Rotor : Lighter, rotor recess shape change to increase compression ratio
2.
Tension bolt : Strengthening ribs added
3.
Front cover : Shape changed for new metering
4.
Side housings : Inlet port erea enlarged
STRUCTURAL VIEW
HOUSING-RELATED PARTS
in
the 1989
RX-7
is
basically the same as
FRONT HOUSING
in
the previous model but with some modli
oil
pump
FRONT ROTOR HOUSING
c:=:-
_
FRONT OIL SEAL
._)
REAR HOUSING
REAR ROTOR HOUSING
INTERMEDIATE
HOUSING
C-2
·-
97UOCX·502
Page 5
;:;'"'TA
~
TING-RELATED
PARTS
BALANCE WEIGHT
ECCENTRIC PULLEY
REAR ROTOR
' •
FRONT ROTOR
DRIVE PLATE
COUNTER WEIGHT
FLYWHEEL
-.
C-3
Page 6
SPECIFICATIONS
cc
Model
(cu
1n)
Item
Eng1ne type Rotary eng1ne
Displacement
Number
Combustion
Compression
A1r
Port
of cyl1nders and
chamber
Induction
t1m1ng
rat10
Intake
Exhaust
arrangement
type
Open
Close
Open
Close
Pnmary 4S0 ATOC
Secondary
Auxiliary
Pnmary
Secondary
Auxil1ary
Turbo Non-Turbo
6S4 X 2 (40.0 X
2 rotors. longitudinal
Bathtub
9.0 1
4 port
1nduct1on
32°
ATOC
S0°
ABOC
soo
ABOC
0
7S
BBDC
48°
ATOC
2)
6 port
32°
4S
40°
30°
80"
9.7 1
1nduct1on
ATOC
0
ATOC
ABOC
ABOC
ABOC
~~
\
Fuel
supply
lgn1t1on
(Green
Idle
grounded)
t1ming
1-p1n)
speed
system EGI
(w1th
grounded)
(w1th
test
test
connector
connector
(Green
Tra1l1ng
Lead1ng
1-pln)
rpm
± 2 ' ATOC (REO)
20°
so
±
1 o ATOC (YELLOW)
750 ± 25
l,~
97UOCX 504
C-4
Page 7
INTERCHANGEABILITY
:::
,.,,ng
chart shows interchangeability of major components of the previous model and the 1989 mode'
X Not interchangeable
...
ousmg-
·~
ated
;:.a
r1S
;;
:~at1ng-
-~
a~ed
=~~s
Part
Front rotor hous1ng
Rear rotor hous1ng
Front
hous1ng
i ntermed1ate housing
Rear housing
seal1ng
nner
Outer sealing rubber
Front cover
Orl
pan
Tens1on
::ccentnc shaft
Rotor
~~pex
S de
seal
:::orner
3a',ance weight I
J I pump dnve sprocket
: :centr1c
'C
=centnc shaft bypass valve - -
~
. ·ey lock bolt
~
.
:.
heel
• · beanng
.1ter
rubber
bolt
seal
seal
shaft pulley t
(MIT)
(MIT)
we1ght
(A/T)
-1
. -
i
---1
I
+
J
-~·
.
l
I,
Interchangeability
X
X
0
X
0
X
0
X
0
0
0
X
0
X
0
0
X
0
X
Remark
• Knock sensor boss added
• Inlet port area enlarged
• Shape changed to Incorporate new
tng
Oil
pump
• Ribs added
•
We1ght
•
Combustion chamber shape changed
• Shape changed
• Shape changed
• Shape changed
•
We1ght
•
Shape changed
•
We1ght
'
to
center of shank
reduct1on
reduct1on
reduct1on
metw
•
C-5
Page 8
TENSION BOLT
...
OTHERS
No.18 BOLT
(}1
T
STRENGTHNING RIBS
128 ± 2mm
HEAT-SHRINK PROTECTOR
lllllllllllllllllllllllllllllll
(5.04 ± 0.08 in)
NOTE
No.1? SOL
OTHERS. THERE IS AN IDENTIFICATION
The strength of the tension bolts
The tension
transmiss1on of eng1ne noise. To reduce this noise. the heat-shrik protector
through the intermediate housing boss. The No. 18
protector).
shrunk
bolt installed into the No. 18 hole differs from others
If
the bolt
w1th
a l1ghter or match.
T IS LONGER THAN
MARK.
1s
increased by addit1on of strengthening ribs
is
reused and the protector
No.18 BOLT
bolt
is
damaged, replace the protector. The protector
C-6
in
that
is
supplied as an assembly (bolt
in
the middle of the shank.
it
is
not fully enclosed. lead1ng to
is
used on the bolt where
w1th
washer and
97UOCI 506
1t
goes
1s
easily
Page 9
,
.•
FRONT COVER
FRONT COVER GASKET
FRONT COVER
~.
~BACKUP
0-RING
RING
•
~
· 989
:::::ded
RX-7
front cover
between the front cover and front housing for improved sealing.
is
changed to incorporate a new metering
C-7
oil
97UOCX 507
pump.
Page 10
ROTOR
TURBO
RIBS
NON-TURBO
RIBS
~
~
\
A
/J
I
c--~~
v
A A
~
A~
1 0.9mm (0.43 in)
,_
4
8.8mm (0.35 in)
r---/1
~-
The rotor
9.7 :
These improvements
The rotor ribs are redesigned for increased strength.
The combustion chamber rotor recess
The rotor for turbo and non-turbo engines are distinguished by the rotor recess shape.
in
the 1989
1 for non-turbo model) than the previous engine.
