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It defines how to do gasoline airpath claibration
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AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
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die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
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ilung
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GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Maturity Author Checked Description
L.ROCAMORA / JL.ALBERT A.LAPEYRE First version
P ES E TCI TC TLS P ES E TCI TC TLS17/03/2010
AIRPATH CALIBRATION
Date 17 March 2010
From L.ROCAMORA / JL.ALBERT
To G.MICHON / D.CRENNE
Project leader B.OLIVIER
Project code A-0355E
Campaign EDTR_145_2010_ETB03
Customer PROTON CAMPRO
Campaign name EDTR_145_2010_ETB03
Test name Test 6 G103
Test date From 09 to 12 February 2010
ETB 3
Engine Proton 1.6L IAFM + n°346
Subject Air path calibration
Author : F. ANTONIO page1/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Table of contents
AIRPATH CALIBRATION 1
1 INTRODUCTION 3
2 TEST CONDITIONS 3
3 RESULTS & METHODS 53.a AMP acquisition 53.b Pressure loss through the air cleaner determination: 53.c TIA_THR / T_OIL / TAM 63.d VOLUMETRIC EFFICIENCIES 73.e Eff_vol_flow_cor 83.f REDUCED AREA 9
4 CONCLUSION 9
5 VALIDATION AND GRAPHS 9
Author : F. ANTONIO page2/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
AIRPATH CALIBRATION
1 INTRODUCTIONThe aim of these tests was to calibrate the "Intake Air System".The target of the Intake System (INSY) is to coordinate the air flow controlling components (throttle and variable intake manifold) and to predict the air mass flow behaviour.With Systems like this, equipped with a manifold pressure (MAP) sensor, the mass air flow is not directly measured but only calculated out of the air density, it strongly depends on the knowledge of the air temperature in the manifold. Any deviations from the temperatures valid during the calibration of the engine have to be compensated.
2 TEST CONDITIONS
Air intake temperature: Regulated at 25°C.
Coolant temperature: Regulated at 90°C water-out.
Oil temperature: Regulated at 110°C
Relative humidity: Regulated at 50%
OIL Type: TCO_002 commercial COFLU 05W30
Fuel: ALVEA Ron95 commercial (Ron measured 98.4) regulated at 25°C
Fuel pump: Pressure regulated at 4bars relative by the bench
Engine name: PROTON 1.6L IAFM n°346
ECU: EASY-U1.28 U00110 CPC.515.000.C002 C3sample (with Canon plug)
Software calibration: U0120A3b.a2l
Calibration file: U0120A_IAFM_PLUS_16_DET_20100119_ dc03.s19
Exhaust line: Catalyst and vehicle pipe with muffler.
Temperatures limits: Exhaust global limit < 900 °C
Catalyst < 950°C
Devices: Morphee, INCA, Indicom, Gas analysis.
Author : F. ANTONIO page3/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Proton engine configuration: Naturally-aspired engine. MAP sensor with air temperature measurement included in inlet manifold. (NC_MAP_CONF
= 1) VIM actuator. No AMP; PUT; PRS_AIC_DOWN sensors available (NC_AMP_CONF = 0 / NC_PUT_CONF
= 0 / NC_PRS_AIC_DOWN = 0). No TIA_THR; TIA_CYL sensors available.
Then the air path strategy was calibrated respecting the chronology of the following method:
MAP acquisition validation (during input/output check test). AMP acquisition and PRS_LOSS_AIC determination. TIA acquisition (TIA_THR and TIA_CYL). Volumetric efficiencies determination. AR_RED tables calibration.
Involved tables and variables were:AMP learning:
c_n_amp_ad_max c_n_amp_ad_min c_amp_hys c_amp_max c_amp_min c_t_dly_amp_ad_map_mes_min ip_tps_amp_ad_map_mes_min_1 ip_prs_loss_aic
TIA_THR model: ip_tia_thr ip_fac_tia_thr
MAF model: ip_eff_vol_ofs_3_[0][0][0] ip_eff_vol_slop_3_[0][0][0] ip_eff_vol_ofs_3_[1][0][0] ip_eff_vol_slop_3_[1][0][0]
Eff_vol_flow_cor: ip_eff_vol_prs_ex_cor_1[0] ip_eff_vol_prs_ex_cor_1[1] ip_eff_vol_vo_cor_2[0] ip_eff_vol_vo_cor_2[1 ip_prs_ex lc_prs_ex_swi]
Author : F. ANTONIO page4/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Reduced area: ip_ar_red_thr ip_tps_sp_mdl_bas
3 RESULTS & METHODS
3.a AMP acquisitionDue to non presence of AMP sensor, the ambient pressure is measured by MAP sensor in the two following cases:
At the first tooth detection, AMP = MAP At full load (naturally aspired engine) where AMP = MAP – pressure loss through the air
cleaner.
