Fuel Conservation Strategies Cruise Flight
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CRuiSE FLigHT iS THE pHASE OF FLigHT BETWEEN CLiMB AND DESCENT.
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Aero quArterly
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Fel Conservaton Stratees: cs Fh b W Roberson, Senor Sfet Pot, Fgt Opertons; Robert Root, Fgt Opertons Engneerng; nd De ads, Fgt Opertons Engneer Ths artcle s the second n a seres exlorn el conservaton stratees.
A c f c c c v cm m, m, b c m . A b, cm, m vm f. ths a ds s fh, pss vas
Cruise light deined
s shs, ad s h s wd s spd aas. i as dssss h ashp w s fh ad s dx
cs fh s h phas fh ha as w ad ds. th as pas
(ci) whh was dsssd h s a hs ss, “F csva Sas: cs idx expad” h sd-a 2007 AERO 2007 AERO .
p ad p a sd pa hs phas fh. As a asd, apad w ad av, whh as pas p
usd apppa, h ci a h fh aa p (Fmc) a hp as sa d pa ss. Hwv,
ad sa, a avdd hh apppa s pa. th vaas ha a h a ad
a pas d’ ak advaa hs pw .
a spd s, ad s, ad, s d, av (cg). ths a ss spd s.
A hh-v jvs a f spd s. ths jvs, whh dpd h pspv h p, dspah, pa , pas pa, a pd v as: 1. max h dsa avd a v a (.., ax a). 2. m h sd a v dsa vd (.., p ). 3. m a p (.., ). 4. m a pa s h p (.., s, [econ] spd). 5. maa h fh shd. th s w jvs a ssa h sa as h ass h apa w fw ahv p a.
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P c -m m q m m b c m m f.
Considerations aeCting Cruise strategies
h spd ha w pvd h hs dsa avd a v a d ad h d a v s dsa.
i add h va sa jvs
lrc has hsa dd as h spd av mrc ha w s a 1 p das a s aa s p
sd av s fh, ps a d da wh sh sas ha a h pa aad h s sa s d a fh. ths sas a d: ■
■
F a xd spd ha s pa wh h a a spd s. F a spd aad ahv a
■
d ava (.., rtA) a a x. F a spd aad ahv fw wh hd
■
(.., ax da). Wh dd aa a sp spd a a .
possiBle Cruise sCheMes th a w ha spd ss h s phas fh. th ada spd s -a s (lrc). lrc spd s ad wh ax-a s (mrc) spd, whh s
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CI=
ka pd d. th ass x, Aero dynamcs dynamcs or Naval Avators , vsd 1965, sas: “ms -a s pa s dd a h fh d whh pvds 99 p h as ax sp a. th advaa s ha 1 p a s add 3 5 p hh s v. S hh s spd has a a advaas, h sa sa a s a a
Tm c ~ $/ F c ~ c/b
aa.” ths p s apha sad 1. bas s h d s assad wh a fh, a h h spd s a pa s econ spd, asd h d ci. ths spd, whh ds s ads w p ad p , s asd a sa h -ad pa xpss ha a sp ah a’s pa. ci s dd as h a dpd ss ss.
long-range Cruise and Cost index th ashp w lrc spd ad econ spd s d ah b apa d. As sad, lrc s asd a 1 p pa a, wh h econ spd ss ci as a p ha s asd a dad a aa ss. Hwv, s pss dv a ci a s ds ha appxas
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REPRESENTaTiVE COmPaRiSON OF mRC aND lRC
Fre 1 Modern fht manaement systems atomatcally adjst LRC seed throhot crse or weht chane de to el brn, as well as chanes n crse alttde.
68
MRC: Mach .826 67
LRC: Mach .840 1% Penalty
) g k 0 0 0 , 1 / m n ( e g A e l i m l e u F
66
65
64
63
62
0.76
0.77
0.78
0.79
0.80
0.81
0.82
0.83
MRC
0.84
0.85
0.86
LRC
cruiSe mAcH number
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lrc s h s spd ha ss. F 2 shws h appxa ashp b a apas. i s v pa ha h lrc spd s as vsa hh ha h spd ha w s s h ci sd s as. i ad wh a w sa a dsa, a ps w p f lrc spd hk ha w v h h s s h a . As shw 2, h s sa sv s s a v w s dx, wh pvd h ax a. A p a as dsa hs d s fh p d cis h Fmc ad pa wh lrc sv h pdd a dsa.
eeCts o wind on Cruise speed i add aa p ss, h s h f econ sad lrc wh s b apas. th lrc spd
F xap, h ps a s awd, h econ spd w dd d ax h advaa ad h awd d h s. cvs, h econ spd w asd wh f a hadwd s h pa assad wh h hadwd (s xap . 3).
the relationship Between operating Costs and Cost index i ps as av h ss, a spd d ci w aa h s a pa h apa. i,
suMMary i d fh ws ahv p s pa, s ssa s dsad h fh’s sa jvs, ad h s h s spd ha s s hs jvs. i s a pa ha a-wd sas a s h d dvas h vd sa. Apppa s vas wh ah a, ad ss v ah fh. b Fh opas e assss as’ fh pas dpas p a aa ci ha w a h ss h s. F a, pas a Fhops.e@..
hwv, a a xps s h ss, a as ci w a h s a pa. i h as, h ha ci w s has h s spd aad h Fmc. ev aa a s dx asd appxa ss ad f econ spd
aad h Fmc s pa adjsd wds a s ad h econ spd s. As
a d sa s s h a. t sd s v, ci shd asd a phsv vaa a pa’s
a s, lrc s da wd ds, wh h econ spd s pd a s wd ds.
sp pa ss. F hs as, fh ws pa v a dd ci va h fh pas dpa, ad s a advsa dva hs va ss sp sh- sas dad .
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Aero quArterly
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RElaTiONShiP OF COST iNDEX TO lRC FOR BOEiNG aiRPlaNES
Fre 2 The LRC-eqvalent cost ndex vares or derent arlane models and ennes.
tpa a ci vas
mrc
m
lrc
(c m km)
H c mc mb
E I (I) aiRPlaNE mODEl
TyPiCal aiRliNE Ci ValUES
aPPROXimaTE lRC EqUiValENT
71 7
0
40 60
70
737-3/4/500
0
5 25
25
737-6/7/800
0
10 30
35
7 57
0
1 5 50
85
767
0
1 5 55
70
777
0
9 0 1 50
180
mD-11
0
80 120
200
7 4 7 -4 0 0
0
25 80
230
ECON SPEED iS OPTimiZED FOR CRUiSE WiND CONDiTiONS
Fre 3
mRC
EON c COST iNDEX
100 kT TailWiND
ZERO WiND
100 kT hEaDWiND
0
0 . 77 3 *
0.773
0.785
80
0 . 78 7
0.796
0.803
max**
0 . 8 11
0.811
0.811
*Fmc w sw dw w s a ci=0 econ spd. **A ax ci, Fmc w f a vp a wd ds.
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