Elshcon - Cameron Transportation Seafastening and Barge Stability Report

7/25/2019 Elshcon - Cameron Transportation Seafastening and Barge Stability Report

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CAMERON COMPRESSORS PACKAGESTRANSPORTATION AND SEAFASTENING DESIGN,

BARGE STABILITY ANALYSISREPORT

Document Number Rev. P!e No.

PEL"CAM"REP"#$"%$#&"$$$$# 0 2 of 37

RE'. DATE DESCRIPTION PREPARED

BY

C(ECKED BY APPRO'ED

BY

CAMERON

RE'IE)

0 03 Oct 2015 Issued for Review L. Luis Raphael G. Okoyo

ELSHCON NIGERIA LTD. - ENERGY SERVICES PROVIDER

DOC*MENT NO. PEL"CAM"REP"#$"%$#&"$$$$#

This docum!" co!"#i!s i!fo$m#"io!% &hich is '$o'$i"#$( "o Cameron and Elshcon Nigeria Ltd.. Thisi!fo$m#"io! is "o ) h*d i! co!fid!c. Disc*osu$% $'$oduc"io!% o$ o"h$ us of "his docum!" is '$ohi)i"d&i"hou" "h '$io$ &$i""! co!s!" of both parties.






PEL"CAM"REP"#$"%$#&"$$$$# 0 3 of 37

Table of Contents

ABBRE'IATIONS.......................................................................................................................................

E+EC*TI'E S*MMARY..........................................................................................................................

# INTROD*CTION.................................................................................................................................

#.# PROECT BACKGRO*ND.................................................................................................................. ..........

#.% CAMERON -CASES-......................................................................................................................................

#. OBECTI'E.................................................................................................................................................... ..

% REFERENCES, CODES AND STANDARDS.....................................................................................

%.# REFERENCES....................................................................................................................................... ......... ..

%.% CODES AND STANDARDS.............................................................................................................................

%.%.# INTERNATIONAL STANDARDS........................................................................................... ......... .....

%.%.% COMPANY STANDARDS.......................................................................................................................

%. ORDER OF PRECEDENCE............................................................................................................................

DESIGN BASIS.....................................................................................................................................

/ BARGE ANALYSIS...............................................................................................................................

/.# CALC*LATION OF (YDROSTATIC DATA....................................................................................... ........

/.#.# DISPLACEMENT AND DRAFT 0LIG(T CONDITION1.................................................................##

/.#.% CENTER OF GRA'ITY, CENTER OF B*OYANCY AND *NIT IMMERSION..........................#%

/.#. *NIT IMMERSION...............................................................................................................................#

/.% (YDROSTATIC DATA 0LOADED CONDITION1........................................................................... ..........#

/.%.# *NBALLASTED......................................................................................................................... ......... ..#

/.%.% BALLAST................................................................................................................................................#/

/.%. INCLINED STABILITY........................................................................................................................#/

& LOADO*T AND TRANSPORTATION PLAN.................................................................................#2

&.# DESCRIPTION OF CARGO................................................................................................................ .........#2

&.% MET(OD FOR DESIGN AND ANALYSIS............................................................................................ .....#2

&. MODEL INP*TS.............................................................................................................................................#3

&..# LOAD CASES.........................................................................................................................................#3






PEL"CAM"REP"#$"%$#&"$$$$# 0 + of 37

&./ ANALYSIS O*TP*T......................................................................................................................................#4

&./.# LOADS S*MMARY.......................................................................................................................... ....#4

&./.% REACTION FORCES...........................................................................................................................%$

&./. P*NC(ING S(EAR 0OINTCAN1 C(ECK.....................................................................................#

2 CONCL*SIONS AND RECOMMENDATIONS.............................................................................. %






PEL"CAM"REP"#$"%$#&"$$$$# 0 , of 37

Abbrev5t5on6

AI A!erica" etroleu! I"stitute

AI#$ A!erica" I"stitute of #teel $o"structio"

A%# A!erica" %eldi"& #ociety

$'()* $o!pressio" with )e"di"& +#A$# output a,,reviatio"-

$G +or $oG- $e"ter of &ravity

I.. I"side dia!eter

G' 'etace"tric hei&ht / vertical dista"ce ,etwee" the co!,i"ed ce"ter of

&ravity a"d the !etace"ter which is a !easure of vessel sta,ility

) ei&ht of ce"ter of ,uoya"cy a,ove keel

G ei&ht of ce"ter of &ravity a,ove keel

' ei&ht of !etace"ter a,ove keel

LA)4$ Lateral orsio"al )uckli"& with "o Aial Load +#A$# output

a,,reviatio"-

LO$A Local $apacity +#A$# output a,,reviatio"-

O.. Outside dia!eter

4$ 4"ity $heck ratio






PEL"CAM"REP"#$"%$#&"$$$$# 0 of 37

E7ecut5ve Summr8

6lshco" *i&eria Li!ited has ,ee" co"tracted to tra"sport 3 7 co!pressor packa&es +cases- fro!

O""e to u"u worksite.

hese cases are proposed to ,e tra"sported via a car&o ,ar&e with a ra!p at the ,ow for roll/

o"8roll/off access ,y a self/propelled !odular truck +#'-. he cases are to ,e loaded o"

prefa,ricated cradles o" the ,ar&e deck to allow a" #' vehicle to ,ri"& the cases a"d placed

the! directly over the cradles / "o cra"es will ,e "eeded for the ,ar&e o"loadi"& a"d offloadi"&

operatio"s.

4po" arrival at the fi"al desti"atio" the cradles were desi&"ed for a hei&ht that will e"a,le a"

#' to co!forta,ly &o u"der the cases pick the! up a"d the" !ove the! out of the ,ar&e

throu&h the ra!p the" tra"sport the! to the fou"datio" locatio" where a cra"e will ,e a,le to

u"load the!.

he ,ar&e chose" ,y the clie"t is the 6*L 'iracle !easuri"& 90 !eters i" le"&th 12 !eters

across a"d 2.5 !eters full hull depth. *o hydrostatic data has ,ee" provided o" this ,ar&e.

$alculatio"s show that the ,ar&e will have satisfactory sta,ility a loaded draft of a,out 1 !eter

a"d a loaded displace!e"t of a,out 913 !etric to""es. he port a"d star,oard forward a"d aft

,allast ta"ks !ay ,e filled for additio"al ,allast althou&h that will reduce the free,oard sli&htly.

he three co!pressor cases will ,e loaded i" li"e o" the ,ar&e ce"terli"e.

he cradles were desi&"ed to spread the co"ce"trated loads fro! the stool colu!"s o"to the

i"ter"al ,ulkheads of the ,ar&e to provide a stro"&er ,ackup support for the car&o. I" additio"

the car&o is sta,ili:ed ,y ,raci"& to port a"d star,oard o" the ,ar&e deck for seafaste"i"&.