AMP learning activation was calibrated for: C_AMP_HYS = 2 hpa of difference in order to enable learning at Full load conditions. C_AMP_MIN = 500hpa C_AMP_MAX = 1200hpa C_N_AMP_AD_MAX = 4200rpm C_N_AMP_AD_MIN = 1600rpm IP_TPS_AMP_AD_MAP_MAS_MIN_1 comes from the previous calibration
3.b Pressure loss through the air cleaner determination:
The aim of this test was to model the pressure decrease between ambient pressure AMP and the pressure upstream the throttle PUT due to air filter and ducts in the air cleaner and the air intake.
This table was calibrated, using the difference between AMP bench measurement and the MAP system measurement, on the full load points at different engine speeds between AMP acquisition limits of C_N_AMP_MIN and C_N_AMP_MAX.
The VS effect was not calibrated at engine bench so the values were constant function of vehicle speed.
Pressure loss through the air cleaner:
0 80 200 300
0 0 10 22 4050 0 10 22 40100 0 10 22 40200 0 10 22 40
VS
MAF_KGH
Author : F. ANTONIO page5/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
3.c TIA_THR / T_OIL / TAM
According to the air temperature sensor position inside the intake manifold, it is expected that TIA_IM and TIA_CYL are comparable to the measured air temperature. Therefore TIA_IM and TIA_CYL are set equal to TIA, which normally based on the measured TIA_MES value.So the TIA configuration was TIA = TIA_IM = TIA_CYL.
The calculation of TIA_THR is made from TIA, by taking into account the influences of:1. The mass air flow through the throttle (mapped via MAF_THR_STK_TIA, N_32)2. The manifold wall temperature (mapped via TIA, TOIL)
Exhaust gas recirculation and canister purge effects are not taken into account.
IP_TIA_THR table was calibrated using volumetric efficiency measures with VIM off, using bench measures of inlet temperature near throttle compared to inlet manifold temperature.
Results:
-25.5 0 20.25 30 45 54.75 69.75 90-30 0 0 0 0 0 0 0 0-10 0.109 0 0 0 0 0 0 00 0.172 0 0 0 0 0 0 0
25 0.344 0.250 0 0 0 0 0 045 0.500 0.391 0.266 0.203 0 0 0 065 0.656 0.594 0.531 0.500 0.453 0.406 0 085 0.844 0.859 0.875 0.891 0.859 0.844 0.500 0120 1.210 1.360 1.484 1.550 1.629 1.630 1.400 0.050
80 100 150 200 250 300 350 400992 -2.3 -2.3 -2.3 -2.3 -3.0 -1.5 -2.3 -3.8
1504 -3.0 -2.3 -2.3 -2.3 -2.3 -2.3 -2.3 -3.82016 -3.0 -3.0 -2.3 -3.0 -2.3 -2.3 -3.0 -3.83008 -3.8 -3.8 -3.0 -3.0 -2.3 -2.3 -2.3 -2.34000 -3.8 -3.8 -3.8 -4.5 -4.5 -3.8 -3.8 -3.84992 -3.8 -4.5 -3.8 -4.5 -3.8 -3.0 -2.3 -2.36016 -4.5 -4.5 -5.3 -5.3 -4.5 -3.8 -3.8 -3.86496 -4.5 -5.3 -5.3 -4.5 -4.5 -4.5 -3.8 -3.8
IP_TIA_THR
ldp
_n_3
2_ti
a_t
hr
ldp_tia_fac_tia_thr
ld
p_t
oil
_fa
c_ti
a_th
r
ldp_maf_stk_tia_thr
IP_FAC_TIA_THR
Author : F. ANTONIO page6/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
3.d VOLUMETRIC EFFICIENCIES
The aim of the test was to calibrate the volumetric efficiency slope and offset in two VIM positions so that the linear model best fits the reality of the actual engine. Because in the Intake Manifold Model, the mass air flow into the cylinder is modelled as a linear (volumetric efficiency) depending on the intake manifold pressure. These coefficients depend on the engine speed and then are valid for a real linear relation between the MAF_CYL and the MAP in regular conditions. In steady state and without EGR or canister purge, MAF_CYL=MAF_THR.
On the Proton engine configuration, four tables were used to the volumetric efficiency calibration:VIM_OFF:IP_EFF_VOL_OFS_3[0][0][0]: volumetric efficiency slope in VIM position 0IP_EFF_VOL_SLOP_3[0][0][0]: volumetric efficiency offset in VIM position 0VIM_ON:IP_EFF_VOL_OFS_3[1][0][0]: volumetric efficiency slope in VIM position 1IP_EFF_VOL_SLOP_3[1][0][0]: volumetric efficiency offset in VIM position 1
The table change between the two VIM states (OFF / ON) is made by the index STATE_ACR_EFF_VOL_CLC.
