Lifting Lug Design(3064)
Short Description
LIFTING LUG CALCUATION...
Description
PROJECT : EQUIPE!T !O. :
LIFTING LUG DESIGN Revi"ion !o. ade# Revi"ed $y C%e&'ed $y (pproved $y
LIFTING LUG DESIGN
Pro)e&t E*uipment !o. Revi"ion !o.
A. GEOMETRIC DAT DATA
+eig%t of empty ve""el, +e e""el Out"ide Radiu" !um$er of lug", n Lifting angle, 2 (ngle 3
-/ 0g
Lug radiu", rL Lug $a"e 4idt%, 4L T%i&'ne"" of lug, tL 5i"tan&e $et4een lug $a"e to % ole &enter, %L 5iameter of %ole, d "%a&'le material Pin "i6e, 5p B. MATERIAL MATERIAL & MECHANICAL PROPERTIES
aterial u"ed for lifting lug 7pe&ified yield "tre"", 7y 7pe&ified ten"ile "tre"", 7m Impa&t fa&tor, f C. ALLOWABLE ALLOWABLE STRESSES
(llo4a$le $earing "tre"", "tre"", 7$r.all 7$r.all < = . 7y> 7y> (llo4a$le ten"ile "tre"", 7t.all < = .9; 7y> (llo4a$le "%ear "tre"", "tre"", 7".all < = .9 .9 7y> (llo4a$le $ending "tre"", 7$n.all < = .?? 7y>
D. LIFTING LUG DESIGN DESIGN 1 FORCE DIAGRAM
18// 0g#&m99; 0g#&m-
PROJECT : EQUIPE!T !O. :
LIFTING LUG DESIGN Revi"ion !o. ade# Revi"ed $y C%e&'ed $y (pproved $y
PROJECT : EQUIPE!T !O. :
LIFTING LUG DESIGN Revi"ion !o. ade# Revi"ed $y C%e&'ed $y (pproved $y
5e"ign Load, +t < = f.+e> 5e"ign Load per lug, @y < = +t#n> erti&al erti&al &omponent for&e, @y Re"ultant for&e, @&< = @y#"in2> Component for&e, @A< = @& &o"2 "in3> Component for&e, @6< = @& &o"2 &o"3>
2 STRESS CHECK CHECK AT AT LUG EYE
Ten"ile "tre"" Re"ultant for&e, @& Cro""B"e&tional area, (e = tL Ten"ile "tre"", 7t 7in&e 7tD7t.all, t%erefore t%e lifting lug "i6e i" 7(TI7@(CTOR
Fearing Fearing "tre"" Re"ultant for&e, @& 5iameter pin, 5p Cro""B"e&tional area, (& < =5p tL> Fearing "tre"", 7$ 7in&e 7$D7$.all, t%erefore t%e lifting lug "i6e i" 7(TI7@(CTOR
7%ear "tre"" "tre"" Re"ultant for&e, @& Cro""B"e&tional area, (& < = -..tL>
PROJECT : EQUIPE!T !O. :
LIFTING LUG DESIGN Revi"ion !o. ade# Revi"ed $y C%e&'ed $y (pproved $y
7%earing "tre"", 7" 7in&e 7"D7".all, t%erefore t%e lifting lug "i6e i" 7(TI7@(CTOR
PROJECT : EQUIPE!T !O. :
LIFTING LUG DESIGN Revi"ion !o. ade# Revi"ed $y C%e&'ed $y (pproved $y 3 STRESS CHECK AT LUG BASE
Ten"ile "tre"" in B5ire&tion B5ire&tion ert&al for&e, @y Cro"" "e&tional area of lug, (t < = -ArLAtL> Ten"ile "tre"", 7t < = @y#(t> 7t#7t.all Fending "tre"" in B5ire&tion Component for&e, @A Fending moment in GBaAi", A=@AH%L 7e&tion modulu", G6B6 = 4L-HtL#? Fending "tre"", 7A=A#G6B6 7A#7A.all Plane Fending "tre"" in GB5ire&tion GB5ire&tion Component for&e, @6 Fending moment in BaAi", 6=@6H%L 7e&tion modulu", GABA= 4LHtL -#? Fending "tre"", 76 = 6#GABA 76#76.all Com$ine Com$ine "tre""e" T%erefore t%e lifting lug i" SATISFACTORY
PROJECT : EQUIPE!T !O. :
LIFTING LUG DESIGN Revi"ion !o. ade# Revi"ed $y C%e&'ed $y (pproved $y
0 5ate PST
FPCL (PLBCB/?9
119 119/ /! 8?? 8?? mm / o o 8mm - - mm /;mm 1/ 1/ mm /mm
-;.9 -;.9 mm
77B/1?L 1?.;/8; !#mm99.;18 !#mm1.;
1;-.;/ !#mm8?.981 !#mm?8.1; !#mm11-.1?9 !#mm-
0 5ate PST
0 5ate PST
-819. -819.; ;! ;81.; ;81.; ! ;81.; ;81.; ! ;81.; ;81.; ! ! ?.8E ?.8EB1B1- !
