Fuel Consumption Calculator

7/23/2019 Fuel Consumption Calculator

1/25

ITEM

REV. QTY. TAG. NO. SCH. SERVIC

1 2 1 20FO057 4/2 80 0.084 250 !0 57 a 17.00 100 "00 #$lot gas to ac$% rel$e&

2

"

4

5

!

7

8

9

10

1. 'he actual &lo( o& 20FO057 $s a)out 110 SCF* &or a )ore %$a+eter o& 0.084.

PIPE SIZE(IN.)

ORIFICE(IN.)

FLOW QUANTITY(SCFH)

UPSTREAMPRESSURE

(PSIG)

DP(PSI)

MW

SG

TEMP.(F)

FLANGERATING

INSTRUMENT SPECIFICATION

Citgo Petroleum Corporation135th Street & New Avenue

Lemont, IL 6043

Flange-type Restrictive Orifices

ALL ITEMS SHALL COMPL !ITH "ENERAL SPECIFICATION SHEETS

MATERIAL# M$nel

In!tallation note!"1# $ri%e 'ia# A!!pei%e' to !uitre(uire' on'ition!#)# *a!+et!

urni!he' -. ven'or#


2/25

ITEM

REV. QTY. TAG. NO. SCH. SERVICE

1 1 1 20FO184 11/2 80 0.285 !0 57 a 0.58! 100 "000 -c$% pu+p ent hea%er pur

2

"

4

5

!

7

8

9

10

1. te+ 1 $s +a%e o& +onel.

PIPE SIZE(IN.)

ORIFICE(IN.)

FLOW QUANTITY(SCFH)

UPSTREAMPRESSURE

(PSIG)

DP(PSI)

MW

SG

TEMP.(F)

FLANGERATING



Lemont, IL 6043

Uni$n Restrictive Orifices


MATERIAL# %&'SS

In!tallation note!"

1# /nle!! otherwi!e !pei%e', the onl. mar+ing! on the ori%e ta- !hall -e the or%e 'iametein'iate' -. a 'eimal ration a! !hown on the 'rawing with 116in# %gure !tamping han

)# 2here line! are to -e in!ulate', the in!ulate' material overing the union !hall -e applie' a

manner that the mar+ing! on the ta- will -e ull. epo!e'#3# No a!-e!to!-earing material i! aepta-le ven'or to provi'e 7 ga!+et!#


3/25

ITEM

REV. QTY. TAG. NO. SCH. SERVI

1 1 1 20FO175 4/2 80 0.1"5 !0 55 a 17.00 100 150 #$lot gas to 20F527.

2

"

4

5

!

7

8

9

10

PIPE SIZE(IN.)

ORIFICE(IN.)

FLOW QUANTITY(SCFH)

UPSTREAMPRESSURE

(PSIG)

DP(PSI)

MW

SG

TEMP.(F)

FLANGERATING


Citgo Petroleum Corporation135th Street & New AvenueLemont, IL 6043

Flange-type Restrictive Orifices


MATERIAL# %&'SS

In!tallation note!"1# $ri%e 'ia# A!!pei%e' to !uitre(uire' on'ition!#)# *a!+et!urni!he' -. ven'or#


4/25

ITEM

REV. QTY. TAG. NO. SCH. SERVICE

1 1 1 4/2 80 a 100

2

"

4

5

!

7

8

9

10

PIPE SIZE(IN.)

ORIFICE(IN.)

FLOW QUANTITY(SCFH)

UPSTREAMPRESSURE

(PSIG)

DP(PSI)

MW

SG

TEMP.(F)

FLANGERATING



Lemont, IL 6043

Uni$n Restrictive Orifices


MATERIAL# %&'SS

In!tallation note!"