RX-7
results
is
lighter and provides a higher compression ratio (9.0 : 1 for turbo model and
in
a engine with more power and torque.
1s
made more uniform by utilizing a mechanical cutting process.
97UOCX 508
C-8
Page 11
...
D
LUBRICATION SYSTEM
OUTLINE
OUTLINE OF CONSTRUCTION
STRUCTURAL VIEW
SPECIFICATIONS
INTERCHANGEABILITY
Low pressure
High pressure _
Type
Regulated pressure
Type
Outlet pressure kPa (kg/cm
Dr1ve
InJeCtion
Operation temperature
Capac1ty cc (cu
Type
Type
A/C
"D"
range
Model
1-p1n)
grounded) rpm
Secondary
Operat1on temp.
l1ters
(US gal. Imp gal)
kPa (kg/cm
volume cc (cu ln)/15 sec. i
t1me
mm
oc
2
2
oc
(In)
(1n)
(oF)
,
ps1)
,
ps1)
(°F) i
in)
rpm
rpm
sec.
138
EGI
750 ± 25 (for AlT
Long
Honzontal -draft
45 (1.772)
(1
45
M/T.
67-77
A/T
60-70
Nylon
235-275
441-588
MIT 10.300 (628.3) x
Lead1ng
Tra1l1ng
(153-171)
(140-158)
2,700-3.100
70 (18.5, 15.4)
6 (164 and 45 mesh)
F1lter
D1aphragm
(2.4-2.8,
Impeller
(4.5-6
Voltage dnve
111-118
105-115
20° ± 2°
Eng1ne
Eng1ne
MIT. 875 A/T 800
750
(at warm
L1near
MIT
AlT. 0
engine
..
N Range)
l1fe
wet
(2
slaj:l~---
772) X 2
paper
34.1-39
(1ntank)
0,
64.0-85
(6.8-7.2)
(221-239)
2,
A/T
5°
± 1 o ATDC
control
control
1.60-2.20
un1t
un1t
eng1ne)
soleno1d
52-0.92
3 barrel)
or more
or more
8)
3)
12.000 (732) x 2
ATDC
97UOF1 511
F1-11
Page 35
VARIABLE DYNAMIC EFFECT INTAKE (VOl) SYSTEM
~.-
s systern cors.sts of the VOl valve, solenoid valve, and actuator. The
.
~
::::
Ooerat
-OeENGINE
~=EED
on
of
th1s
system
OPEN V %
~
,
·.
is
as shown below.
~
0
HIGH ENGINE SPEED J
(VDI VALVE: OPEN CONDITION)
VOl
valve
is
built into the exten mani-
VDI VALVE
= INTAKE AIR
·~
PRESSURE WAVE
•
co...,
I
..
.....
• • • PRESSURE WAVE
ABOVE
5,200
::
:.·,.;
ANGLE SENSOR
:
-::~;Jine
:
·-::::s~re
~~-::speed,
.
::: . ::
·· . ::
:·-::
,·
;:::s
operation, when intake air flows to a port closed by the rotor a pressure wave
wave then goes toward the open intake port, compressing the intake air along the way.
the VOl valve
. e opens and the pressure wave quickly pressurizes the intake air through the shortened path.
'::xced
c-essunzation
1nto
remaining
VDI VALVE
OPENING
AREA
LARGE
rpm
_______
INTAKE AIR
AMOUNT
is
closed, causing the pressure wave path to be long. At high engine speed,
the combustion chamber
is
induced at the time of the opening of the intake port, when the high-pressure
in
the working chamber generates strong pressure waves that rush into the intake
at
all
engine speeds.
(m1/h)
SMALL~--------~------~
0
ENGINE SPEED
JI
5,200 8,000
(rpm)
97UOF1
is
created.
509
At
F1-12
Page 36
FUEL SYSTEM
MIXING PLATE
INJECTOR
SECONDARY
INJECTOR
AIR
SOCKET
BLEED
AIR
BLEED
SOCKET
· 19 plate
·
:J.ke
air port.
97UOF2-508
is
installed at the tip of primary Injector to direct the primary fuel inJection fuel directly into
F1-13
Page 37
SERVICE POINT
PULSATION
®----INSULATOR
NEW 0-RING
~======s~~----AIR
INTERMEDIATE
HOUSING
'---"
~MIXING
BLEED SOCKET
PLATE
~·
MIXING PLATE
The pr1mary inJector
1 Install the parts
2 Use a new
3
A1
gn 1re 1abs
in
Insulator and 0-rings.
of
NOTCH
is
installed noting the following:
the order shown
the mixing plate with the notches
in
the figure.
F1-14
TAB
in
the intermediate housing.
'UDF2 509
~··
Page 38
CONTROL SYSTEM
AIRFLOW METER
SLIDING CORE
INTAKE
THERMOSENSOR
AIR
~
CONNECTOR
I
AIR BYPASS
PASSAGE
INTAKE AIR
THERMOSENSOR
t
AIRFLOW METER
t
~-.
-~
eter
-
:
Jn.
97UOF2-513
is
changed from a vane type to a linear type. The sliding core moves parallel to the airflow
there
is
little air damping and low air resistance
as
a result of the streamlined shape.
F1-15
Page 39
THROTTLE-IDLE-POSITION AUTO-ADJUSTING SYSTEM
· · · SENSOR OPEN
~·
NARROW
FULL
RANGE
NARROW
FULL RANGE
RANGE
RANGE
SENSOR
CLOSED
(0%)
150/o
SENSOR
OPEN (100%)
I
: APPROX.