*o vessel !otio" data has ,ee" provided. )ased o" eperie"ce it is assu!ed that the !ai!u!

roll acceleratio" is 0.22 & the !ai!u! pitch acceleratio" is 0.15 & a"d the !ai!u! heave

acceleratio" is 0.05 &.






PEL"CAM"REP"#$"%$#&"$$$$# 0 7 of 37

# INTROD*CTION

#.# PROECT BACKGRO*ND

6lshco" *i&eria Li!ited has ,ee" co"tracted to tra"sport 3 7 co!pressor packa&es

+cases- fro! O""e to u"u worksite.

hese cases are proposed to ,e tra"sported via a car&o ,ar&e with a ra!p at the ,ow for

roll/o"8roll/off access ,y a self/propelled !odular truck +#'-. he cases are to ,e

loaded o" prefa,ricated cradles o" the ,ar&e deck to allow a" #' vehicle to ,ri"& the

cases a"d placed the! directly over the cradles / "o cra"es will ,e "eeded for the ,ar&e

o"loadi"& a"d offloadi"& operatio"s.

4po" arrival at the fi"al desti"atio" the cradles were desi&"ed for a hei&ht that will

e"a,le a" #' to co!forta,ly &o u"der the cases pick the! up a"d the" !ove the!

out of the ,ar&e throu&h the ra!p the" tra"sport the! to the fou"datio" locatio" where a

cra"e will ,e a,le to u"load the!.

#.% CAMERON -CASES-

6ach $a!ero" $ase co"sists of a co!pressor packa&e used for oil a"d &as eploratio".

6ach $ase wei&hs 5311; k& a"d !easures 12.19 !eters i" le"&th 9.<5 !eters i" width

9.== !eters i" hei&ht.

*o structural details of the e>uip!e"t skid fra!es have ,ee" provided for each case o"ly

the i"for!atio" that they are wood crates.

#. OBECTI'E

he purpose of this docu!e"t is to prese"t the desi&" report for the tra"sportatio" cradles

for each case the seafaste"i"& layout a"d the a"alysis of the ,ar&e sta,ility

displace!e"t draft a"d !etace"tric hei&ht.






PEL"CAM"REP"#$"%$#&"$$$$# 0 of 37

% REFERENCES, CODES AND STANDARDS

%.# REFERENCES

%.% CODES AND STANDARDS

I" &e"eral the detailed desi&" was co"ducted i" co!plia"ce with applica,le $odes a"d

#ta"dards ,i"di"& o" the offshore oil a"d &as i"dustry a"d pro?ect specificatio"s.

All e"&i"eeri"& works shall co!ply with *atio"al a"d I"ter"atio"al #ta"dards. As !uch

as possi,le the "ew desi&" uses pipes ,ea!s a"d plate si:es a"d !ethods co!!o"ly

used i" the i"dustry.

%.%.# INTERNATIONAL STANDARDS

• AI#$ #teel $o"structio" 'a"ual 7 A# 13th 6ditio".

• AI Reco!!e"d ractice 2A

•)ritish #ta"dards

• A*#I8A%# 1.181.1'/200@ #tructural %eldi"& $ode

%.%.% COMPANY STANDARDS

• *o releva"t co!pa"y sta"dards are i"voked

%. ORDER OF PRECEDENCE

I" case of co"flict the Re&ulatio"s $odes a"d #ta"dards shall ,e applied i" the

followi"& priority order

a- *i&eria" Gover"!e"t Le&islatio".

,- ro?ect #pecificatio" a"d ata #heets.

c- $o!pa"yBs #pecificatio"s a"d #ta"dards.

d- I"dustry #ta"dards.

e- $o"tractor $odes a"d %orki"& #ta"dards.






PEL"CAM"REP"#$"%$#&"$$$$# 0 / of 37

DESIGN BASIS

he followi"& ta,le descri,es the desi&" a"d a"alysis para!eters used as ,asis for

calculatio"s

DESIGNATION 'AL*E *NITS

Or5entt5on C D E Glo,al $oordi"ate #yste!F (E poi"ts

upward

u"its !eter

S t e e 9 P r o : e r t 5 e 6

#teel e"sity =.<9; '. o""es8!

3

Dield #tress +y- 'ild steel +u"less otherwise i"dicated- 29.< k*8c!2

'odulus of 6lasticity 20103 k*8c!2

'odulus of Ri&idity +#hear 'odulus- =.=29103 k*8c!2

oisso"Bs Ratio 0.3 /

A 9 9 o ; b 9

e 6 'ai!u! allowa,le ,e"di"& stress 0.@@ y k*8c!2

'ai!u! allowa,le co!pressio" stress 0.@0 y k*8c!2

'ai!u! allowa,le shear stress 0.90 y k*8c!2

a,le 1 #teel esi&" para!eters

DESCRIPTION LENGT( 0m1 )IDT( 0m1 (EIG(T 0m1

)ar&e hull 90.0 12.0 2.5

)ar&e displace!e"t 230 !.to""es

raft 0.5 !

I"ter"al structure 5 tra"sverse ,ulkheadsF o"e lo"&itudi"al ,ulkhead o" ce"terli"e

$o!part!e"tatio" 12 ,allast ta"ks / @ o" port side a"d @ o" star,oard side.

e"sity of water #altwater H 1025 k&8!3

reshwater H 1000 k&8!3

a,le 2 )ar&e para!eters






PEL"CAM"REP"#$"%$#&"$$$$# 0 01 of 37

/ BARGE ANALYSIS

/.# CALC*LATION OF (YDROSTATIC DATA

he chose" ,ar&e is 6*L 'iracle. *o specific hydrostatic data for this ,ar&e has ,ee"

provided ,y the custo!er.

he ,ar&e profile a"d pla" views are show" i" the followi"& fi&ures.

i&ure 1 rofile view of 6*L 'Iracle ,ar&e at ce"terli"e

i&ure 2 la" view of 6*L 'Iracle ,ar&e

4si"& the data show" i" the drawi"& of the ,ar&e the followi"& additio"al hydrostatic

data was calculated usi"& ,asic pri"ciples of "aval architecture

• isplace!e"t +li&ht co"ditio"-

• raft +li&ht co"ditio"-

• $e"ter of &ravity +G- +li&ht co"ditio"-

• $e"ter of ,uoya"cy +)- +li&ht co"ditio"-

• I!!ersio" ,aseli"e






PEL"CAM"REP"#$"%$#&"$$$$# 0 00 of 37

• isplace!e"t +loaded co"ditio"-

• raft +loaded co"ditio"-

• $o!,i"ed $OG +G- +loaded co"ditio"-

• isplace!e"t of $e"ter of )ouya"cy whe" i"cli"ed 10 de&rees +ort8#t,d-

• 'etace"ter elevatio" +'-

• 'etace"tric hei&ht +G'-



CAMERON COMPRESSORS PACKAGES

TRANSPORTATION AND SEAFASTENING DESIGN,BARGE STABILITY ANALYSIS

REPORT


PEL"CAM"REP"#$"%$#&"$$$$# 0 02 of 37

/.#.# DISPLACEMENT AND DRAFT 0LIG(T CONDITION1

he followi"& ta,le uses the i"for!atio" &ive" i" the ,ar&e drawi"& to esti!ate the total wei&ht of the vessel. he" usi"& Archi!edes

pri"ciple a draft ca" ,e calculated for the deadwei&ht +or displace!e"t- of the ,ar&e.