1# /nle!! otherwi!e !pei%e', the onl. mar+ing! on the ori%e ta- !hall -e the or%e 'iametein'iate' -. a 'eimal ration a! !hown on the 'rawing with 116in# %gure !tamping han')# 2here line! are to -e in!ulate', the in!ulate' material overing the union !hall -e applie' a

manner that the mar+ing! on the ta- will -e ull. epo!e'#3# No a!-e!to!-earing material i! aepta-le ven'or to provi'e 7 ga!+et!#


5/25

ello( $s an $nput cell 3reen $s a calculat$on

#1 !0 ps$g 11.12 ##*

,n%erl$ne $s alue actuall6 use% 3reen $n gre6 $s a looup alue0.603 tp 2.50

0.!07

h$te $n )lac $s a &$nal ans(er

2 0.106 $n.

+portant re&erence $n&or+at$on a)out a cell $s $n $olet

From Fluor table

Cell &or $terat$on ($th goal see 'arget 'o: cell &or goal see Chang$ng cell &or goal;1st Cell< ;2n% Cell< ;"r% Cellutane 0.009254 0.012779

Caut$on th$s sheet calculates propert$es )ase% on 6ello(h$ghl$ghte% cells. 'he $scos$t$espressure an% te+perature@ ho(eer@ the S' alues &or pure co+ponents ($ll change so $S'.

#ropert$es us$ngcorespon%$ng states

Vc,cm3/mol-

1

From VISC Sheet - manual entry-- ue !IS

in%ivi%ual , then ue &il'e( metho% in )r

mixture .

@ c# E 78 ps$g @ c# E 90 ps$g


10/25

M

!.91 2.02 0.00919

8.!! 1!.04 0.011!7

12.98 "0.07 0.00988

18."0 44.10 0.00855

15.78 42.08 0.00904

8.98 17.021.28

$ll change an% are a &unct$on o&' or # change up%ate ($th

Cpo,cal/gmol-

K , cP

#ebite $or

a%heet to *al*ulate


11/25

11 o& 25

e+ont@ ll$no$s289577424.xls/?O1

RESTRICTIVE ORIFICE ---- Mt!o" 1

+ough metho% )rovi%e% originally in an arti*le in Chemi*al ngineering magaine t)/)ore %$a+eter 0.9"

#2/#1 0.05 Thin plate, no choked flow.

Calculation not applicable: refer to Kirk-Cunningha ethod.

@ $nchesG Hg@ gas &lo( $n SCF* !0 F@ 1 at+:G #@ #1@ #2@ ps$aG Sg Mg/Ma$r #$% S$& tp,mm

'1@ ?G tp@ plate th$cness. 0.5 1.5

0.75 1.5

Hg 250 SCF* E !0 F@ 1 at+ Complt P'op'ty S!t 1 1.5

57.00 'r 2.51 $rom heet 1.5 2

#1 !0 ps$g #r 0.11 2 2.5

#2 " ps$ " "

M( 17 4 "

Sg 0.59 +anual allo(e% ! "

' 100 %eg. F 1.28 8 !

#late ?ate "00 "00@ !00I -S 10 !tp 2.50 ++ From Fluor table 12 !

J 1.00 0.98 Cal*ulate% uing virial euation 14 9

1@ no+ 2.00 $n. Sch. 80 1! 9

18 12

Sat. Cure 'est I-M=K 'est I-M=K /!AM0 20 12

*ot 3as 'est 0.4"" /!AM0 24 1!

>1 0.1"5 #r/'r 0.044 J 1.00

>0 0.014

T!$% plat o'$($c

#o)-Mo"'at P

1ing table $romFluor )e*i$i*ation:2Flange "y)e

+etri*tive 3ri$i*e2

#

1ing initial )ro)ertie 56, "6

#1

D $Q

%&SQRT( P(P1 'P2)&(2S%T1)"

#

5!!

(*+&.125)1&5

M,*-o /00,03 4+464*73 *-/* %/0 40 4,/ %/0 48*9, o9 +,9f,6* %/0.Fo: *-9o%- / *-4; +/*, 40 ;,&>o9,4/,*,9 0* >, ? @. (R,f,9,;6, +%. 1.223 R46-/9 M4,9B0 Fo: M,/09,,;*E;%4;,,94;% H/;>oo=3 9 ,.3 M6G9/: H43 1@. P/%, 122 9,f,90 *o *-, :o9=of C;;4;%-/ (151) /; W/9S4*- (1").49=C;;4;%-/ /++4,0 :-,; P2?.@P1. C;;4;%-/ 0-o:, *-/* 6-o=, fo:(694*46/3 4.,.3 M $1 *-9o/*) o,0 ;o* o669 fo9 *-4; o94f46, +/*,0.