I
SENSOR CLOSED
AUTO-ADJUSTING
___..~
300/o
SENSOR CLOSED
SENSOR OPEN
AREA
SENSOR
OPEN (100%)
50/o
.:.
··e:.ly
developed
-· ~ system automatically
.:. · =:
e
tre
narrow range throttle sensor
:
=:::on
·
.:: S-::
~:::erat1on
c.·
,
auto-adJUSting system, the eng1ne control unit will compensate for actual output values of
···
e output
respectively for fail-safe operation
:;;
~e
:::
25° o respect1vely for fall-safe operation.
is
for the full range sensor
control
throttle-idle-position auto-adjusting system
less than
un1t
15%
compensates
I~
I~
:
THROTTLE AUTO-ADJUSTING AREA
IDLE
POSITION
compensates
or
more
within the range from
250/o
~'
for certain variations
is
set to
output
than
25%
at idle, the engine control
is
the same. The sensor
is
in
a signal of
is
set to reg1ster a
5%-25%.
850/o
I
FULL
THROTTLE
97UOF2 514
incorporated
the output signal of the throttle sensors .
20%
w1thin
of full-open. With the throttle idle-
the engine control unit.
15%-25%.
un1t
If
over or
fixes the value
15°/o
s1gnal
under
the s1gnal1s fixed at
at
at
1dle,
15%
and the
and
5%
\.!.
F1-16
Page 40
LEAN BEST-IDLE CONTROL SYSTEM
WATER THERMO
INHIBITOR
SWITCH
(A/T )
SENSOR
EC-AT
CONTROL
UNIT
~
rL
NEUTRAL SWITCH (M/T
CLUTCH
PiS PRESSURE SWITC
:::EAR DEFROSTER SWITCH
SWITCH (M/T
A/C SWITCH
BLOWER SWITCH
HEADLIGHT SWITCH
FOG LIGHT SWITCH
(ONLY
CANADA
)
)
H
)
I
~
---c:
=
~~LE
SENSOR (NARROW
RANGE)
ENGINE CONTROL UNIT
DETECTION OF ENGINE
WARM CONDITION
DETECTION OF ENGINE
NO-LOAD CONDITION
(ONLY FOG LIGHT SWITCH:
DETECTION OF
ENGINE LOAD CONDITION)
--
DETECTION OF ENGINE
IDLE CONDITION
t
~
DETERMINA-
TION
LEAN BEST-
~
f-
IDLE
CONDITION
OF
I
FUEL
INJEC-
TOR
BATTER
y
re
--o ••
• ANGLE SENSOR (NE
. _
-::j
fuel consumption and reduced exhaust emissions
·.V1th
this system, the engine control unit sets fuel injection
- .
:;1ng
lean misfire and rough idle.
SIGNAL)
DETERMINATION OF LEAN
BEST-IDLE AMOUNT
at
idle, the lean best-idle control system
F1-17
K
97UOF2-515
at
idle to the leanest amount possible
is
Page 41
SPARK ADVANCE FEEDBACK SYSTEM (ENGINE AT IDLE)
SPARK
ADVANCE
FEEDBACK
AMOUNT
DETECTION OF
ENGINE IDLE
THROTTLE SENSOR
(NARROW RANGE)
CONDITION
1
I
-50-------------~------~----
oo
- - - - - - - - -,..---'--'
I
1
I
CRANK
SENSOR (NE SIGNAL)
ANGLE
DETERMINATION
OF
ADVANCE
SPARK
FEEDBACK
AMOUNT
I
IGNITION COIL
'
RS
rpm
DECREASED
TS:
RS:
TS
TARGET ENGINE SPEED
REAL ENGINE SPEED
RS
INCREASED
rpm
To
prevent rough idle caused by incorrect idle speeds, the spark advance feedback system controls the
spark advance. The engine
tion
timmg to
obta1n
the preprogrammed target speed
control unit judges the engine speed (real speed:
(TS).
RS)
and then adjusts the igni-
F1-18
LJ7UOF2
516
Page 42
SERVICE POINT
THROTTLE SENSOR ADJUSTMENT
IDLE MIXTURE ADJUSTMENT
/
.....
__________________________
::::' adJUStment: Not usually necessary unless throttle sensor unit
auto-adjusting system automatically compensates.
~
JJustment
Not
necessary because of lean best-idle control system. (Varrable
eliminated.)
F1-19
is
replaced.
_
Th
rottle-rdle-pos ~ :::
res
~-
~
=-
Page 43
SELF-DIAGNOSIS FUNCTION
DESCRIPTION
When troubles are suspected
Failures of individual input and output devices are indicated and retrieved from the control unit as malfunc-
tion
code
numbers.
Note
The control unit constantly checks for malfunction of the input devices.
tion of output devices only during a 3-second period after the ignition switch has been turned
ON
while the test connector
in
the
ma1n
is
1nput
devices or output devices, check for the cause with the SST.
grounded.
It checks for malfunc-
IGNITION COIL
WITH
IGNITER---
(TRAILING SIDE)
~JE~~~~::LEJ~~-~
CRANK ANGLE '
SENSOR (G-SIGNAL)
~
_
---.
---,
FAIL-SAFE
FUNCTION
_L
WATER
THERMOSENSOR
AIRFLOW~
METER
INTAKEAIR
THERMOSENSOR
(AFM)
INTAKE AIR
THERMOSENSOR /
(ENGINE)
~~
~
\)
~
~
--
/
DETECTION
OF
MALFUNCTION
WARNING
FUNCTION
&
MALFUNCTION
CODE
FUNCTION
-
-
-=-
~
~
Wu~~~~:GE;-1
~
THROTTLE~
SENSOR Q
(NARROW-RANGE) .