;81.; ;81.; ! 1-; mm;1.8-;9;; !#mm-
;81.; ;81.; ! -;.9 -;.9 mm !#mm11-./9 !#mm-
;81.; ;81.; ! /; mm-
0 5ate PST
-;.?-8-8 -;.?-8-8 !#mm-
0 5ate PST
;81.; ;81.; ! 9 mm-./-819 !#mm.-?;8-;
! !Bmm !Bmm -/////.// mm/ !#mm
?.8E ?.8EB1B1- ! 8.-?EB1 8.-?EB1 !Bmm 9//./// mm/ 1.91EB19 !#mm1.8/EB1?
.-?;8 .-?;8-; -; D 1 NOT OVERSTRESSED
0 5ate PST
!
(PL
LIFTING LUG DESIGN FOR EXCHANGER
Pro)e&t
RUTKCK(
E*uip. !o.
(PLBCB-
Revi"ion !o.
( GEOMETRIC DATA +eig%t of empty ve""el, +e e""el Out"ide Radiu" !um$er of lug", n Lifting angle, 2 (ngle 3
/; 0g
/9//; 1-/ /
Lug radiu", rL Lug $a"e 4idt%, 4L T%i&'ne"" of lug, tL 5i"tan&e $et4een lug $a"e to %ole &enter, %L 5iameter of %ole, d
/; 1 8 8 /
"%a&'le material Pin "i6e, 5p MATERIAL & MECHANICAL PROPERTI ES F MATERIAL aterial u"ed for lifting lug 7pe&ified yield "tre"", 7y
7pe&ified ten"ile "tre"", 7m Impa&t fa&tor, f C ALLOWABLE STRESSES (llo4a$le $earing "tre"", "tre"", 7$r.all 7$r.all < = . 7y> (llo4a$le ten"ile ten"ile "tre"", 7t.all < = .9; 7y> (llo4a$le "%ear "tre"", "tre"", 7".all < = .9 7y> (llo4a$le $ending "tre"", "tre"", 7$n.all < = .?? 7y> 7y>
5 LIFTING LUG DESIGN
1
/;
-
-.9/ 0g#&m
;-;1.;? 0g#&m-
7(B-9 r -;.?; ;1;.1;8? 1
19.;;/ -.-;-?; -.-?/; 1/;./9/;
1 FORCE DIAGRAM
5e"ign Load, +t < = f.+e> 5e"ign Load per lug, @y < = +t#n> erti&al &omponent for&e, @y Re"ultant for&e, @& @&< = @y#"in2> Component for&e, @A< = @& &o"2 "in3> Component for&e, @6< = @& &o"2 &o"3>
/9//; 1199; 1199; 1199; 8.EB1-
- STRESS CHECK AT LUG EYE
a Ten"i en"ile le "tr "tre" e"" " Re"ultant for&e, @& Cro""B"e&tional area, (e = tL Ten"ile "tre"", 7t 7in&e 7tD7t.all, t%erefore t%e lifting lug "i6e i" 7(TI7@(CTOR
1199; 19 1.8;
$ Fear Fearin ing g "tre "tre"" "" Re"ultant for&e, @& 5iameter pin, 5p Cro""B"e&tional area, (& < =5p tL> Fearing "tre"", 7$ 7in&e 7$D7$.all, t%erefore t%e lifting lug "i6e i" 7(TI7@(CTOR
1199; /; -9; 9?.819-?
& 7%ear %ear "tr "tre" e"" " Re"ultant for&e, @& Cro""B"e&tional area, (& < = -..tL> 7%earing "tre"", 7" 7in&e 7"D7".all, t%erefore t%e lifting lug "i6e i" 7(TI7@(CTOR
1199; - 9.8;
/ STRESS CHECK AT LUG BASE
a Ten"ile en"ile "tre"" in in B5i B5ire&ti re&tion on ert&al for&e, @y Cro"" "e&tional area of lug, (t < = -ArLAtL> Ten"ile "tre"", 7t < = @y#(t> 7t#7t.all
1199; 9 -/./;819/ .-;/1;
$ Fendin Fending g "tre"" "tre"" in B5ire B5ire&ti &tion on Component for&e, @A Fending moment in GBaAi", A=@AH%L 7e&tion modulu", G6B6 = 4L-HtL#? Fending "tre"", 7A=A#G6B6 7A#7A.all
11????.?8
& Plane Plane Fending Fending "tre"" "tre"" in GB5ire&ti GB5ire&tion on Component for&e, @6 Fending moment in BaAi", 6=@6H%L
8.EB19.?EB1
7e&tion modulu", GABA= 4LHtL-#? Fending "tre"", 76 = 6#GABA 76#76.all
1???.??8 ?.8EB1; 9.99EB18
d Com$ Com$in ine e "tr "tre" e""e "e" "
.-;/1; NOT OVE
T%erefore t%e lifting lug i" SATISFACTORY
R( PP, P(R(5EEP 8-
! mm
mm mm mm mm mm
mm
/9 !#mm!#mm-
!#mm!#mm!#mm!#mm-
! ! ! ! ! !