PART

DESCRIPTI

ON

PLATE

THICKN

ESS

(mm)

SHELL STIFFENERS FRAME COLUMNS BOTTOM

PLATE

AREA

(m2)

DECK

PLATE

AREA

(m2)

SIDE

SHELL

STARBD

(m2)

SIDE

SHELL

PORT (m2)

SIDE

SHELL

BOW (m2)

SIDE

SHELL

STERN

(m2)

TRANSVE

RSE BHDS

(m2)

LONGIT.

BHD (m2)

No. of

BOTTOM

STIFFENE

RS

No. of

DECK

STIFFENE

RS

No. of STBD

STIFFENER

S

No. of

PORT

STIFFENE

RS

No. of

BOW

STIFFENE

RS

No. of

STERN

STIFFENE

RS

No. of

INTERNAL

BHD

STIFFENERS

DIMENSION

S (mm)

UNIT WGT.

(kgm)

DIMENS.

(mm)

UNIT WGT.

(kgm)

Bottom 10 100x100

x8

19.3 414 18

Deck 10 100x100

x8

19.3 480 18

Stbd & Port

Sides

10 100x 100

x8

19.3 93.125 93.125 3 3

Bow 10 100x100

x8

19.3 47.28 18

Stern 10 100x100

x8

19.3 45 18

Trns!erse

B"ds.

8 100x100

x#

15 150 18

$on%itd.

B"ds.

8 100x100

x8

19.3 93.125 3

Deck 300x100 54.2





REPORT


PEL"CAM"REP"#$"%$#&"$$$$# 0 03 of 37

'rmes x13

Bottom

'rmes

300x100

x8

32

Side S"e((

'rmes

300x100

x8

32

'rme

)o(mns

273x9 #0.31

WEIGHTS

(kg)

!2"#$.

%&

!&'&$.

""

&!%#."! &!%#."! !&.%! !$!2.%& "&%#".! $"&.$" #$.

!

!#' 2!' 2!' !$".

'

!%2.&

$

$'#

a,le 3 )reak dow" of ,ar&e structural ele!e"ts to arrive at a deadwei&ht






PEL"CAM"REP"#$"%$#&"$$$$# 0 0+ of 37

eadwei&ht of the ,ar&e H displace!e"t H J wei&ht+struct. ele!e"ts- 81000 k&8to""e

)ar&e displace!e"t H 22;.< !etric to""es

he draft is a !easure of how !uch the hull si"ks i" the water for a &ive" displace!e"t.

Archi!edes pri"ciple e>uates the volu!e of displaced water ,ei"& e>ual to the wei&ht of

the floati"& ,ody.

raft H +isplace!e"t 8 Kwater - +hull pla"ar area-

raft H 22;<00 8 1025- +12 ! 3=.5 !- H 0.50 !

$o"se>ue"tly the free,oard which is the hei&ht of the side shell a,ove the water level is

epthhull / raft H 2.5 / 0.5 H 2.0 !

/.#.% CENTER OF GRA'ITY, CENTER OF B*OYANCY AND *NIT IMMERSION

he ,ar&e ce"ter of &ravity +$oG- is i!porta"t i" sta,ility ,ecause it is the ce"ter of

!ass a"d i"ertia a"d whe" co!pared to the locatio" of the !etace"ter is a crucial factor

i" !ai"tai"i"& the vessel upri&ht a"d sta,le.

I" this case si"ce the side shell plati"& thick"esses a"d stiffe"er layouts are sy!!etrical

a,out ce"terli"e o"ly the area of the deck plati"& a"d the area of the ,otto! plati"& were

used to calculated the G +hei&ht of the $oG fro! the ,ar&e keel-.

COMPONENT )EIG(T

0<!1

DISTANCE FROM

BOTTOM OF (*LL

0m1

PROD*CT OF )GT. 7

DIST

0<!.m1

eck lati"& 3=@=5.99 2.9;5 ;9000.22

)otto! lati"& 329;5.0= 0.005 [email protected]<

OAL# =01=0.51 1.391;= ;91@2.=0

a,le 9 $alculatio" of the $oG locatio" i" the tra"sverse vertical pla" ,y the !o!e"t !ethod

= he G H ;91@2.= 8 =01=0.51 H 1.391; !






PEL"CAM"REP"#$"%$#&"$$$$# 0 0, of 37

i&ure 3 Graphical represe"tatio" of keel +- ce"ter of ,uoya"cy +)- a"d ce"ter of &ravity+$G- i" the tra"sverse vertical pla"e of the ,ar&e hull

/.#. *NIT IMMERSION

*or!ally a rate of vessel i!!ersio" i" water is &ive" i" ter!s of force8le"&th of

i!!ersio" typically to"s8i"ch.

he calculated u"it i!!ersio" rate is the displace!e"t 8 draft.

he esti!ated to""es8i"ch i!!ersio" H 11.=2

/.% (YDROSTATIC DATA 0LOADED CONDITION1

/.%.# *NBALLASTED

%he" the three $ases co!e o",oard the ,ar&e is loaded.

I" this co"ditio" / without ,allast / the followi"& cha"&es will occur

• isplace!e"t +loadedF "o ,allast- H 22;.@ ( 1<3.2@ H 913.0@ !etric to""es

• raft +loadedF "o ,allast- H 0.; !eters

• Gco!,i"ed H 3.= !eters

• ) H 0.95 !eters

• ' H 1<.1 !eters

• G' H ' / G H 1<.1 / 3.= H 19.9 !eters

#ta,ility is "ot a pro,le!M






PEL"CAM"REP"#$"%$#&"$$$$# 0 0 of 37

/.%.% BALLAST

)allast is o"ly reco!!e"ded duri"& the o"loadi"& a"d offloadi"& operatio"s to !ai"tai"

deck level. Otherwise addi"& ,allast duri"& the voya&e will lower the co!,i"ed ce"ter

of &ravity thus i"creasi"& the !otio"/i"duced acceleratio"s acti"& o" the car&o.

uri"& o"loadi"& a"d offloadi"& operatio"s it is reco!!e"ded that the ,ow ,allast ta"ks

o" port a"d star,oard side ,e used to help keep the ,ar&e o" eve" keel. As the first a"d

seco"d cases are placed at the aft !ost positio"s o" the ,ar&e deck the forward ,allast

ta"ks should ,e ,allasted to !ai"tai" eve" keel.