12/25

12 o& 25

e+ont@ ll$no$s289577424.xls/

#c& 40.98 ps$g Cho'e% Flo# - $or thi*' )late 2 0.106 $n. >eta 0.055


13/25

1" o& 25e+ont@ ll$no$s

2#5""!2!.80&R

RESTRICTIVE ORIFICE ---- Mt!o" *

tb%b 7.46 "hi*' )late metho% a))lie: *ho'e% $lo#. M$n. #ressure $s 40.98 ps$g

- throat crosssect$onal area@ sL. &tG I/sG Co 0.72G #1 $nlet pressure@ ps&G gc "2.174

'1 $nlet te+perature@ FG ? 1545." &tI&/I+ole?.

Hg 250 SCF* E !0 F@ 1 at+ St. ' !0 F

11.22 ##* 14.!9! ps$a

0.04 l)s./c& Co 0.72

1 1.9"9 $n.

#1 !0 ps$g 1.28 5ro)erty Sheet

exp. 8.0"

M( 17.02 5ro)erty Sheet

#c& 40.98 ps$g Cho'e% Flo#

' 100 %eg. F

- 0.004 sL. $n. Complt P'op'ty S!t

'r 2.51 1ing initial )ro)ertie 56, "6

0.06+ $n. #r 0.11

>eta 0.0"48 Sat. Cure 'est I-M=K >elo( use charts

tp 0.50 $n. *ot 3as 'est 0.4"" /!AM0

'est I-M=K I-M=K

>1 0.1"5

>0 0.014

#r/'r 0.044

T!$c plat o'$($c o' (lo)%o&&l, C!o" Flo)

Cho'e% Flo#: e. 4-49, )g. 699, aniel Cro#l, ;oe)h >9.

ro# ouvar re*ommen . or o # ar)-e ge or *e

#ith +e6?@9,999 el%om %oe thi o**ur.

#1A $

W

Co P1 = %6M RT

1

2= ' 1

(='1)&(=1)

!!C9o: Lo


14/25

14 o& 25e+ont@ ll$no$s

2#5

J 1.00


15/25

10/12/2015 Calclat$o% (o' o't! m'$ca% M(g. Co. Com2t$o% $' FE

ORIFICE T S4EET

'6pe o& Or$&$ce #late Stan%ar%

ra$n *ole &or Con%ensate: one

M-M,M ,?D?ange%: FF=?='- #?=SS,?= 40 C 5i)e iameter0

M-M,M FO ?-'= ?=H,?= 10@000 ##*

1"1@510 SCF*

# ?eLu$re% : -' ?=H,?= M-. FO ?-'= 29.78 C B-uation0

C-C,-'= M-M,M FO ?-'= -t ,?D: 11@589 ##* h(O.B. 'urn%o(n O. 0

152@400 SCF* O.B.

#=?M-=' #?=SS,?= OSS -' M-. ?-'= -t ,?D: 1."5 #S3

"7.5" C

O?FC= =' M-. C-C. ?=OS ,M>=? 1@050@!2!

3ri$i*e +e0

OM- FF=?='- #?=SS,?= 7.45 C ?etu)ulentO.B.

OM- FO ?-'= 5@000 ##* Sa$e Min. +ate0

!5@750 SCF* M$n.O.B.

MM,M FF=?='- #?=SS,?= 0."0 C

MM,M #ract$cal: FO ?-'= 1@000 ##* Ma*h !o. 30

1"@150 SCF* 3as Or$&$ce eloc$t6 $s O.B.

