ade=ate.


13/29

SIDE ALL ($% DESI;N CALCULATION (:a4t #%

TAN7 NO. < TR:6,$


Tan? %eig@tA % $' in 2'"2 !!

Tan? 5idt@A 5 *).)* in 2)'' !!

Tan? 6engt@A 6 => De1lection+ t12 '.(($ in

3'.'"

>a0 (@t#% 0.03 in

(@t#% -+)"6 psi

-s per Ta?le ##.- Ca3e No.#a

Rectangular plate, all edges simply supported, uniform over entire plate

!1s2

?g1!"

liFg%

N1!2

-(qb4)/Et3

Ma0i>=> 9endin 3t4e33+ (qb2)/ t2

4

a

4

4

4


14/29

SIDE ALL ($% DESI;N CALCULATION (:a4t $%

TAN7 NO. < TR:6,$


Tan? %eig@tA % ;* in (;'' !!

Tan? 5idt@A 5 ;*.'# in (;'' !!

Tan? 6engt@A 6 a0 (@t$% 0.01 in

(@t$% #+#5" psi

-s per Ta?le ##.- Ca3e No.#e

Rectangular plate, all edges simply supported, it! load increasing uniformly along idt!

!1s2

?g1!"

7 liFg%7!ax8'.=> 9endin 3t4e33+ (qb2)/ t2

4

a

4

4

4


15/29

SIDE ALL ($% DESI;N CALCULATION RESULTS

TAN7 NO. < TR:6,$


T@erefore A Consider Gorst condition of part ( and part 2

At Center,

Ma0i>=> De1lection >a0 (@t#% >a0 (@t$%

'.'" '.'(

,.,- in

G@ere t12 '.(($ in

+ince +um of #a$ %eflection 5 t'2 6 .

(@t#%

(@t$%

)A"$* (A(


16/29

SIDE ALL ($% STIFFENER LOCATION

TAN7 NO. < TR:6,$



17/29

SIDE ALL ($% KORIONTAL STIFFENER CALCULATION (>ino4 3ti11ene4%

TAN7 NO. < TR:6,$


Maxi!u! ending !o!ent occurs at t@e point G@ere dM1dx ' and s@ear force is &eroA

t@at isA at t@e !iddle of t@e ea!.

6 2*'." !! ((.)" in

#;.2) l1in #''.' !! 2".# in

6oad F $.5!$ psi

unit load 5 F x psi

!*.$- l1in

use /B ;' x $

((.)" in

9endin Mo>ent

As per /ale 8.1 Case 2e of Roars )niform load on entire span*

-t x 612 ;.a0

M>a0

' 3ti11ene4

alloGale

!ax

7;56)8

55a

6

5


18/29

SIDE ALL ($% ERTICAL STIFFENER CALCULATION

TAN7 NO. < REF8

:ROBECT < REF8

6 ,RE/0 !! ,RE/0 in

,RE/0 l1in ,RE/0 !! ,RE/0 in

6oad F REF8 psi

unit load 5 F x psi

REF8 l1in

use /B ;' x $

,RE/0 in

9endin Mo>ent

As per /ale 8.1 Case 2d of Roars )niformly increasing load* -t x '.;)$6 ,RE/0 in

Maxi!u! !o!entA

NAME/ l3in 7 6 ,RE/0 in 8

C@ec?ing 4ection Modulus of 4tiffener reFuired

M1I

%enceA 7I1K8 reFuired M1K

,N-ME

,N-ME

-lloGale 4ection Modulus of 4tiffener reFuired

7I1K8 reFuired NAME/

U3in F9 *, 0 "

I1K 7stiffener8 ,.-,* ,N-ME 7I1K8 reFuired

The4e1o4e+ Ma0 ?endin 3t4e33

!ax psi ,N-ME

De1lection

As per /ale 8.1 Case 2d of Roars )niformly increasing load*

-t x '.;2;6 ,N-ME in

EI

NAME/ ,RE/0 REF8 in REF8

REF8

M!ax '.'2(;56

2

/K

in"

in"

H>a0

M>a0

' 3ti11ene4

alloGale

>a0 '.''("'* x 56)

55a

6

5


19/29

SECTIONAL STIFFENER :RO:ERTIES CALCULATION

TAN7 NO.

Documents

CIS EVA(SideWall) 6320 Sdwl 01