To calibrate these tables, were done measures of System MAP and Bench MAF at 300mbars (low load), at 600mbars (part load) and at Full Load, on engine speeds corresponding to table breakpoints and on both positions of VIM.Slope and offset of resultant lines were calculated via Excel function at each engine speed breakpoint of volumetric efficiency maps.Then the results were reported in tables.
800 992 1216 1600 2016 2400 3008 3616 4000 4416 4608 4800 5408 5792 6208 6496
80 0.039 0.049 0.060 0.079 0.099 0.125 0.156 0.200 0.232 0.252 0.257 0.263 0.277 0.288 0.294 0.29085 0.039 0.049 0.060 0.079 0.099 0.125 0.156 0.200 0.232 0.252 0.257 0.263 0.277 0.288 0.294 0.29090 0.039 0.049 0.060 0.079 0.099 0.125 0.156 0.200 0.232 0.252 0.257 0.263 0.277 0.288 0.294 0.29095 0.039 0.049 0.060 0.079 0.099 0.125 0.156 0.200 0.232 0.252 0.257 0.263 0.277 0.288 0.294 0.290100 0.039 0.049 0.060 0.079 0.099 0.125 0.156 0.200 0.232 0.252 0.257 0.263 0.277 0.288 0.294 0.290105 0.039 0.049 0.060 0.079 0.099 0.125 0.156 0.200 0.232 0.252 0.257 0.263 0.277 0.288 0.294 0.290110 0.039 0.049 0.060 0.079 0.099 0.125 0.156 0.200 0.232 0.252 0.257 0.263 0.277 0.288 0.294 0.290115 0.039 0.049 0.060 0.079 0.099 0.125 0.156 0.200 0.232 0.252 0.257 0.263 0.277 0.288 0.294 0.290
IP_EFF_VOL_SLOP_3[0][0][0]
Cam
_mv_
in_1
_in
sy
Engine speed (rpm)
800 992 1216 1600 2016 2400 3008 3616 4000 4416 4608 4800 5408 5792 6208 6496
80 0.038 0.047 0.058 0.078 0.094 0.123 0.153 0.186 0.217 0.247 0.261 0.269 0.313 0.329 0.333 0.34285 0.038 0.047 0.058 0.078 0.094 0.123 0.153 0.186 0.217 0.247 0.261 0.269 0.313 0.329 0.333 0.34290 0.038 0.047 0.058 0.078 0.094 0.123 0.153 0.186 0.217 0.247 0.261 0.269 0.313 0.329 0.333 0.34295 0.038 0.047 0.058 0.078 0.094 0.123 0.153 0.186 0.217 0.247 0.261 0.269 0.313 0.329 0.333 0.342100 0.038 0.047 0.058 0.078 0.094 0.123 0.153 0.186 0.217 0.247 0.261 0.269 0.313 0.329 0.333 0.342105 0.038 0.047 0.058 0.078 0.094 0.123 0.153 0.186 0.217 0.247 0.261 0.269 0.313 0.329 0.333 0.342110 0.038 0.047 0.058 0.078 0.094 0.123 0.153 0.186 0.217 0.247 0.261 0.269 0.313 0.329 0.333 0.342115 0.038 0.047 0.058 0.078 0.094 0.123 0.153 0.186 0.217 0.247 0.261 0.269 0.313 0.329 0.333 0.342
IP_EFF_VOL_SLOP_3[1][0][0]
Cam
_mv_
in_1
_in
sy
Engine speed (rpm)
Author : F. ANTONIO page7/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
800 992 1216 1600 2016 2400 3008 3616 4000 4416 4608 4800 5408 5792 6208 6496
80 3.688 4.469 5.469 5.750 8.344 10.000 7.781 10.813 15.125 17.438 17.406 18.406 21.563 26.688 29.656 27.21985 3.688 4.469 5.469 5.750 8.344 10.000 7.781 10.813 15.125 17.438 17.406 18.406 21.563 26.688 29.656 27.21990 3.688 4.469 5.469 5.750 8.344 10.000 7.781 10.813 15.125 17.438 17.406 18.406 21.563 26.688 29.656 27.21995 3.688 4.469 5.469 5.750 8.344 10.000 7.781 10.813 15.125 17.438 17.406 18.406 21.563 26.688 29.656 27.219100 3.688 4.469 5.469 5.750 8.344 10.000 7.781 10.813 15.125 17.438 17.406 18.406 21.563 26.688 29.656 27.219105 3.688 4.469 5.469 5.750 8.344 10.000 7.781 10.813 15.125 17.438 17.406 18.406 21.563 26.688 29.656 27.219110 3.688 4.469 5.469 5.750 8.344 10.000 7.781 10.813 15.125 17.438 17.406 18.406 21.563 26.688 29.656 27.219115 3.688 4.469 5.469 5.750 8.344 10.000 7.781 10.813 15.125 17.438 17.406 18.406 21.563 26.688 29.656 27.219