PRESSURE--SENSOR
OXYGEN
METERING
PUMP POSITION c o
SENSOR o
SENSOR-\
OIL--~~1._
-~---·-
-
·-
1
-o
.__/
-~
-----'
ATMOSPHERIC
PRESSURE
SENSOR
TEST CONNECTOR
(GREEN: 1-PIN)
F1-20
97UOF2-024
Page 44
MALFUNCTION CODE NUMBER
SST
Jg H018
3elf-Dragnosis
Checker
9A1
SHF
UIAGIIlSrS
97UOF1-512
CHfClER
Inspection Procedure
1.
Warm
stop
2.
Connect the SST to the check connector (Green: 6-pin) and
the negative battery
Set the select switch to position
3.
Connect a jumper
1-pin)
up
the
engine
it.
and a body
to normal
operating
terminal.
A.
wire between the test
ground.
temperature
connector
(Green:
and
,..
• • I
I~
:: :
J.AGNOSIS
~-,
11\T/"
• G
·1cr1:o:
G/
1_1.11_1!
0
~-,'-[-\-'---\-'-
SElF
--~
DIAGNOSIS
~
CHECKER
MALFUNCTION
V CODE NUMBER
::111-:1/
--
--
CHECKER
97UOF1
97UOF1
514
510
4.
Turn the ignition switch ON.
5.
Check
sounds
6.
If
7.
If
than 20 sec.,
control unit
And
voltage. Replace
88
88
that
88
flashes on the digital display
and
the buzzer
for 3 sec. after turning the ignition switch ON.
does
flashes
check
not flash,
and
check
(1
F)
the
check
the buzzer
the
check
sounds
continuously for
for a short circuit between the
terminal and
engine
the
check
control unit
engine
control unit
connector (Green: 6-pin).
(3X)
connector
and (3Z) terminal
if
necessary
perform Step 4 again.
8.
Check
9.
Start the
for any malfunction
engine
and
check
code
numbers.
for further malfunction
numbers.
10.
If
a malfunction
cause of the
code
problem.
number
is
indicated,
check
Note
Cancel the malfunction code numbers by performing
the after-repair procedure
following repairs.
F1-21
wiring.
more
engine
and
code
for the
Page 45
Principle of code cycle
Malfunction codes are determined
1.
Malfunction code cycle break
The time between malfunction
as
below by use of the MIL and Self-Diagnosis Checker
code
cycles
is
4.0 sec. (the time the MIL and checker buzzer are off).
97UOF1-515
1 CYCLE
ON
OFF
MALFUNCTION CODE
CYCLE
4.0 SEC.
2. Second digit of malfunction code (ones position)
The digit
are on
in
the ones position of the malfunction code represents the number of times the MIL and buzzer
0.4 sec. during one cycle.
4
0.4
~---~
MALFUNCTION
CYCLE BREAK
4.0 SEC.
1 CYCLE CODE
ON
JU\fl"
OFF
-1--!-
0.4
SEC. SEC.
BREAK
ffilll
-----
9MUOF 1
543
CODE No.: 03
89lll!4X
565
3. First digit of malfunction code (tens position)
The digit
are on 1
The MIL and buzzer are off for 1.6 sec. between the long and short pulses.
in
the tens position of the malfunction code represents the number of times the MIL and buzzer
.2
sec. during one cycle.
1 CYCLE
;-----~----.,
FIRST DIGIT SECOND
1.6 4.0 SEC.
SEC.
MALFUNCTION
CODE
CYCLE
BREAK
DIGIT
F1--22
CODE
No.
89U04X
22
566
Page 46
Code number
Caution
a)
If there
is
more than one failure present, the lowest number malfunction code
first, the subsequent malfunction codes appear
b)
After repairing
ble,
at least 5 seconds to erase the malfunction code memory.
In
put devices
all
failures, turn the ignition switch OFF, disconnect the negative battery ca-
in
order.
is
displayed
Code
No.
l'
:2
devices
Input
lgn1110n
with
(Trail1ng
Crank angle sensor Broken
(Ne
coil
1gn1ter
s1de)
s1gnal)
Malfunction
plug. broken
ClfCUit
c1rcuit
Malfunction
of spark
w1re.
w1re.
short
short
Fail-safe function
T
rail1ng-s1de
pulse cut
Fuel
InJeCtion
1 lion cut
1gn1t1on
and
1gn1-
Output signal pattern
(Self-Diagnosis Checker or MIL)
Jl
I
angle sensor Broken
Crank
(G
s1gnal)
ClfCUit
short Fuel InJection and
w1re.
t1on
cut
1gn1
I
Bas1c
A1rflow
meter (AFM) Broken
Water thermosensor
a1r
Intake
'll
t
thermosensor (AFM)
;ntake
a1r
sensor
Throttle
1Full
Pressure sensor Broken
:
·1take
:Yessure)
-'ltmosphenc pres-
~u
Built
J x ygen sensor
:-
eedback system
-
· •ottle sensor
.arrow range)
'.'eter1ng
· -s,t,on sensor
·
.'
.c:enng
'.'8P)
·.·-:c-:er
'.':JP)
thermo-Broken
(Eng1ne)
sensor
range)
man1fold
re
sensor
(A
ECU)
oil
oil
oil
TP)
pump
pump
pump
1n
:1g
ClfCUII
Broken
ClfCUI!
Broken
ClfCUit
ClfCUit
Broken
ClfCUit
ClfCUII
Malfunct1on1ng ECU
Oxygen
below 0 55V
system
operat1on
Oxygen
ma1ns 0 SSV
system
operat1on
Broken
circuit
Broken
CirCUit
Malfunct1onmg
tors.
broken
or
malfunct10n1ng
Malfunct
on1ng
broken
111re.