O"ce the third case is i" place a"d the #' has !oved off the ,ar&e the ,allast should

,e re!oved a"d all ta"ks should ,e co!pletely e!pty to preve"t water sloshi"& arou"d

i" the ta"ks a"d causi"& a free surface effect which would i"crease the vessel !otio"s.

/.%. INCLINED STABILITY

If the ,ar&e lists +to port or star,oard- up to 10 de&rees the sta,ility is still ok a"d it

develops a ri&hti"& !o!e"t of approi!ately =13.5 to""es.!eters.

he !etace"ter ca" ,e esti!ated as show" i" the fi&ure ,elow






PEL"CAM"REP"#$"%$#&"$$$$# 0 07 of 37

i&ure 9 Nessel sta,ility whe" listi"& 10 de&rees tra"sversely






PEL"CAM"REP"#$"%$#&"$$$$# 0 0 of 37

& LOADO*T AND TRANSPORTATION PLAN

&.# DESCRIPTION OF CARGO

he car&o co"sists of three wood crates each co"tai"i"& a &as co!pressor.

he followi"& ta,le shows the particulars for each of the cases

$A#6

*o.

I'6*#IO*# +!eters- %6IG

+k&-

%6IG

+k*-L6*G %I 6IG

1 12.19 9.<5 9.== 5311;.00 520.;2

2 12.19 9.<5 9.== 5311;.00 520.;2

3 12.19 9.<5 9.== 5311;.00 520.;2

a,le 5 ata provided for each $a!ero" $ase

&.% MET(OD FOR DESIGN AND ANALYSIS

he desi&" a"d a"alysis of the loadout a"d seafaste"i"& sche!e for the tra"sportatio" of

the three cases o" the deck of a towed ,ar&e was do"e usi"& a worldclass structural

a"alysis software called #A$# fre>ue"tly used for this purpose.

i&ure 5 Niews of the #A$# !odel / erspectiveF #ide 6levatio"F 6"d 6levatio"






PEL"CAM"REP"#$"%$#&"$$$$# 0 0/ of 37

&. MODEL INP*TS

he !odel co"sist of ?oi"ts a"d !e!,er ele!e"ts. he ?oi"ts defi"e the &eo!etry of the

structure he !e!,er ele!e"ts defi"e the types a"d si:es of structural ,ea!s pipes a"d

plates.

he !odel i"cludes the followi"& structural !e!,ers as eplai"ed i" the followi"& ta,le

6#$RIIO* P4A*ID D6 IA'66R

+i"ches-

%ALL .

+!!-

#66L

GRA6

R6'AR#

$olu!"s 19 ipe <.@25 <.1< 'ild +A3@ or

e>ual-

$ap )ea! 2 62@0AA 'ild +A3@ or

e>ual-

%ide la"&e

)races 10 ipe 5.5@3 @.55 'ild +A3@ or

e>ual-

ra"sverse

)rackets

@ 4A200 'ild +A3@ or

e>ual-

$ha""el

Gussets lates @ late 12.5 'ild +A3@ or

e>ual-

ou,ler lates 20 late 12.5 'ild +A3@ or

e>ual-

a,le @ 'odel !e!,er ele!e"ts properties i"put

&..# LOAD CASES

he !odel i"cludes ,asic a"d co!,i"atio" load cases to a"alyses differe"t sce"arios the

vessel !ay ,e eposed to duri"& the sea voya&e.

he followi"& ta,le details all the !odel load cases.

LOA $A#6 6#$RIIO* D6 A$OR IR6$IO* R6'AR#






PEL"CAM"REP"#$"%$#&"$$$$# 0 21 of 37

*o.

1 eadwei&ht #tatic 1.05 Nertical +/E-

2 eadwei&ht y"a!ic 0.15 ori:o"tal +C- itchi"&

3 eadwei&ht y"a!ic 0.22 ori:o"tal +D- Rolli"&

5 22.9/k"ot %i"d #tatic 1.0 ori:o"tal +C- 0.0 de&.

@ 22.9/k"ot %i"d #tatic 1.0 ia&o"al or. +C

Q D-

95 de&.

= 22.9/k"ot %i"d #tatic 1.0 ori:o"tal +D- ;0 de&.

a,le = )asic Load $ases i" the !odel

$O')I*6

LOA $A#6

*o.

LOA $A#6

*o.

A$OR )A#I$ LOA

$A#6 *o.

A$OR )A#I$ LOA

$A#6 *o.

A$OR

10 1 1.00 2 1.00 5 1.00

11 1 1.00 2 1.00 @ 1.00

12 1 1.00 3 1.00 @ 1.00

13 1 1.00 3 1.00 = 1.00

100 1 1.05 2 1.00 3 1.00

110 100 1.00 5 1.00 / /

120 100 1.00 @ 1.00 / /

130 100 1.00 = 1.00 / /

a,le < $o!,i"ed Load $ases i" the !odel






PEL"CAM"REP"#$"%$#&"$$$$# 0 20 of 37

&./ ANALYSIS O*TP*T

&./.# LOADS S*MMARY

)asic Loads

Lo>

C6e No.

F7 F8 F? M7 M8 M?

k* k* k* k*/! k*/! k*/!

1 0.00 0.00 /@2@.=0 /1503.;0 /9=05.=0 0.00

2 ;9.00 0.00 0.00 0.00 2<9.=0 /225.@0

3 0.00 13=.<= 0.00 /91=.@0 0.00 /1035.30

5 1.<2 0.00 0.00 0.00 2.30 /9.90

@ 1.2; 2.<= 0.00 /3.30 1.@0 /23.;0

= 0.00 9.0@ 0.00 /9.=0 0.00 /2;.90

a,le ; )asic Load $ases / applied forces a"d !o!e"ts

$o!,i"ed Loads

Lo>

C6e No.

F7 F8 F? M7 M8 M?

k* k* k* k*/! k*/! k*/!