IP_EFF_VOL_OFS_3[0][0][0]Engine speed (rpm)
Cam
_mv_
in_1
_in
sy
800 992 1216 1600 2016 2400 3008 3616 4000 4416 4608 4800 5408 5792 6208 6496
80 3.844 4.469 4.875 5.438 5.531 8.625 13.469 10.625 12.594 11.656 13.063 14.563 21.156 24.313 28.500 28.25085 3.844 4.469 4.875 5.438 5.531 8.625 13.469 10.625 12.594 11.656 13.063 14.563 21.156 24.313 28.500 28.25090 3.844 4.469 4.875 5.438 5.531 8.625 13.469 10.625 12.594 11.656 13.063 14.563 21.156 24.313 28.500 28.25095 3.844 4.469 4.875 5.438 5.531 8.625 13.469 10.625 12.594 11.656 13.063 14.563 21.156 24.313 28.500 28.250100 3.844 4.469 4.875 5.438 5.531 8.625 13.469 10.625 12.594 11.656 13.063 14.563 21.156 24.313 28.500 28.250105 3.844 4.469 4.875 5.438 5.531 8.625 13.469 10.625 12.594 11.656 13.063 14.563 21.156 24.313 28.500 28.250110 3.844 4.469 4.875 5.438 5.531 8.625 13.469 10.625 12.594 11.656 13.063 14.563 21.156 24.313 28.500 28.250115 3.844 4.469 4.875 5.438 5.531 8.625 13.469 10.625 12.594 11.656 13.063 14.563 21.156 24.313 28.500 28.250C
am_m
v_in
_1_i
nsy
IP_EFF_VOL_OFS_3[1][0][0]Engine speed (rpm)
3.e Eff_vol_flow_cor
Because of no linearity of the air path model and to avoid so important MAF error the model eff_vol_flow_cor was calibrated from 1000rpm to 2400rpmIt was normally used on turbo engine.
Configuration: Lc_prs_ex_swi = 1 Ip_prs_ex = 1013mbar ip_eff_vol_vo_cor_2[0] = 1 ip_eff_vol_vo_cor_2[1 = 1 ip_eff_vol_prs_ex_cor_1[1] = 0
From data of a complete engine characterization, ip_eff_vol_prs_ex_cor_1[0] was tuned to minimize MAF error from 1000rpm to 2500rpm.
Author : F. ANTONIO page8/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
800 992 1216 1600 2016 2400 3008 3616 4000 4416 4608 4800 5408 5792 6208 6496
0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 00.3 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 00.4 0 -0.5 -0.5 0 0 -1.004 0 0 0 0 0 0 0 0 0 00.4 0 -0.699 -0.699 -0.851 0 -1.999 0 0 0 0 0 0 0 0 0 00.5 0 -0.851 -0.851 -0.949 0 -1.999 0 0 0 0 0 0 0 0 0 00.5 0 -1.001 -1.001 -1.099 0 -4.001 0 0 0 0 0 0 0 0 0 00.6 0 -1.321 -1.379 -1.501 0 -6 0 0 0 0 0 0 0 0 0 00.7 0 -1.7 -1.501 -1.099 0 -6 0 0 0 0 0 0 0 0 0 00.9 0 -1.901 0 0 0 -6 0 0 0 0 0 0 0 0 0 00.9 0 -1.999 0 0 0 -6 0 0 0 0 0 0 0 0 0 01 0 -1.999 0 0 0 -3 0 0 0 0 0 0 0 0 0 0
1.1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
IP_EFF_VOL_PRS_COR_1[0]
pq
_map
_prs
_ex
Engine speed (rpm)
Author : F. ANTONIO page9/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
3.f REDUCED AREA
This test allows calibrating the basic reduced area which represents the real area air flow.On the Proton application, only the throttle opening section was considered, then only the table IP_AR_RED_THR was calibrated.
So to calibrate this table, sweeps were done on several engine speeds at iso TPS values, and for all throttle position breakpoints, the table was readjusted to reduce the variables AR_RED_DIF_REL and PUT_MDL_DIF_REL until 0.Then the map IP_TPS_SP_MDL_BAS is an inversion of the table IP_AR_RED_THR.See graph page 31.