1
t:on.ng
ECU.
short
w1re.
w1re.
short
short
w1re.
w1re.
short
short
w1re.
short
w1re.
sensor
output
rema1ns
80
sec
aher
beg1n1ng
sensor
output
· 0
sec
after
begm1ng
short Throttle valve open1ng
w1re.
short
w1re.
MOP.
steo
w1re.
short
ECU
MOP.
step
srort c rcu
t.
rralfunc-
alter1ator
or
'
1
FiB
re
FIB
mo
c1rcu1t
,"lotors
battery
fuel InJection
amount and
t1m1ng
Coolant temp. input
f1xed
Intake
f1xed
Intake
f1xed
Throttle valve open1ng
angle input signal
at
20%
Intake
1nput
mmHg (29.9 inHg)
Atmospheric pressure
1nput
760
mmHg
Feedback system canceled (For EGI)
Feedback system canceled (For EGI)
angle
at
full open
MOP
f1xed
Bas1c
and
1Qn1t1on
MOP
Bas1c
and
1Qn1t1on
Basic fuel
amount and ignit1on
t1m1ng
F1-23
f1xed
at
80°C
a1r
temp.
at
20°C
a1r
temp.
at
20°C
open
man1fold
s1gnal
s1gnal
1nput
smallest
fuel
1nJect1on
f1xed
smallest
fuel
1nj8ct1on
InJeCtion
fixed
1gn1!10n
(176°F)
(68°F)
(68°F)
pressure
f1xed
f1xed
(29.9
s1gnal
t1m1ng
tmng
1nput
1nput
at
amount
f1xed
amoun:
f1xed
f1xed
760
at
1nHg)
f1xed
open
open
..
llll
n
fU
Jll
J1l
run
JUI
rull
JUII[
i
m
Jrull
ImJII
97UOFI-516
Page 47
Output devices
Code
No.
25
! Soleno1d valve (Pressure regulator control (PRC))
Regulated pressure
Type
Output pressure kPa (kg/cm
Dnve
InJeCtion
Operat1on temperature
Capac1ty
Type
Operat1on
Type
volume
(green 1
t1me
--
·-
Primary
Secondary
Operation temp.
l1ters
(US gal, Imp gal)
1
1
Low
H1gh
kPa
cc
(cu ln)/15 sec
p1n)
grounded)
rpm
mm
(1n)
mm
(1n)
oc
(oF)
2
ps1)
,
pressure
pressure
(kg/cm2 ps1)
2
ps1)
,
oc
(°F)
cc
(cu
1n)
rpm
sec
138
Turbocharged engine
750 ± 25
l1fe
Long
Honzontal draft
45
45
55-65
Incorporated
235--275
490-637
1
(131-149)
Water cooled
57.0 (0.58, 8.25)
Engine
70 (18
Nylon 6 (164 & 45 mesh)
F1lter
D1aphragm
(2.4--2.8,
Impeller (In-tank)
(5
Voltage dnve
133
-142
105-:15
12.000 (732) X 2
Leading 5u ± 1 o ATDC
Tratl1ng
Eng1ne control
Eng1ne control
1.60
A1r
~~~
wet
(2
stage-3 barrel)
(1
772)
(1
772) X 2
1.8-3.8
oil
w1th
turbocharger
5,
15.4)
paper
0-6.5,
(8.1-8.7)
(221
20" ± 2°
800
-2.20
cooled
or
34.
1-39.8)
71
1-924)
-239)
ATDC
un1t
un1t
more
97UOF? 519
,..
F2-11
Page 61
FUEL SYSTEM
MIXING PLATE
•
PRIMARY INJECTOR
A mixing plate
the intake air
PRIMARY INJECTOR
is
installed
port.
at
l b
J~
97UOF2 508
the tip of primary injector to direct the primary fuel inject1on fuel directly into
F2-12
\..··
Page 62
SERVICE POINT
NEW
PULSATION DAMPER
0-RING
2
508
into
l-1-----AIR
~----------MIXING
INTERMEDIATE
HOUSING
BLEED SOCKET
PLATE
MIXING PLATE
NOTCH
·
"lary
injector
·::
the parts
-'
"'
new insulator and 0-rings.
is
installed noting the following
in
the order shown
in
the figure.
:he tabs of the mixing plate with the notches
F2-13
TAB
in
the intermediate housing.
Page 63
TURBOCHARGER CONTROL SYSTEM
SYSTEM CONSTRUCTION
INTERCOOLER
SOLENOID
DUTY
•
FRONT ROTOR
AIR CLEANER
TURBOCHARGER
EXHAUST MANIFOLD
(COMPLETELY-INDEPENDENT
TWIN SCROLL TURBO)
97UOF2-51
Two newly developed systems are employed to increase engine horsepower, a newly des1gned completely-
independent twin scroll turbo and a precise turbo boost pressure control system.
F2-14
0
Page 64
COMPLETEL ¥-INDEPENDENT TWIN SCROLL TURBO
PREVIOUS OPEN-TYPE
SIDE HOUSING
ROTOR HOUSING
INTERMEDIATE
HOUSING
ROTOR HOUSING
SIDE HOUSING
COMPLETELY-INDEPENDENT TYPE
SIDE HOUSING
ROTOR HOUSING
INTERMEDIATE
TURBINE
WHEEL
PRESSURE
WAVE
:.
::ompletely-independent twin scroll turbo improves horsepower by utilizing more fully the inherent
··
:.aves created by the escaping exhaust gases.