10 ;5.<3 0.00 /@2@.=0 /1503.;0 /991<.=0 /230.00

11 ;5.2; 2.<= /@2@.=0 /150=.20 /991;.90 /29;.50

12 1.2; 190.=9 /@2@.=0 /1;29.<0 /9=09.10 /105;.10

13 0.00 191.;3 /@2@.=0 /1;[email protected] /9=05.=0 /10@9.=0

100 ;9.00 13=.<= /@5<.03 /1;;@.=0 /9@[email protected] /12@0.<0

110 ;5.<3 13=.<= /@5<.09 /1;;@.=0 /[email protected] /[email protected]

120 ;5.2; 190.=9 /@5<.09 /2000.00 /9@59.=0 /12<9.=0

130 ;9.00 191.;3 /@5<.03 /2001.90 /9@[email protected] /12;0.30

a,le 10 $o!,i"ed Load $ases / applied forces a"d !o!e"ts






PEL"CAM"REP"#$"%$#&"$$$$# 0 22 of 37

&./.% REACTION FORCES

he reactio"s forces are o" the deck of the ,ar&e u"der the colu!"s a"d the ,races.

he C/aiss i" the !odel poi"ts towards the ,ar&e ,ow.

i&ure @ oi"ts represe"ti"& all co""ectio"s ,etwee" the colu!"s a"d ,races o" the ,ar&e deck.

+*ote oi"ts 0031 a"d 0000 are o"ly for purposes of defi"i"& directio"s i" the !odel a"d are "ot

colu!"s.-

#A$#/IN #D#6' R6A$IO* OR$6#

OI* LOA

$A#6

$OOR.

#D#. SSSSSSS OR$6# SSSSSSS

C D E

+*- +*- +*-

005; 1 GLO) /0.0; 1.@;; /9.1<5

O)LP /0.955 1.095 /9.3=1

2 GLO) 0.23< /0.252 0.99<

O)LP 0.2<= /0.131 0.9=1

3 GLO) /0.2@9 2.<;< /5.05

O)LP /0.<<5 2.09= /5.3<5

5 GLO) 0.025 /0.002 0.009






PEL"CAM"REP"#$"%$#&"$$$$# 0 23 of 37

O)LP 0.029 0.009 0.003

@ GLO) 0.015 0.05 /0.091

O)LP 0.009 0.095 /0.09<

= GLO) /0.003 0.0=2 /0.0@2

O)LP /0.01; 0.0@ /0.0=1

10 GLO) 0.1=9 1.99@ /3.=33

O)LP /0.193 0.;1; /3.<;=

11 GLO) 0.1@9 1.9;= /3.==<

O)LP /0.1@9 0.;@ /3.;9;

12 GLO) /0.33; 9.@9= /;.2=@

O)LP /1.33@ 3.13< /;.<05

13 GLO) /0.35= 9.@= /;.2;=

O)LP /1.35< 3.152 /;.<2<

100 GLO) /0.12 9.931 /<.;;@

O)LP /1.0=5 3.019 /;.509

110 GLO) /0.0;5 9.92; /<.;;2

O)LP /1.051 3.01< /;.501

120 GLO) /0.105 9.9< /;.03=

O)LP /1.0=1 3.05; /;.553

130 GLO) /0.123 9.503 /;.05<

O)LP /1.0;9 3.0=9 /;.5=@

0035 1 GLO) /1.<@; /3.5=9 /5;.32@

2 GLO) =.0;@ 0.;2 15.9=1

3 GLO) 2.199 12.1;= /20.11

5 GLO) 0.125 0.002 0.12<

@ GLO) 0.119 0.1;= /0.05;

= GLO) 0.03= 0.2== /0.212

10 GLO) 5.352 /2.@52 /93.=2=

11 GLO) 5.391 /2.95@ /93.;19

12 GLO) 0.3<; <.<21 /=;.9;@

13 GLO) 0.312 <.;01 /=;.@9<

100 GLO) =.2=< ;.3@5 /@@.;32

110 GLO) =.903 ;.3@= /@@.<03

120 GLO) =.3;2 ;.5@2 /@@.;;1

130 GLO) =.319 ;.@92 /@=.199

003@ 1 GLO) 0.952 /<.=<5 /15.==2

2 GLO) 5.=05 1.5@2 1.@5<






PEL"CAM"REP"#$"%$#&"$$$$# 0 2+ of 37

3 GLO) 0.=;1 <.<<@ /9.2;<

5 GLO) 0.1 0.00< 0.013

@ GLO) 0.0=@ 0.1<@ /0.029

= GLO) 0.00= 0.255 /0.09=

10 GLO) @.25= /=.21@ /19.101

11 GLO) @.233 /=.03= /19.13<

12 GLO) 1.31; 0.2<= /20.0;3

13 GLO) 1.251 0.35@ /20.11@

100 GLO) @.;=1 1.229 /1;.2

110 GLO) =.0=1 1.231 /1;.1<=

120 GLO) =.09= 1.90; /1;.229

130 GLO) @.;=< 1.9=; /1;.29@

003= 1 GLO) 9.3 /9.@<5 /1<.=22

2 GLO) ;.12= 0.50< 0.35

3 GLO) 1.215 =.;0= /9.2<@

5 GLO) 0.152 0.003 0.002

@ GLO) 0.11 0.15; /0.03

= GLO) 0.009 0.221 /0.095

10 GLO) 13.5=< /9.1=5 /1<.3=1

11 GLO) 13.53@ /9.01; /1<.903

12 GLO) 5.@29 3.3< /23.03;

13 GLO) 5.51< 3.993 /23.053

100 GLO) 19.<5@ 3.9;5 /23.5;9

110 GLO) 15.00< 3.9;< /23.5;2

120 GLO) 19.;@@ 3.@59 /23.@29

130 GLO) 19.<@ 3.=1@ /23.@3;

005< 1 GLO) /0.15; 5.223 /10.0@3

O)LP /1.=93 2.@2@ /10.<;2

2 GLO) 0.293 0.1;@ /0.3=2

O)LP 0.1=2 0.1=9 /0.92

3 GLO) /0.1@2 5.231 /;.=31

O)LP /1.=9< 2.=09 /10.5@;

5 GLO) 0.02< 0.001 /0.002

O)LP 0.02@ 0.00; /0.009

@ GLO) 0.01< 0.0<3 /0.0;1

O)LP /0.00< 0.0@3 /0.10=

= GLO) /0.003 0.11@ /0.12=






PEL"CAM"REP"#$"%$#&"$$$$# 0 2, of 37

O)LP /0.03< 0.0< /0.19=

10 GLO) 0.112 5.92 /10.93=

O)LP /1.595 2.<0; /11.31@

11 GLO) 0.102 5.502 /10.52@

O)LP /1.5< 2.<@2 /11.91;

12 GLO) /0.303 10.53= /1;.<<5

O)LP /3.5 5.3;3 /21.5@;