IP_AR_RED_THR and IP_TPS_SP_MDL_BAS final tables:
1 2 3 4 5 7 9 11 15 20 25 30 35 40 50 82
0.066 0.123 0.169 0.227 0.289 0.434 0.595 0.775 1.206 1.790 2.580 3.655 4.943 7.000 12.810 13.500
TPS_SEG (%)IP_AR_RED_THR
0.066 0.123 0.169 0.227 0.289 0.434 0.595 0.775 1.206 1.790 2.580 3.655 4.943 7.000 12.810 13.500
1 2 3 4 5 7 9 11 15 20 25 30 35 40 50 82
IP_TPS_SP_MDL_BASAR_RED (cm²)
4 CONCLUSIONCalibrations were correctly performed without any problem.
Different tables validations revealed that maps were correctly calibrated, with global TIA_THR error below 3°C and global MAF error between - 5% (low rpm, part loads) and 3%.
The volumetric efficiency were also reworked on the breakpoints 800 rpm, 1000 rpm, 1200 rpm, 1600 rpm, 2400 rpm, 5400 rpm & 5800 rpm in order to minimize a so important error at low MAF (<200mg/strk). Slope and the offset were changed on the table to have better accuracy at low MAF and keeping a correlation (MAF system / MAF bench) acceptable for higher MAF. This change explains the area at low rpm & part load where MAF_DIF reach -5% during the first validation.
To correct this error, eff_vol_flow_cor was activated and tuned from 1000 to 2400rpm. This function permits to a supercharger engine to model MAF as a curve instead of a line, function of the ratio MAP / PRS_EX. and engine speed. In our case PRS_EX is fixed to 1013This calibrations was validated with the last engine characterisation, EDTR145 TEST 17, results were correct, see to the graphs page 11
For the table of IP_AR_RED_THR, original breakpoints at 13% and 17% of TPS_SEG were changed for breakpoints 30% and 40 % in order to be more accurate at high load and high rpm.
Author : F. ANTONIO page10/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
5 VALIDATION AND GRAPHSFull engine characterisation (EDTR145 TEST 11) was performed to validate the overall calibrated function. Air path was validated from this test. More detail in report TEST 11.
TIA_THR comparison between bench and system:Inlet air temperature was regulated to 25°C
Engine Name :Proton 1.6L IAFM +
Ron 95 commercialComments :Date :EASY UECU :
Calibration file :
19/03/2010
U0120A_IAFM_PLUS_16_EDT_20100306_dc12.s19
PM
E (
ba
r)
0
1
2
3
4
5
6
7
8
9
10
11
12
13
Engine speed (rpm)
1000 1250 1500 1750 2000 2250 2500 2750 3000 3250 3500 3750 4000 4250 4500 4750 5000 5250 5500 5750 6000 6250 6500
2
-2
-1
-1
-1
-1
1
1
1
0
0
1
-2-2
-1-3-1
-0-011
-2
-1
-1
Differences on TIA_THR Temperature (System-Bench) [°C]
-3
-2
-1
0
1
2
3
Author : F. ANTONIO page11/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Air path validation without eff_vol_flow_cor calibration:
Engine Name :Proton 1.6L IAFM +
Ron 95 commercialComments :Date :EASY UECU :
Calibration file :
19/03/2010
U0120A_IAFM_PLUS_16_EDT_20100306_dc12.s19
PM
E (
ba
r)
0
1
2
3
4
5
6
7
8
9
10
11
12
13
Engine speed (rpm)
1000 1250 1500 1750 2000 2250 2500 2750 3000 3250 3500 3750 4000 4250 4500 4750 5000 5250 5500 5750 6000 6250 6500
-3
-3-4
-4-2
-2
21
1
0
0
-1
-1
-1
0
-1-1
-1-1-0
1212
2
1
-4
Difference MAF (Bench/System) [%]
-5
-4
-3
-2
-1
0
1
2
3
4
5
-5
-4
-3
-2
-1
0
1
2
3
4
5
Air path validation after eff_vol_flow_cor calibration:
Author : F. ANTONIO page12/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Author : F. ANTONIO page13/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
IP_AR_RED_THR :
1 2 3 4 5 7 9 11 15 20 25 30 35 40 50 82BM3_1.6_dc004 original 0.12 0.15 0.19 0.25 0.33 0.46 0.64 0.88 1.09 1.32 1.50 1.80 2.94 4.80 9.00 16.34ETB3_1.6L final mapping 0.07 0.12 0.17 0.23 0.29 0.43 0.59 0.78 1.21 1.79 2.58 3.66 4.94 7.00 12.81 13.50
IP_AR_RED_THRtps_seg (%)
IP_AR_RED_THR
0
1
2
34
5
6
7
8
9
10
1112
13
14
15
0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90
TPS (%)
IP_A
R_R
ED
_TH
R
BM3_1.6_dc004 original ETB3_1.6L final mapping
IP_TPS_SP_MDL_BAS
0
10
20
30
40
50
60
70
80
90
0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0 6.5 7.0 7.5 8.0 8.5 9.0 9.5 10.0
10.5
11.0
11.5
12.0
12.5
13.0
13.5
14.0
14.5
IP_AR_RED_THR
TP
S (
%)
Author : F. ANTONIO page14/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
validation_calibration_ UO120A_IAFM_PLUS_16_EDT_20090119_dc04_1 (C_PQ_PUT_CTL=0.53)
-30
-25
-20
-15
-10
-5
0
5
10
15
20
25
30
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30
TPS (%)
AR
_RE
D_D
IF_R
EL
(%
)
1000rpm 1500rpm 2000rpm 3000rpm 4000rpm 5000rpm 6000rpm
validation_calibration_ UO120A_IAFM_PLUS_16_EDT_20090119_dc04_1 (C_PQ_PUT_CTL=0.53)
-30
-25
-20
-15
-10
-5
0
5
10
15
20
25
30
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 40 42 44 46 48 50 52 54 56 58 60 62 64 66 68 70 72 74 76 78 80 82 84