· -otors
:
:.
as
it
is
directed straight toward the turb1ne wheel. The pressure waves are thus used rather
ed
to mix with the exhaust gases of the opposite rotor.
HOUSING
ROTOR HOUSING
SIDE HOUSING
97UOF2 5 · ·
It
does this by isolating the gas flow of the front
F2-15
Page 65
TURBO BOOST PRESSURE CONTROL SYSTEM
This system controls the turbocharger maximum boost pressure by the duty signal from the engine control unit.
CRANK ANGLE S
(NE SIGNAL)
THROTTLE SENS
(FULL RANGE)
PRESSURE SENS
ENSOR
OR
OR
,-----------------------------l
ENGINE CONTROL UNIT
I I
I I
I I
I I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
L
______
ATMOSPHERIC
PRESSURE
SENSOR
r-
~
~
BASIC
OUTPUT
DUTY SIGNAL
TARGET
BOOST
PRESSURE
REAL
BOOST
PRESSURE
DETERMINATION
u-~OUTPUT
L__
DUTY SIGNAL
FEEDBACK
DUTY SIGNAL
u
_
_________
OF
__j
I
I
I
I
I
I
I
I
I
'
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
BATTERY
DUTY
SOLEN OlD
VALVE
TURBO BOOST MAXIMUM PRESSURE GRAPH
·1
DUTY SIGNAL
ENGINE
CONTROL UNIT
AIR
CLEANER
BOOST!
PRE-
SSURE
ENGINE SPEED
Operation
1.
The duty signal from engine control unit
is
varied from
5%
to
95%
based on information from the full range
throttle sensor and the crank angle sensor (Ne signal). The output duty signal
gine control unit by the
2 The duty signal
3
As
the duty increases, the duty solenoid valve opening increases, and the pressure
1s
bas1c
output duty signal, and feedback duty signal.
sent to the duty solenoid valve from the engine control unit.
ator decreases.
4 The wastegate valve then closes, and the turbo boost pressure increases.
The
eng1ne
The boost pressure
control
un1t
contains the data to set the turbo boost maximum pressure as shown
is
basically determined by the throttle opening angle and engme speed.
SOLENOID
3
ACTUATOR
@)
WASTE GATE
VALVE
97UOF2 512
is
determine within the en-
a1r
actmg on the actu-
in
the graph.
F2-16
Page 66
CONTROL SYSTEM
AIRFLOW METER
INTAKE
THERMOSENSOR
AIR
CONNECTOR
JR I
ATE
AIR
BYPASS
PASSAGE
INTAKE
THERMOSENSOR
AIR
~
lge
er-
ph
-
-=-:c?r
.. -there
1s
changed
from a
is little air
vane
damping
type
to a linear type. The sliding
and
low
air res1stance as a result of
F2-17
core
moves
the
parallel to the
streaml1ned
a,.
sr--::::.:c
_ -
Page 67
CONTROL SYSTEM
AIRFLOW METER
CONNECTOR
INTAKE AIR
THERMOSENSOR
) 512
AIR BYPASS
PASSAGE
INTAKE AIR
THERMOSENSOR
~
AIRFLOW
~
POTENTIOMETER
METER
lge
en-
:tu-
ph.
· _
:.
=:es1gn.
meter
is
changed from a vane type to a
there
is
little air damping and low
l1near
type. The sliding core moves parallel
a1r
res1stance as a result of the streamlined
F2-17
to
the
sr
a,. ~ :.
:::~"'
Page 68
THROTTLE-IDLE-POSITION AUTO-ADJUSTING SYSTEM
_1_ --
NARROW
RANGE
FULL
RANGE
SENSOR
CLOSED
NARROW
RANGE
FULL I
RANGEr-;---~
I
I
5%
,>------L.,--
SENSOR
(0%)
15125%
I....,._
..,...
%1
I
I
1
OPEN
20%
_____
_
15%
I
~'----~:
--~------------------------~~----~
:
I
25%
---
- - -
--
(100%)
--------AUTO-ADJUSTING
::,/APPROX.
--SENSOR
---SENSOR
'SENSOR
30%
OPEN
CLOSED
CLOSED
AREA
85%
/1
1
1
SENSOR
OPEN
(100%)
:~
1
I
I
THROTTLE
IDLE POSITION
----...______AUTO-ADJUSTING
A newly developed throttle-idle-position auto-adjusting system
This system
idle, the narrow range throttle sensor
At
position auto adjusting system, the engine control unit
If
the output
25%
respectively for fail-safe operation.
Operation for the
engine
and
25%
automatically compensates for certain variations
is
set to output a signal of
will
is
less than
full range sensor
15%
or more than
25%
at
idle, the engine control unit fixes the value
is
the same. The sensor
control unit compensates within the range from
respectively for fail-safe operation.
compensate for actual output values
5%-25%.
F2-18
AREA
0
FULL
THROTTLE
is
incorporated within the engine control unit.
in
the output signal
20%
is
set to register a
If
over or under the signal
of
full-open.
of
the throttle sensors.