13 GLO) /0.329 10.5=1 /1;.;21

O)LP /3.53 5.91 /21.@0;

100 GLO) /0.0<5 10.;12 /20.@@;

O)LP /3.90= 5.@35 /22.92@

110 GLO) /0.05= 10.;12 /20.@=1

O)LP /3.3< 5.@99 /22.93

120 GLO) /0.0@< 10.;;9 /20.=@

O)LP /3.915 5.@;< /22.533

130 GLO) /0.0<< 11.02< /20.=;@

O)LP /3.995 5.=15 /22.5=3

0032 1 GLO) 2.29= /25.0@5 /105.509

2 GLO) =.=<; /0.@= /9.99;

3 GLO) /0.155 5.1<2 /20.231

5 GLO) 0.13; /0.009 /0.092

@ GLO) 0.0;2 0.1<< /0.155

= GLO) /0.00; 0.2= /0.1==

10 GLO) 10.1=5 /25.=3< /10;.;;5

11 GLO) 10.12< /25.59@ /110.10<

12 GLO) 2.1<9 /1;.@;9 /125.<;1

13 GLO) 2.0<3 /1;.@13 /125.;13

100 GLO) ;.;;3 /21.<05 /135.9@

110 GLO) 10.132 /21.<0; /135.502

120 GLO) 10.0<5 /21.@1= /135.@15

130 GLO) ;.;<5 /21.53@ /135.@3=

005= 1 GLO) /0.3=; 2.5=3 /=.0<;

O)LP /1.=0@ /1.0< /=.2=@

2 GLO) 0.1<1 0.3@; /0.<<<

O)LP /0.09= 0.013 /0.;==

3 GLO) /0.11< 2.30@ /5.1;3

O)LP /1.392 /0.3<; /5.50;






PEL"CAM"REP"#$"%$#&"$$$$# 0 2 of 37

5 GLO) 0.029 0.001 /0.009

O)LP 0.02 0.011 /0.01

@ GLO) 0.019 0.095 /0.09=

O)LP /0.012 0.023 /0.0@1

= GLO) /0.009 0.0@3 /0.0@2

O)LP /0.03= 0.021 /0.0==

10 GLO) /0.1=9 2.;93 /=.;<1

O)LP /1.=33 /1.05@ /<.2@3

11 GLO) /0.1<9 2.;<< /<.029

O)LP /1.=@5 /1.099 /<.315

12 GLO) /0.9<2 9.;29 /12.32;

O)LP /3.0@1 /1.99@ /12.<9@

13 GLO) /0.501 9.;92 /12.399

O)LP /3.0<@ /1.99= /12.<@2

100 GLO) /0.335 5.3== /13.525

O)LP /3.1< /1.50; /19.12@

110 GLO) /0.311 5.3=< /13.52;

O)LP /3.1@ /1.9;; /19.13@

120 GLO) /0.32 5.922 /13.5=1

O)LP /3.1;3 /1.9<= /19.1<=

130 GLO) /0.33; 5.99 /13.5<@

O)LP /3.21< /1.9<< /19.203

0005 1 GLO) /1.<13 3.555 /5;.3<=

2 GLO) =.00@ /0.;0@ 15.50<

3 GLO) /2.251 12.1<@ 20.0@=

5 GLO) 0.129 /0.001 0.12;

@ GLO) 0.05; 0.1;5 0.29

= GLO) /0.09 0.2== 0.211

10 GLO) 5.31= 2.@9= /93.=5

11 GLO) 5.253 2.<99 /93.@3;

12 GLO) /9.009 15.;3@ /3;.0<

13 GLO) /9.109 [email protected]< /3;.10;

100 GLO) 2.<52 15.013 /2@.=<1

110 GLO) 2.;=@ 15.012 /2@.@53

120 GLO) 2.;11 15.20< /[email protected]

130 GLO) 2.<12 15.2; /[email protected]=1

0033 1 GLO) /2.352 /9.0@@ /[email protected]






PEL"CAM"REP"#$"%$#&"$$$$# 0 27 of 37

2 GLO) @.;;2 /1.25= /2.005

3 GLO) /2.90< =.5@2 /5.513

5 GLO) 0.13 /0.011 /0.015

@ GLO) 0.0= 0.15< /0.05@

= GLO) /0.031 0.235 /0.0@9

10 GLO) 9.== /5.335 /2<.0=

11 GLO) 9.=1 /5.1@5 /2<.111

12 GLO) /9.@; 3.@59 /31.@1;

13 GLO) /9.=;1 3.=31 /31.@2<

100 GLO) 2.119 2.035 /39.<=1

110 GLO) 2.299 2.029 /39.<<@

120 GLO) 2.1<9 2.1;9 /39.;2=

130 GLO) 2.0<9 2.2= /39.;35

0039 1 GLO) /1.2=< /5.@=2 /30.<2

2 GLO) 9.;@9 /1.02= /9.12;

3 GLO) /2.@5 =.@1= /@.591

5 GLO) 0.0;@ /0.003 /0.039

@ GLO) 0.03 0.1<3 /0.0==

= GLO) /0.059 0.2@3 /0.0=5

10 GLO) 3.=<2 /@.=02 /39.;<9

11 GLO) 3.=1@ /@.515 /35.02=

12 GLO) /3.<;< 2.12; /3=.93<

13 GLO) /3.;<2 2.20< /3=.93@

100 GLO) 0.;=2 0.@35 /93.031

110 GLO) 1.0@< 0.@32 /93.0@@

120 GLO) 1.002 0.<1< /93.10<

130 GLO) 0.;1< 0.<;< /93.10@

000@ 1 GLO) 0.9;9 <.<02 /15.=<3

2 GLO) 5.@99 /1.5= 1.@@3

3 GLO) /0.<=3 <.<=3 9.2;3

5 GLO) 0.0;; /0.00< 0.013

@ GLO) 0.0@3 0.1=5 0.092

= GLO) /0.01 0.255 0.09=

10 GLO) @.23@ =.229 /19.10=

11 GLO) @.2 =.90= /19.0=<

12 GLO) /0.31= 1=.<9; /11.99<

13 GLO) /0.3; 1=.;2; /11.993






PEL"CAM"REP"#$"%$#&"$$$$# 0 2 of 37

100 GLO) 5.2<; [email protected] /10.@1@

110 GLO) 5.3<< [email protected]< /10.@03

120 GLO) 5.352 1@.=2 /10.5=9

130 GLO) 5.2=; 1@.< /10.5@;

0030 1 GLO) /0.0<9 /1.=09 /9.1;3

O)LP /0.95 /1.09; /9.3<

2 GLO) 0.231 0.25@ 0.959

O)LP 0.2< 0.135 0.9==

3 GLO) 0.2@ 2.<;< 5.05

O)LP 0.<<1 2.09< 5.3<5

5 GLO) 0.025 0.002 0.009

O)LP 0.029 /0.009 0.003

@ GLO) 0.02 0.052 0.09=

O)LP 0.03 0.09 0.053

= GLO) 0.003 0.0=2 0.0@2

O)LP 0.01; 0.0@ 0.0=1

10 GLO) 0.1=1 /1.99@ /3.=35

O)LP /0.19@ /0.;1< /3.;