MM,M O?FC= =' ?=OS ,M>=? 10@000

Change in 5hyi*al 5ro)ertie0

F, Change $n propert$es O.B

'- 3-S '=M#=?-',?= 70 F

'- 3-S #?=SS,?= "0 ps$g

3-S COM#?=SS>' CO=FFC='@ J@ 1.000

3-S S#=CFC *=-' ?-'O@ @ 1."981784205

3-S DSCOS' E FO CO'OS 0.01!"455501 c#

>-S= '=M#=?-',?= !0 F

>-S= #?=SS,?= 14.!9! ps$g

>-S= COM#?=SS>' F-C'O?@ J@ 1.000

OM- ##= -M='=?@ C*=S 24N CS #$pe

##= '=?- -M='=?@ C*=S 2".5 nches

F-3= O?FC= -M='=?@ %o@ C*=S @ 4.2!222527"9 nches

O?FC= >='- 0.1814

#-'= M-'=?- SS

#-'= >-S= '*=?M- =#-SO 0.0000097 1/F

#-'= '*=?M- =#-SO 0.0000089 1/F

C*-3= 3-S =S' OD=? #-'= 0.94

C*-3= 3-S '=M#=?-',?= 4.9 F

SC*-?3= M-C* O.@ M1 S C?'C-@ 0.12!

!or "a#iu !low Calculation

CP ##*: 274.091 B 0.5972 1 0.9905

Ft) 1.00" CP SCF*: "!04.474 Fp 1.0000

F+ 1.000 F3 0.99857 F#) 1.0000

Fa 1.000 F'& 0.989! Fl 0.9998

Flo($ng con%$t$ons (ere use% to calculate the %$scharge rate o& the or$&$ce.


16/25

10/12/2015 Calclat$o% (o' FE-355

ORIFICE T S4EET

'6pe o& Or$&$ce #late ntegral

ra$n *ole &or Con%ensate: one

M-M,M ,?D?ange%: FF=?='- #?=SS,?= !0.2 C 5i)e iameter0

M-M,M FO ?-'= ?=H,?= 172 ##*

2@"20 SCF*

# ?eLu$re% : -' ?=H,?= M-. FO ?-'= !0.20 C B-uation0

C-C,-'= M-M,M FO ?-'= -t ,?D: 171 ##* h(O.B. 'urn%o(n O.

2@"20 SCF* O.B.

#=?M-=' #?=SS,?= OSS -' M-. ?-'= -t ,?D: 1.5! #S3

4"."0 CO?FC= =' M-. C-C. ?=OS ,M>=? 17!@990

3ri$i*e +e0

OM- FF=?='- #?=SS,?= 15.0" C ?etu)ulentO.B.

OM- FO ?-'= 8! ##* Sa$e Min. +ate0

1@1!0 SCF* M$n.O.B.

MM,M FF=?='- #?=SS,?= 0.!0 C

MM,M #ract$cal: FO ?-'= 17 ##* Ma*h !o. 30

2"0 SCF* 3as Or$&$ce eloc$t6 $s O.B.

MM,M O?FC= =' ?=OS ,M>=? 10@000

Change in 5hyi*al 5ro)ertie0

F, Change $n propert$es O.B

'- 3-S '=M#=?-',?= 70 F

'- 3-S #?=SS,?= 1"0 ps$g

3-S COM#?=SS>' CO=FFC='@ J@ 1.000

3-S S#=CFC *=-' ?-'O@ @ 1."

3-S DSCOS' E FO CO'OS 0.018 c#

>-S= '=M#=?-',?= !0 F

>-S= #?=SS,?= 14.!9! ps$g

>-S= COM#?=SS>' F-C'O?@ J@ 1.000

OM- ##= -M='=?@ C*=S 1/2N Sch40 CS

##= '=?- -M='=?@ C*=S 0.!!4 nches

F-3= O?FC= -M='=?@ %o@ C*=S @ 0."4 nches

O?FC= >='- 0.5120

#-'= M-'=?- SS

#-'= >-S= '*=?M- =#-SO 0.0000097 1/F

#-'= '*=?M- =#-SO 0.0000089 1/F

C*-3= 3-S =S' OD=? #-'= 0."5

C*-3= 3-S '=M#=?-',?= 1.8 F

SC*-?3= M-C* O.@ M1 S C?'C-@ 0.09!