W1th
the throttle idle
of
15%
signal at idle, and the
is
15%-25%.
at
15%
fixed at
CJ7UOF2514
and
5%
Page 69
-EAN BEST-IDLE CONTROL SYSTEM
WATER THERM
OSENSOR
ENGINE CONTROL UNIT
OF
DETECTION
WARM CONDITION
ENGINE
~
'
NEUTRAL SWITC
CLUTCH SWITC
P/S PRESSURE SWITC
A/C SWITC
BLOWER SWITC
HEADLIGHT SWITC
:::::AR DEFROSTER SWITC
FOG
LIGHT SWITC
CANAD
(ONLY
~
THROTTLE
(N~
::RANK ANGLE SENS
SE
H
H--
H
H
H
H
H
H
A)
NSOR
GE)
~
OR
(NE
J
SIGNAL
DETECTION
ENGINE
NO-LOAD
CONDITION
FOG
(ONLY
DETECTION
CONDITION)
DETECTION
ENGINE IDLE CONDITION
LIGHT SWITCH:
OF
ENGINE LOAD
OF
DETERMINATION
LEAN BEST-IDLE AMOUNT
OF
•
OF
DETERMINATION
LEAN BEST-
~
CONDITION
-
OF
IDLE
FUEL
INJEC-
TOR
I
~
-
BATT
ER'
I
i
i
)
514
mit.
rs.
idle
)%.
3.nd
the
5%
_
-=-~
fuel consumption and reduced exhaust emissions
::
'h
this system, the engine control unit sets fuel injection
-
.;J
lean misfire and rough idle.
F2-19
at
idle, the lean best-idle control s.
at
idle to the leanest amount
::::::··
::J:::::::
Page 70
SPARK ADVANCE FEEDBACK SYSTEM (ENGINE AT IDLE)
SPARK
ADVANCE
FEEDBACK
AMOUNT
THROTTLE SENSOR
(NARROW
RANGE)
DETECTION
OF
ENGINE IDLE
CONDITION
-5or----
oo
- - - - - - - -
______
I
I
I
__._
_______
I
I
-.--_...__-'
_
CRANK ANGLE
SENSOR (NE SIGNAL)
DETERMINATION
OF
ADVANCE
SPARK
FEEDBACK
AMOUNT
I
IGNITION
COIL
'
RS
rpm
DECREASED
TS:
TARGET ENGINE SPEED
REAL ENGINE SPEED
RS:
TS
RSrpm
INCREASED
To
orevent rough idle caused by incorrect idle speeds, the spark advance feedback system controls the
spark advance. The engine
tlor
t~:<~
ng
to
obtain the preprogrammed target speed
control unit judges the engine speed (real speed:
(TS)
RS)
and then adjusts the igni-
F2-20
97UOF2516
Page 71
SERVICE POINT
THROTTLE SENSOR ADJUSTMENT
)m
EASED
•
IDLE MIXTURE ADJUSTMENT
516
•
...
··
e sensor adjustment: Not usually necessary unless throttle sensor unit
auto-adjusting system automatically compensates.
· xture adjustment Not necessary because
eliminated.)
of
F2-21
lean best-idle control system. (Vanable res::· • ·
is
replaced.
Throttle-idle-pas'~··
Page 72
SELF-DIAGNOSIS FUNCTION
DESCRIPTION
Whefl troubles are suspected
Fa1'1ures
tion
of
1nd1V1dual
code
numbers.
Note
The
control unit constantly checks for malfunction of the input devices. It checks for malfunction of output devices only during a 3-second period after the ignition switch has been turned
ON
while the test connector
input and output devices are indicated and retneved from the control
in
the main input devices or output devices.
is
grounded.
check
for the cause with the SST
un1t
as malfunc-
IGNITION
WITH IGNITER r
(TRAILING SIDE)
M~~~C:'EJ~-.
CRANK ANGLE
SENSOR (G-SIGNAL)
KNOCK
COIL---~~---.'~'
SENSOR-0
\,,{J~
---,
'
----,
FAIL-SAFE
FUNCTION
WATER----f7·~
THERMOSENSOR
AIRFLOW~
METER
INTAKEAIR
THERMOSENSOR
(AFM)
INTAKE AIR
THERMOSENSOR (ENGINE)
~;~
'0
~
~
--
7
DETECTION
OF
MALFUNCTION
WARNING
FUNCTION
&
MALFUNCTION
CODE
FUNCTION
_j_
-
-
-=-
~l~~~~:~;L
~
THROTTLE~-
(~~~~~~-RANGE)
PRESSURE--SENSOR
OXYGEN
METERING
PUMP POSITION
SENSOR
SENSOR-\
OIL--~
Q._"__
-~-
-~
-----'
ATMOSPHERIC
PRESSURE
SENSOR
TEST CONNECTOR
(GREEN: 1-PIN)
F2-22
97UQF2 024
Page 73
MALFUNCTION CODE NUMBER
SST
49 H018
Self-D1agnos1s
Checker
9A1
• ..,
,-,
1-1
~----~-
~~~~.:~_
Sflf
OIAGJIOSIS
CHECKER
97UOF2 520
Inspection Procedure
1.
Warm up the engine to normal operating temperature and
stop
it.
2.
Connect the SST
the negative battery
the select switch to position
Set
3.
Connect a jumper wire between the test connector (Green:
to
the check connector (Green: 6-pin) and
terminal.
A.
1-pin) and a body ground
~\1\T/
•
"""11-11
O'd/
--/-H-'-1-'-
SElf
DIAGNOSIS
M()..,rTQR
LA
... P
0
49
HOle
!Mt
--
•G
1::111-:1/
•
ICil
SELF·DIAGNDSIS
MO~rTOft
LAMP
Q
000
0
0
I
•tlo4018MI
--.
-
1
1
1-1
-
-I
1_111_._,.11
CHECKER
SELECT
0
voo
[J'•
0
~.
flll&0f_O
..
v
--
CHHKER
SELECT SW
[g]:
lll.loO(
..
~
SW
J...,.
...
97UOF2 522
MALFUNCTION
CODE
NUMBER
97UOF2 518
4.
Turn the ignition switch ON.
5.