11 GLO) 0.1@@ /1.3;@ /3.@;3

O)LP /0.19 /0.<=9 /3.<51

12 GLO) 0.1;@ 1.29= 0.;03

O)LP 0.9@1 1.03; 1.05=

13 GLO) 0.1< 1.2@= 0.;1;

O)LP 0.99; 1.05; 1.0=@

100 GLO) 0.903 1.3@5 1.101

O)LP 0.@<; 1.0<2 1.2@3

110 GLO) 0.92= 1.3@= 1.105

O)LP 0.=13 1.0=< 1.2@@

120 GLO) 0.922 1.91< 1.19<

O)LP 0.=1; 1.121 1.31@

130 GLO) 0.90@ 1.93= 1.1@3

O)LP 0.=0= 1.192 1.339

000= 1 GLO) 9.353 9.@<9 /1<.=3=

2 GLO) ;.05@ /0.9;; 0.3@2

3 GLO) /1.335 =.;3 9.2;

5 GLO) 0.151 /0.003 0.002

@ GLO) 0.101 0.155 0.033






PEL"CAM"REP"#$"%$#&"$$$$# 0 2/ of 37

= GLO) /0.00< 0.222 0.095

10 GLO) 13.5@ 9.1<3 /1<.3=9

11 GLO) 13.51 9.391 /1<.392

12 GLO) 3.11; 12.=@; /19.919

13 GLO) 3.01 12.<3@ /19.902

100 GLO) 12.2;2 12.39; /15.022

110 GLO) 12.992 12.39= /15.02

120 GLO) 12.3;3 12.509 /19.;<;

130 GLO) 12.2<9 12.5=2 /19.;==

0015 1 GLO) /0.@<< 2.2@1 /35.=91

2 GLO) 9.39< 0.15@ /@.101

3 GLO) /3.3< ;.0;= /<.91

5 GLO) 0.0<< 0.002 /0.05

@ GLO) 0.01 0.1<2 /0.11

= GLO) /0.0=5 0.255 /0.10@

10 GLO) 3.=9; 2.91; /91.<;1

11 GLO) 3.@= 2.5;; /91.;52

12 GLO) /9.05< 11.59 /99.2@1

13 GLO) /9.192 11.@13 /99.25=

100 GLO) 0.29@ 11.@2= /52.03;

110 GLO) 0.335 11.@2; /52.0<<

120 GLO) 0.25@ 11.<0; /52.19;

130 GLO) 0.1=2 11.<<2 /52.199

002; 1 GLO) /0.15@ /5.215 /10.0@

O)LP /1.=3< /2.@2 /10.<<<

2 GLO) 0.29 /0.219 /0.3<5

O)LP 0.1@3 /0.1<@ /0.93@

3 GLO) 0.1@1 5.22@ ;.=31

O)LP 1.=9@ 2.@;; 10.5@<

5 GLO) 0.02< /0.001 /0.002

O)LP 0.02@ /0.00; /0.009

@ GLO) 0.022 0.0<1 0.0<<

O)LP 0.09@ 0.05 0.101

= GLO) 0.003 0.11@ 0.12=

O)LP 0.03< 0.0< 0.19=

10 GLO) 0.112 /5.92; /10.99=

O)LP /1.59; /2.<15 /11.32<






PEL"CAM"REP"#$"%$#&"$$$$# 0 31 of 37

11 GLO) 0.10@ /5.39= /10.35=

O)LP /1.52; /2.=5@ /11.222

12 GLO) 0.02= 0.0;2 /0.291

O)LP 0.059 0.13 /0.21<

13 GLO) 0.00< 0.12= /0.203

O)LP 0.09@ 0.1@ /0.1=2

100 GLO) 0.23= /0.9@9 /1.21=

O)LP 0.0<9 /0.23= /1.3

110 GLO) 0.2@5 /0.9@5 /1.21;

O)LP 0.11 /0.29@ /1.309

120 GLO) 0.25; /0.3<2 /1.12;

O)LP 0.13 /0.1<= /1.1;;

130 GLO) 0.29 /0.39= /1.0;1

O)LP 0.122 /0.15< /1.153

0001 1 GLO) 2.059 29.<03 /105.=92

2 GLO) <.0<5 1.0=9 /9.132

3 GLO) 0.2;< 5.935 20.92=

5 GLO) 0.193 0.00; /0.03<

@ GLO) 0.11 0.203 0.103

= GLO) 0.013 0.2=< 0.1<9

10 GLO) 10.2<2 25.<<@ /10;.;12

11 GLO) 10.25 [email protected]< /10;.==1

12 GLO) 2.9@2 30.991 /<5.212

13 GLO) 2.3@5 30.51= /<5.132

100 GLO) 10.59 32.553 /;9.=39

110 GLO) 10.@<3 32.5@1 /;9.==2

120 GLO) 10.@5 32.=55 /;9.@31

130 GLO) 10.553 32.<3 /;9.55

002< 1 GLO) /0.3=1 /2.5@3 /=.0=;