17/25

This method



Crane "5 469, 2Flo# o$ Flui% "hrough Valve, Fitting, an% 5i)e,2 D@r% )rinting. t)/)ore %$a+eter 0.!7

#2/#1 0.01!!!7 Thin plate, no choked flow.

Stan%ar% Con%$t$ons #@ ps$a 14.!9! '@ F !0

Complt P'op'ty S!t

Flange taps 'r 1.4" $rom heet

Hg 8! SCF* 0.72 ir'-Cunningham #r 0.11

0.0! 1.28

59.00

#1 !0 ps$g 0.60+ ASM, Crane 469 Sat. Cure 'est I-M=K 'est

#2 1 ps$ 0.!07 Cunningham *ot 3as 'est 0.4"" I-M=KM( 24 0.!07 +anual allo(e% #r/'r 0.078

/!AM00.01 +anual allo(e% >1 0.100

' 120 %eg. F >0 0.15!

#late ?ate "00 "00@ !00I -S /!AM0

tp 1.50 ++ From Fluor table J 0.99

J 0.99 +anual allo(e%

1@ no+ 0.75 $n. Sch. 1!0

0.01151 +anual allo(e% 4@874

5! ps$g

% $.44 ##* calc E.47 ##* 5roblem olve% #ith goal ee'

Match Hg 4.9" ##*

#c& 40.98 ps$g Cho'e% Flo# - $or thi*' )late o 0.088 $n. >eta 0.144

T!$% plat o'$($cll (lo) co%"$t$o%2

%&"' calculation not practical --- ()*(+ too low ---Kirk-Cunninghaethod.

l)s./hrG %$+ens$onlessG C 1/&tG %o $nchesG # ps$G r I+ass/c&

E 14.!9!ps$a Q 1 at+., J&6f 1ing initial )ro)ertie

56, "6#

C@ &t1

, J&6f

g@ c# ?e1

#p

#1

W$

P

EK/*4o; 22!3 C9/;, TP !13//+*, o; .2! of *,8*.

1#1 Y C

2

Fo: *-9o%- / *-4; +/*, 40 ;,&>o9, 4/,*,9 0* >, ? @.(R,f,9,;6, +%. 1.223 R46-/9 M4,9B0 Fo: M,/09,,;* E;%4;,,94;% H/;>oo=3 9 ,.3 M6G9/: H43 1@.

P/%, 122 9,f,90 *o *-, :o9= of C;;4;%-/ (151) /; W/9S4*- (1"). I; 253 49= ,8+o9, *-, 44*0 ofC;;4;%-/B0 :o9=. H, fo; *-/* ASME fo9/0 :o9=, f4;, :4*- /0*,;* of Y C 6o >, ,f4;, 04;% ASME/; o*-,9 ,*-o0.

49=C;;4;%-/ /++4,0 :-,; P2?.@P

1. C;;4;%-/ 0-o:, *-/* 6-o=, fo: (694*46/3 4.,.3 M $1 *-9o/*) o,0

;o* o669 fo9 *-4; o94f46, +/*,0.


18/25



Crane "5 469, 2Flo# o$ Flui% "hrough Valve, Fitting, an% 5i)e,2 D@r% )rinting.

#2/#1 0.0"""""

Complt P'op'ty S!t

=st$+ate% Co+press$)$l$t6 Factor J: &

Stan%ar% Con%$t$ons #@ ps$a 14.!9! '@ F !0 For ): 1.4! Sat. Cur

OK

0.04 *ot 3a

Flange taps 1 Cunningham #

Hg 250 SCF* 0.!! Cunningham re*ommen%e% J) 0.9800.05 1.28 +anual 0.980

87.0 /!