TPS (%)
PU
T_M
DL
_DIF
_RE
L (
%)
1000rpm 1500rpm 2000rpm 3000rpm 4000rpm 5000rpm 6000rpm
Author : F. ANTONIO page15/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Volumetric efficiencies determination, first test:VIM OFF:
Air path at 800rpm
0
5
10
15
20
25
30
35
40
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-4
-3
-2
-1
0
1
2
3
4
MAF_bench MAF_Air_path
Error_MAF
Air path at 1000rpm
0
5
10
15
20
25
30
35
40
45
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-4
-3
-2
-1
0
1
2
3
4
5
MAF_bench MAF_Air_path
Error_MAF
05
1015202530354045505560
200 300 400 500 600 700 800 900 1000 1100
-6-5-4-3-2-10123456
0
10
20
30
40
50
60
70
80
200 300 400 500 600 700 800 900 1000 1100
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0Air path at 1200rpm
05
1015202530354045505560
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-6-5-4-3-2-10123456
MAF_bench MAF_Air_path
Error_MAF
Air path at 1600rpm
0
10
20
30
40
50
60
70
80
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
MAF_bench MAF_Air_path
Error_MAF
0
10
20
30
40
50
60
70
80
90
100
200 300 400 500 600 700 800 900 1000 1100
-2.5
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
2.5
0102030405060708090
100110120130140
200 300 400 500 600 700 800 900 1000 1100
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
Air path at 2000rpm
0
10
20
30
40
50
60
70
80
90
100
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-2.5
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
2.5
MAF_bench MAF_Air_path
Error_MAF
Air path at 2400rpm
0102030405060708090
100110120130140
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
MAF_bench MAF_Air_path
Error_MAF
0102030405060708090
100110120130140150160
200 300 400 500 600 700 800 900 1000 1100
-4.0-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.54.0
0
20
40
60
80
100
120
140
160
180
200
200 300 400 500 600 700 800 900 1000 1100
-5
-4
-3
-2
-1
0
1
2
3
4
5
Author : F. ANTONIO page16/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Air path at 3000rpm
0102030405060708090
100110120130140150160
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-4.0-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.54.0
MAF_bench MAF_Air_path
Error_MAF
Air path at 3600rpm
0
20
40
60
80
100
120
140
160
180
200
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-5
-4
-3
-2
-1
0
1
2
3
4
5
MAF_bench MAF_Air_path
Error_MAF
0
20
40
60
80
100
120
140
160
180
200
220
200 300 400 500 600 700 800 900 1000 1100
-2.5
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
2.5
3.0
020406080
100120140160180200220240
200 300 400 500 600 700 800 900 1000 1100
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
Air path at 4000rpm
0
20
40
60
80
100
120
140
160
180
200
220
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-2.5
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
2.5
3.0
MAF_bench MAF_Air_path
Error_MAF
Air path at 4400rpm
020406080
100120140160180200220240
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
MAF_bench MAF_Air_path
Error_MAF
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
Air path at 4600rpm
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
MAF_bench MAF_Air_path
Error_MAF
Air path at 4800rpm
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
MAF_bench MAF_Air_path
Error_MAF
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
020406080
100120140160180200220240260280
200 300 400 500 600 700 800 900 1000 1100
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
Air path at 5400rpm
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
MAF_bench MAF_Air_path
Error_MAF
Air path at 5800rpm
020406080
100120140160180200220240260280
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
MAF_bench MAF_Air_path
Error_MAF
020406080
100120140160180200220240260280
200 300 400 500 600 700 800 900 1000 1100
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
020406080
100120140160180200220240260280
200 300 400 500 600 700 800 900 1000 1100
-3.5
-2.5
-1.5
-0.5
0.5
1.5
2.5
3.5
Author : F. ANTONIO page17/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Air path at 6200rpm
020406080
100120140160180200220240260280
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
MAF_bench MAF_Air_path
Error_MAF
Air path at 6500rpm
020406080
100120140160180200220240260280
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.5
-2.5
-1.5
-0.5
0.5
1.5
2.5
3.5
MAF_bench MAF_Air_path
Error_MAF
Author : F. ANTONIO page18/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
VIM ON:
Air path at 800rpm
0
5
10
15
20
25
30
35