!
! mm mm!#mm-
! mm!#mm-
! mm!#mm-
! !Bmm mm/ !#mm-
! !Bmm mm/ !#mm-
STRESSED
(PL
LIFTING LUG DESIGN FOR EQUIPMENT
Pro)e&t
E*uipment E*uipment !o. (PLBCB(PLBCBRevi"ion !o.
( GEOMETRIC DATA +eig%t of empty ve""el, +e Keat EA&%anger Out"ide Radiu" !um$er of lug", n Lifting angle, 2 (ngle 3
;; 0g
1; -1 1; 8; ;
"%a&'le material Pin "i6e, 5p
7pe&ified ten"ile "tre"", 7m Impa&t fa&tor, f C ALLOWABLE STRESSES (llo4a$le $earing "tre"", "tre"", 7$r.all 7$r.all < = . 7y> (llo4a$le ten"ile ten"ile "tre"", 7t.all < = .9; 7y> (llo4a$le "%ear "tre"", "tre"", 7".all < = .9 7y> (llo4a$le $ending "tre"", "tre"", 7$n.all < = .?? 7y> 7y>
5 LIFTING LUG DESIGN
;/;; /98 9 ? ??.?1
Lug radiu", rL Lug $a"e 4idt%, 4L T%i&'ne"" of lug, tL 5i"tan&e $et4een lug $a"e to %ole &enter, %L 5iameter of %ole, d
MATERIAL & MECHANICAL PROPERTI ES F MATERIAL aterial u"ed for lifting lug 7pe&ified yield "tre"", 7y
CPCL
;/
-
-?81.? 0g#&m
9-1.;/ 0g#&m-
I7 -?- E-?-.1-/ 9-.?;-
-/;.-1 118.9?1 19.9 18-.-?8;
1 FORCE DIAGRAM
5e"ign Load, +t < = f.+e> 5e"ign Load per lug, @y < = +t#n> erti&al &omponent for&e, @y Re"ultant for&e, @&< = @y#"in2> Component for&e, @A< = @& &o"2 "in3> Component for&e, @6< = @& &o"2 &o"3>
181 -?88.; -?88.; /11;./9 19-;.;/? ?1/.-?
- STRESS CHECK AT LUG EYE
a Ten"i en"ile le "tr "tre" e"" " Re"ultant for&e, @& Cro""B"e&tional area, (e = tL Ten"ile "tre"", 7t 7in&e 7tD7t.all, t%erefore t%e lifting lug "i6e i" 7(TI7@(CTOR
/11;./9 1- -;.;111
$ Fear Fearin ing g "tre "tre"" "" Re"ultant for&e, @& 5iameter pin, 5p Cro""B"e&tional area, (& < =5p tL> Fearing "tre"", 7$ 7in&e 7$D7$.all, t%erefore t%e lifting lug "i6e i" 7(TI7@(CTOR
/11;./9 ;/ 8; /.1/;?9
& 7%ear %ear "tr "tre" e"" " Re"ultant for&e, @& Cro""B"e&tional area, (& < = -..tL> 7%earing "tre"", 7" 7in&e 7"D7".all, t%erefore t%e lifting lug "i6e i" 7(TI7@(CTOR
/11;./9 -9 1-.8;;?
/ STRESS CHECK AT LUG BASE
a Ten"ile en"ile "tre"" in in B5i B5ire&ti re&tion on ert&al for&e, @y Cro"" "e&tional area of lug, (t < = -ArLAtL> Ten"ile "tre"", 7t < = @y#(t> 7t#7t.all
-?88.; /1; .;?9-;8 .8-?/89
$ Fendin Fending g "tre"" "tre"" in B5ire B5ire&ti &tion on Component for&e, @A Fending moment in GBaAi", A=@AH%L 7e&tion modulu", G6B6 = 4L-HtL#? Fending "tre"", 7A=A#G6B6 7A#7A.all
19-;.;/? 18-1?; 11-; .8-9;9; .;?-/?
& Plane Plane Fending Fending "tre"" "tre"" in GB5ire&ti GB5ire&tion on Component for&e, @6 Fending moment in BaAi", 6=@6H%L
?1/.-? 9?/89;.18
7e&tion modulu", GABA= 4LHtL-#? Fending "tre"", 76 = 6#GABA 76#76.all
88; ;.-8; ./9;/
d Com$ Com$in ine e "tr "tre" e""e "e" "
.9?91/1 NOT OVE
T%erefore t%e lifting lug i" SATISFACTORY
;
! mm
mm mm mm mm mm
mm
;r ( !#mm!#mm-
!#mm!#mm!#mm!#mm-
! ! ! ! ! !
!
! mm mm!#mm-
! mm!#mm-
! mm!#mm-
! !Bmm mm/ !#mm-
! !Bmm mm/ !#mm-
STRESSED
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