O)LP /1.@;3 1.0< /=.2@5

2 GLO) 0.1@; /0.3<= /0.;05

O)LP /0.0@@ /0.019 /0.;;@

3 GLO) 0.112 2.302 5.1;5

O)LP 1.335 /0.3<; 5.51

5 GLO) 0.029 /0.001 /0.005

O)LP 0.02 /0.011 /0.01

@ GLO) 0.02 0.099 0.09






PEL"CAM"REP"#$"%$#&"$$$$# 0 30 of 37

O)LP 0.09 0.00< 0.09<

= GLO) 0.009 0.0@3 0.0@2

O)LP 0.03= 0.021 0.0==

10 GLO) /0.1=< /2.;51 /=.;<;

O)LP /1.=9 1.055 /<.2=1

11 GLO) /0.1<2 /2.;0@ /=.;99

O)LP /1.=2 1.0=9 /<.219

12 GLO) /0.23; /0.21= /1.<99

O)LP /0.31< 0.@;; /1.=0=

13 GLO) /0.255 /0.1;< /1.<22

O)LP /0.321 0.=12 /1.@=<

100 GLO) /0.10; /0.==@ /3.193

O)LP /0.51 0.=31 /3.119

110 GLO) /0.0<5 /0.=== /3.19<

O)LP /0.9; 0.=2 /3.129

120 GLO) /0.0<; /0.=32 /3.103

O)LP /0.9= 0.=3< /3.0@=

130 GLO) /0.105 /0.=13 /3.0<1

O)LP /0.9=3 0.=52 /3.03=

0002 1 GLO) /2.;< 9.335 /25.<@3

2 GLO) =.;5= 0.<=< /2.2;9

3 GLO) 2.;@; =.2;1 5.32=

5 GLO) 0.192 0.00@ /0.01;

@ GLO) 0.13@ 0.1@9 0.02<

= GLO) 0.05 0.225 0.05<

10 GLO) 5.11; 5.21; /2<.1=@

11 GLO) 5.113 5.3== /2<.13

12 GLO) 0.125 11.=; /20.50<

13 GLO) 0.03; 11.<51 /20.9=<

100 GLO) =.=;= 12.=21 /29.123

110 GLO) =.;3; 12.=2= /29.192

120 GLO) =.;33 12.<<9 /29.0;5

130 GLO) =.<9= 12.;9@ /29.0@5

0003 1 GLO) /1.0<9 5.@0@ /30.<3=

2 GLO) 9.=01 1.1 /9.113

3 GLO) 2.3@@ =.=3< @.5=5

5 GLO) 0.0;2 0.005 /0.039






PEL"CAM"REP"#$"%$#&"$$$$# 0 32 of 37

@ GLO) 0.0;= 0.1;2 0.03

= GLO) 0.095 0.2@= 0.0=@

10 GLO) 3.=1 @.=11 /39.;<9

11 GLO) 3.=15 @.<;; /39.;21

12 GLO) 1.3=; 13.53@ /29.232

13 GLO) 1.32= 13.@11 /29.1<@

100 GLO) 5.;2; 19.=25 /2;.;1=

110 GLO) @.021 19.=2; /2;.;51

120 GLO) @.02@ 19.;1= /2;.<<<

130 GLO) 5.;=9 19.;;1 /2;.<91

0009 1 GLO) /0.5;; /2.219 /35.=13

2 GLO) 9.22= /0.23; /@.192

3 GLO) 3.2<1 ;.109 <.90<

5 GLO) 0.0<= /0.003 /0.05

@ GLO) 0.112 0.1=< 0.03;

= GLO) 0.0=1 0.255 0.10@

10 GLO) 3.=15 /2.95= /91.;0@

11 GLO) 3.=9 /2.2=5 /91.<1@

12 GLO) 2.=;9 =.0@< /2=.2@@

13 GLO) 2.=53 =.19@ /2=.1;;

100 GLO) @.<=; @.59 /35.233

110 GLO) @.;@@ @.53= /35.2<3

120 GLO) @.;;1 @.=1< /35.1;9

130 GLO) @.;51 @.=;5 /35.12=

a,le 11 eck Reactio"s #u!!ary for every load case

here are "o uplift forces which !ea"s the cases are sta,le a"d have "o te"de"cy to

topple over.





REPORT


PEL"CAM"REP"#$"%$#&"$$$$# 0 33 of 37

&./.%.# MEMBER STRESSES

All structural !e!,ers i" the load spreader cradle are ,ei"& utili:ed ,elow their allowa,le !ai!u! stresses. here are "o u"ity checks over

1.0.

GR4

I

$RII$AL

'6')6R

6#$RIIO* LOA

$O*

'AC.

4*ID

$6$

I#

RO'

6*

ALI6 #R6##6# ALLO%A)L6 #R6##6# $RI.

$O*

66$IN6

L6*G#

$'

S NAL46# S

ACIAL )6*/D )6*/E ACIAL 64L6R )6*/D )6*/E LD LE D E

' *8''2 *8''2 *8''2 *8''2 *8''2 *8''2 *8''2 ' '

) 002@/003; )rackets 100 0.91 0 /1.2; /0.0= 5;.19 12=.21 933.;< 19<.< 19<.< $T.15 1.1 1.1 0.<5 0.<5

)R$ 005=/012@ )races 130 0.55 2.; /9.;9 ;9.11 12.93 11;.=< 2<1.@1 1<@ 1<@ $T.15 2.; 2.; 0.<5 0.<5

$OL 0001/0013 $olu!"s 130 0.;< 1.3 /1=.39 /151.;2 /9<.== 193.0; 3511.<9 1<@ 1<@ $T.15 1.3 1.3 0.<5 0.<5

$R 009@/0093 )ea! 120 0.2; 1.= /0.92 /93.01 0.9@ 13;.1= 19;<.1= 155.21 1@9.<3 $T.15 1.= 1.= 0.<5 0.<5

#4 0093/0055 )ea!

6te"sio"s for

,rackets

130 0.52 0 /0.05 /=;.= /0.5; 199.<2 @505.05 155.21 1@9.<3 $T.15 0.< 0.< 0.<5 0.<5





REPORT


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a,le 12 'ai!u! stresses ,y !e!,er &roups





REPORT


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i&ure = 'e!,ers !ai!u! stress co"tours +perspective view fro! u"der"eath the cradle-.






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&./. P*NC(ING S(EAR 0OINTCAN1 C(ECK

*o pu"chi"& shear checks were do"e i" this a"alysis ,ecause ,y o,servatio" it is

evide"t that pu"chi"& shear is "e&li&i,le.






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2 CONCL*SIONS AND RECOMMENDATIONS

he co"ceived cradle for each of the three cases allows a #' to e"ter ,etwee" the

two rows of colu!"s a"d lower each case o" the colu!"s. )oth rows of colu!"s have

a clear hei&ht of 1.9 !eters.

he wood cases ca" "ot ,e welded to the tra"sportatio" cradle therefore the sche!e

i"cludes three side ,racket cha""els ,raced to the deck o" star,oard a"d port sides.

he a"alysis of the proposed tra"sportatio" layout sche!e i"cludes the effects of vessel

!otio" acceleratio"s acti"& i" the hori:o"tal pla"e due to roll a"d pitch a"dwi"d

,lowi"& at 95 !ph i" the forward dia&o"al a"d tra"sverse directio"s. he a"alysis

results show that "o !e!,ers are overstressed a"d the !a?ority are ,ei"& utili:ed

,elow <0U of allowa,le.

A check o" the sta,ility of the ,ar&e also i"dicates that the draft is o"ly a,out 1 !eter

a"d the !etace"ter is hi&h e"ou&h where sta,ility has "ot ,ee" co!pro!ised. Additio"

of ,allast is "ot "ecessary for the voya&e.

Elshcon - Cameron Transportation Seafastening and Barge Stability Report

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Transcript of Elshcon - Cameron Transportation Seafastening and Barge Stability Report