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3
-2
-1
0
1
2
3
4
MAF_bench MAF_Air_path
Error_MAF
Air path at 1000rpm
0
5
10
15
20
25
30
35
40
45
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-4
-3
-2
-1
0
1
2
3
4
5
MAF_bench MAF_Air_path
Error_MAF
05
1015202530354045505560
200 300 400 500 600 700 800 900 1000 1100
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
05
101520253035404550556065707580
200 300 400 500 600 700 800 900 1000 1100
-4.0-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.54.0
Air path at 1200rpm
05
1015202530354045505560
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
MAF_bench MAF_Air_path
Error_MAF
Air path at 1600rpm
05
101520253035404550556065707580
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-4.0-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.54.0
MAF_bench MAF_Air_path
Error_MAF
0
10
20
30
40
50
60
70
80
90
100
200 300 400 500 600 700 800 900 1000 1100
-2.5
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
2.5
0102030405060708090
100110120
200 300 400 500 600 700 800 900 1000 1100
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
Air path at 2000rpm
0
10
20
30
40
50
60
70
80
90
100
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-2.5
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
2.5
MAF_bench MAF_Air_path
Error_MAF
Air path at 2400rpm
0102030405060708090
100110120
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
MAF_bench MAF_Air_path
Error_MAF
0102030405060708090
100110120130140
200 300 400 500 600 700 800 900 1000 1100
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
0
20
40
60
80
100
120
140
160
180
200 300 400 500 600 700 800 900 1000 1100
-4
-3
-2
-1
0
1
2
3
4
5
Author : F. ANTONIO page19/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Air path at 3000rpm
0102030405060708090
100110120130140
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
MAF_bench MAF_Air_path
Error_MAF
Air path at 3600rpm
0
20
40
60
80
100
120
140
160
180
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-4
-3
-2
-1
0
1
2
3
4
5
MAF_bench MAF_Air_path
Error_MAF
0
20
40
60
80
100
120
140
160
180
200
220
200 300 400 500 600 700 800 900 1000 1100
-2.5
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
2.5
3.0
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
Air path at 4000rpm
0
20
40
60
80
100
120
140
160
180
200
220
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-2.5
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
2.5
3.0
MAF_bench MAF_Air_path
Error_MAF
Air path at 4400rpm
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
MAF_bench MAF_Air_path
Error_MAF
020406080
100120140160180200220240
200 300 400 500 600 700 800 900 1000 1100
-6-5-4-3-2-10123456
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
-6-5-4-3-2-101234567
Air path at 4600rpm
020406080
100120140160180200220240
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-6-5-4-3-2-10123456
MAF_bench MAF_Air_path
Error_MAF
Air path at 4800rpm
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-6-5-4-3-2-101234567
MAF_bench MAF_Air_path
Error_MAF
020406080
100120140160180200220240260280
200 300 400 500 600 700 800 900 1000 1100
-7-6-5-4-3-2-101234567
020406080
100120140160180200220240260280300
200 300 400 500 600 700 800 900 1000 1100
-7-6-5-4-3-2-1012345678
Author : F. ANTONIO page20/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Air path at 5400rpm
020406080
100120140160180200220240260280
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-7-6-5-4-3-2-101234567
MAF_bench MAF_Air_path
Error_MAF
Air path at 5800rpm
020406080
100120140160180200220240260280300
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-7-6-5-4-3-2-1012345678
MAF_bench MAF_Air_path
Error_MAF
020406080
100120140160180200220240260280300
200 300 400 500 600 700 800 900 1000 1100
-8-7-6-5-4-3-2-101234567
020406080
100120140160180200220240260280300320
200 300 400 500 600 700 800 900 1000 1100
-4.0-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.54.0
Air path at 6200rpm
020406080
100120140160180200220240260280300
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-8-7-6-5-4-3-2-101234567
MAF_bench MAF_Air_path
Error_MAF
Air path at 6500rpm
020406080
100120140160180200220240260280300320
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-4.0-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.54.0
MAF_bench MAF_Air_path
Error_MAF
Author : F. ANTONIO page21/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Air path evolution:After the first engine characterization slope and offset were adjusted at 800rpm, 1000rpm, 1200rpm, 1600rpm, 2400rpm and 5400rpm.