#1 90 ps$g 0.787 ASM, Crane 469

#2 " ps$ 0.!07 Cunningham

M( 17 +anual allo(e% For 1: 1.57 Sat. Cure

0.02 +anual allo(e% 0.1! *ot 3as

' 100 %eg. F #

#late ?ate "00 "00@ !00I -S

tp 2.50 ++ From Fluor table

J1 0.991 +anual allo(e% /!

1@ no+ 2.00 $n. Sch. 80

0.01151 +anual allo(e% "@2""

8! ps$g

% ++.43 ##* calc 66.@6 ##* 5roblem olve% #ith goal ee'

Match Hg ##* Hcalc 247 SCF*

#c& 57.4" ps$g Cho'e% Flo# - $or thi*' )late o 0.0$4 $n. >eta 0.028

%&"' calculation not practicaethod.

l)s./hrG %$+ens$onlessG C 1/&tG %o $nchesG # ps$G r I+ass/c&

'r)

Choose Cunningham *-,2iller *%-, or 3luor *4- for 5 #r)

1

>, J&6f

#

C@ &t1

'r1

1, J&6f #r1

g@ c# ?e1

#p

#1 W $ -Pf1

A/+*, f9o ,K/*4o; .@#3 T-, AGA ,K/*4o;3 4; R46-/9 M4,9B0 Fo:M,/09,,;* E;%4;,,94;% H/;>oo=3 9 ,.3 M6G9/: H4 3 CR 1@(T-40 ,K/*4o; :/0 //+*, o94%4;/7 f9o ,K/*4o; 22!3 C9/;, TP !1.)

Fo: *-9o%- / *-4; +/*, 40 ;,


19/25

DSC

D. Willard 10/12/2015 Plant I

G A S M I X T U R E V I S C O S I T Y

This sh! !"l#s $i!h !h %&'&!is Sh!.

M"*"l i*! +"l*s "& i ,G&.,

T-&"!*& 8 C /00 1

%&'&"- "ss*-s !h"! "ss "& &3! " 3'&- " i"l +"'& s'l*!i'. %&'&"- $ill +i"! slih!l6 3'& hih &ss*& (/50 si

il# -!h' sh'$s s'- +i"!i's $h& -'l*l"& $ih!s "& sii3i"!l6 i33&!: i..: MiM;.