Air path at 800rpmVIM OFF
0
5
10
15
20
25
30
35
40
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-10
-8
-6
-4
-2
0
2
4
6
8
10
MAF_Air_path_old MAF_AIRPATH_New
Error_MAF_old Error_MAF_newAir path at 1000rpm
VIM OFF
0
5
10
15
20
25
30
35
40
45
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)M
AF
(kg
/h)
-4
-3
-2
-1
0
1
2
3
4
5
MAF_Air_path MAF_AIRPATH_New
Error_MAF Error_MAF_New
05
1015202530354045505560
200 300 400 500 600 700 800 900 1000 1100
-6-5-4-3-2-10123456
0
10
20
30
40
50
60
70
80
200 300 400 500 600 700 800 900 1000 1100
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
Air path at 1200rpmVIM OFF
05
1015202530354045505560
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-6-5-4-3-2-10123456
MAF_AIRPATH_New MAF_Air_path
Error_MAF_New Error_MAF
Air path at 1600rpmVIM OFF
0
10
20
30
40
50
60
70
80
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
MAF_Air_path_New MAF_Air_path
Error_MAF_New Error_MAF
0
10
20
30
40
50
60
70
80
90
100
200 300 400 500 600 700 800 900 1000 1100
-2.5
-2.0
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
2.0
2.5
0102030405060708090
100110120130140
200 300 400 500 600 700 800 900 1000 1100
-7-6-5-4-3-2-101234567
Air path at 2400rpmVIM OFF
0102030405060708090
100110120130140
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-7-6-5-4-3-2-101234567
MAF_Air_path MAF_Air_path_New
Error_MAF Error_MAF_New
0102030405060708090
100110120130140150160
200 300 400 500 600 700 800 900 1000 1100
-4.0-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.54.0
0
20
40
60
80
100
120
140
160
180
200
200 300 400 500 600 700 800 900 1000 1100
-5
-4
-3
-2
-1
0
1
2
3
4
5
020406080
100120140160180200220
200 300 400 500 600 700 800 900 1000 1100
-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
020406080
100120140160180200220240
200 300 400 500 600 700 800 900 1000 1100
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
020406080
100120140160180200220240260
200 300 400 500 600 700 800 900 1000 1100
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.0
0.0020.0040.0060.0080.00
100.00120.00140.00160.00180.00200.00220.00240.00260.00280.00300.00
200 300 400 500 600 700 800 900 1000 1100
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.54.0
020406080
100120140160180200220240260280300
200 300 400 500 600 700 800 900 1000 1100
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.54.0
Author : F. ANTONIO page22/23
CopyrightAll rights reserved.
G_106G_106
AIR
PA
TH
CA
LIB
RA
TIO
NA
IRP
AT
H C
ALI
BR
AT
ION
Pro
prie
tary
da
ta,
com
pan
y co
nfid
entia
l. A
ll rig
hts
res
erv
ed
.C
on
fié à
titr
e d
e s
ecr
et
d’en
tre
pris
e. T
ous
dro
its r
ése
rvés
.C
om
un
icad
o c
omo
segr
edo
em
pras
eria
l. R
ese
rvad
os
tod
os o
s de
reito
s.C
on
fida
do
com
o s
ecre
to in
du
stria
l. N
os
rese
rvam
os t
odo
s lo
s de
rech
os
Wei
terg
abe
sow
ie V
erv
ielfä
lfig
ung
die
ser
Un
terl
age
, Ver
wer
tun
g u
nd
Mitt
eilu
ng
ihre
s In
ha
lts n
ich
t g
esta
ttet
, so
wei
t n
ich
t au
sdrü
cklic
h zu
gest
and
en.
Zu
nwid
erh
and
lun
gen
ve
rpfli
chte
n z
u S
chad
ene
rast
z.
Alle
Rec
hte
vo
rbe
halte
n, in
sbes
on
dere
für
de
n F
all
de
r P
ate
nte
rte
ilung
od
er
GM
-Ein
tra
gun
g
PT TC2ENGINE DYNO TEST
Air path at 5400rpmVIM ON
0.0020.0040.0060.0080.00
100.00120.00140.00160.00180.00200.00220.00240.00260.00280.00300.00
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.54.0
MAF_Air_path MAF_Air_path_New
Error_MAF Error_MAF_New
Air path at 5800rpmVIM ON
020406080
100120140160180200220240260280300
200 300 400 500 600 700 800 900 1000 1100
MAP system (mbar)
MA
F (
kg/h
)
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.54.0
MAF_Air_path MAF_Air_path_New
Error_MAF Error_MAF_New
020406080
100120140160180200220240260280
200 300 400 500 600 700 800 900 1000 1100
-3.5-3.0-2.5-2.0-1.5-1.0-0.50.00.51.01.52.02.53.03.5
020406080
100120140160180200220240260280
200 300 400 500 600 700 800 900 1000 1100
-3.5
-2.5
-1.5
-0.5
0.5
1.5
2.5
3.5
Author : F. ANTONIO page23/23
CopyrightAll rights reserved.
G_106G_106