il# G"s Mix!*& Vis'si!6 C"l*l"!i' 3'& I"l G"ss '& R"l G"ss < L'$=M'&"! %

Component Man M

>6&' 0.00 Ys 0.009189 = 2.02 0.000 0.000 0.000 0.000 0.000 0.00

M!h" 0.94 Ys 0.011!72 0.0//7 /?.04 0.000 /.000 /.47 /.899 0.000 0.00

E!h" 0.05 Ys 0.009882 0.0099 0.07 0.000 0.??5 /.000 /.00 0.000 0.00

%&'" 0.0/ Ys 0.008547 0.0085 44./0 0.50? 0.50? 0.7?? /.000 0.000 0.00

%&'6l 0.00 Ys 0.0090"9 = 42.08 0.000 0.000 0.000 0.000 0.000 0.00

G"s ? /.00 Ys 0.000000 = 0.000 0.000 0.000 0.000 0.000 0.00

G"s 7 0.00 Ys 0.000000 = 0.00 0.000 0.000 0.000 0.000 0.000 0.00

G"s 8 0.00 Ys 0.000000 = 0.00 0.000 0.000 0.000 0.000 0.000 0.00

G"s 9 0.00 Ys 0.000000 = 0.00 0.000 0.000 0.000 0.000 0.000 0.00

G"s /0 0.00 Ys 0.000000 = 0.00 0.000 0.000 0.000 0.000 0.000 0.00

T'!"l 2.00

Gas a b c Mwt. " @ 3

AlCl2 97.89 9.040/5 8.?8E=0 /.72E=09

AlCl =0.000? /.?E=005 =7.//E=/0 /.4 2.40E=02 4.8/E=08 5.57E=/

C"&@' Bi'xi 0.00/87 2.9E=05 =/.27E=09 44.009 ?.2/4/5 5./2E=0 0 0

C"&@' M''xi 0.00?28 2./?E=05 =/.70E=09 28.0/ ?.4204 8.88E=04 0 0

Chl'&i 0.002/5 2.0/E=005 2.E=09 70.9 ?.02/27 ?.5?E=0 .0/E=09 0.00000

>6&' S*l3i 2.40E=05 =.40E=/0 .0?8 ?.??/50 2.85E=0 0 0

i!&' 0.0044 4.28E=05 7./5E=09 28.0/ ?.89500 7.?2E=04 0 0

Ox6 0.00?24 2.59E=05 =2.7/E=09 /.998 ?.44284 /.25E=0 0 0

>Cl 0.00/77 2.2?E=05 .95E=09 ?.4?/ ?.5/457 0 0 0

S*l3*& Bi'xi 2./2E=05 =/.44E=09 ?4.058 7.//595 5.9E=0 /.08E=0? 0 0

TiCl4 0.007/ 0.00007 /./?E=008 /89.?9 2.92E=02 /.2E=08 2.?2E=/

"!& =0.0009? /.97E=05 =.84E=09 /8.0/5 7.0897? /.55E=0 0 0 0

Information Alligned for MBAL & VISC for auto entrie.

M-'M-'? M$! " @ 3

DA DA DA DA DA DA DA DA DA DA DA










E!& +"l*s i ,Yll'$.,

C"l*l"! +"l*s i ,Lih! G&,.

yi

Manual

i

i

i1

i2

i3

i4

i5

i6

" F @(T) F (T)2F(T) C " F @(T) F (T)2F (T) F (T)4F 3(T)5

C " F @(T) F (T)2F (T) F (T)4F 3(T)5

"() @ () ()


20/25


21/25


22/25


23/25


24/25

0 500 1@000 1@500 2@000 2@500 "@000 "@500

0.0000

0.0100

0.0200

0.0"00

0.0400

0.0500

0.0!00

0.0700

0.0800

0.0900

0.1000

0.1100

0.1200

... .

1.2G M "0

1."G M 17

1.4G M 2

9, SCF4 :60 F, 15.+ p2$a;

.

) T1 $ 1oF3P $ #" +04%3 P1$ +04%3 U04;% C;;4;%-/

6/6/*4o; fo9 Y13 /0 74,4;% *-, -4%-,0* Q. T-, +9,009, 9o+

40 ;o* -: *-, 9o+ 40 *-, +,9/;,;* +9,009, o00.

H#M/?': HM/408.!7##* poun%s per hourH 408.!!/M:


25/25

9, SCF4 M

1.2 50 0.0144 0.0144 "0

1.2 250 0.0"22 0.0"22

1.2 500 0.0455 0.04551.2 1@000 0.0!4" 0.0!4"

1.2 1@500 0.0788 0.0788

1.2 2@000 0.0910 0.0910

1.2 "@000 0.1114 0.1114

1.2 4@000 0.1298 0.1298

1.2 5@000 0.1451 0.1451

1." 50 0.012! 0.012! 17

1." 250 0.0281 0.0281 0.0279

1." 500 0.0"97 0.0"97

1." 1@000 0.05!1 0.05!11." 1@500 0.0!88 0.0!88

1." 2@000 0.0794 0.0794

1." "@000 0.097" 0.097"

1." 4@000 0.1"17 0.1"17

1." 5@000 0.1472 0.1472

1.4 50 0.0072 0.0072 2

1.4 250 0.01!" 0.01!"

1.4 500 0.02"0 0.02"0

1.4 1@000 0.0"25 0.0"25

1.4 1@500 0.0"98 0.0"981.4 2@000 0.04!0 0.04!0

1.4 "@000 0.05!" 0.05!"

1.4 4@000 0.0!!0 0.0!!0

1.4 5@000 0.07"7 0.07"7

'1 100oF@ # 87 ps$g@ #1 90 ps$g@,s$ng Cunn$ngha+

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Fuel Consumption Calculator

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