Check that
sounds for
6.
If
88
7.
If
88
than
control unit
And check the engine
voltage. Replace
perform
8.
Check for any malfunction
9.
Start the engine and check for further malfunction
88
flashes on the digital display and the buzzer
3 sec. after turning the ignition switch ON.
does not flash, check the check connector wiring.
flashes and the buzzer sounds continuously for more
20 sec., check for a short circuit between the engine
(1
F)
terminal and check connector (Green: 6-pin).
control unit (3X) and (3Z) terminal
the engine control unit
if
necessary and
Step 4 again.
code
numbers.
numbers.
10.
If
a malfunction
cause of the
code
problem .
number
is
indicated, check for the
Note
Cancel the malfunction code numbers by performing
the after-repair procedure
following repairs.
F2-23
code
Page 74
Principle of code cycle
Malfunction codes are determined
1.
Malfunction code cycle break
as
below by use of the MIL and Self-Diagnosis Checker.
The time between malfunction code cycles
is
4.0 sec. (the time the MIL and checker buzzer are
97UOF2-523
off).
1 CYCLE
ON
OFF
MALFUNCTION CODE
CYCLE
4.0 SEC.
2. Second digit of malfunction code (ones position)
The digit
are
in
the ones position
on
0.4 sec. during one cycle.
__llJl]
ON
OFF
of
the malfunction code represents the number
1 CYCLE CODE
-+---+-
_j____\_
0.4 0.4
SEC. SEC.
MALFUNCTION
CYClE
'-----------'
4.0 SEC.
BREAK
BREAK
~~
'---------
9MUOF1 543
of
times the MIL and buzzer
CODE No.:
89U04X 565
03
3.
~\t'S.\
d\9.\\ ot
\"\\~
~\~'\\\\\"\\\<c'\<c\\'2>
are on 1.2 sec. during one
ma\tu.n~\\on
))\:J'2>\\\\:Jn
~od~
~~\'\%
d\
me
cycle.
~o%\\\on\
rnai'\unc1.\Dn
cooe represents \ne number
The MIL and buzzer are off tor 1.6 sec. between the long and short pulses.
1 CYCLE
f----.+
12
1.2 SEC. SEC. 1.6
1------l
FIRST DIGIT SECOND
.4
SEC.
MALFUNCTION
CODE
DIGIT
F2-24
o1
times tne
M\l
and buzzer
CODE No.:
22
89U04X-566
Page 75
Code number
Caution
a)
If there
first, the subsequent malfunction codes appear
b)
After repairing all failures, turn the ignition switch OFF, disconnect the negative battery ca-
ble, and depress the brake pedal for at least 5 seconds
is
more than one failure present, the lowest number malfunction code
in
order.
to
erase the malfunction code memory.
is
Input devices
displayed
,..
\
I
Code 1
No.
01
02
03 Crank angle sensor Broken
05 Knock sensor Broken
08
09
10
13
'4
'']
Input
devices Malfunction
lgn1t1on
w1th
(Tra1l1ng
Crank angle sensor Broken
(Ne
(G
A1rflow
Water thermosensor Broken
Intake
1
thermosensor (AFM)
coil Malfunct1on of spark plug. ,
1gn1ter
s1de)
s1gnal)
s1gnal)
meter (AFM) Broken
a1r
:c'
thermo-Broken
·
'Cng1ne)
..
·c
._;:uli
SG\\SCl\
range) angle 1npu\
Pressure sensor
(Intake manifold
pressure)
Atmosphenc pres-
sure sensor (ATP)
(Built
1n
ECU) 760
Oxygen sensor
Feedback system
Throttle sensor
(Narrow range)
oil
-
oil
oil
pump
pump
------
pump
Meter1ng
pos1tlon sensor
Metering
(MOP)
Metenng
(MOP)
broken
Broken
Bro\<..e11
Broken
Malfunct1on1ng ECU Atmosphenc pressure
Oxygen
below
system
Oxygen
i
0.55V
operat1on
I
t
Broken
Broken
Malfunctioning
tors
or
-
--
---1-
I
Malfunct10n1ng
broken
1
t1on1ng
w1re.
short
w1re.
short
w1re,
short
w1re.
short
w1re.
short
w1re.
short
w1re.
short
w1re.
short
\NI\e,
sllor\
w1re,
short
sensor
output
0
55V
80
sec.
operat1on
sensor
output
10
sec
after
beg1n1ng
w1re.
short
w1re.
short
w1re.
ECU
MOP.
w1re.
MOP.
short
alternator
broken
malfunct1on1ng
c1rcu1t
C1rcu1t
C1rcu1t
c1rcu1t
c1rcu1t
c1rcu1t
c1rcu1t
c1rcu1t
CI\C\.11\
C1rcu1t
rema1ns
after
beg1n1ng
rema1ns
F/8
system
C1rcu1t
C1rcu1t
step
short
C1rcu1t
ECU
step
motors
c1rcu't
malfunc-
or
battery
Fail-safe function
Trail1ng-s1de
pulse cut
Fuel
inJeCtion
t1on
cut
Fuel
lnJ8Cllon
t1on
cut
lgn1t1on
Bas1c
amount and ign1tlon
t1ming
Coolant
1
f1xed
at
Intake
f1xed
at
Intake
f1xed
at
111\Cl\\\e
at
20%
Intake
1nput
mmHg (29.9
1nput
Feedback system can
F/8
mo·
celed (For EGI)
Feedback system canceled (For
Throttle valve open1ng
angle
at full open
MOP
Bas1c
and
ign1t1on
MOP
Bas1c
and
1Qn1t1on
.
------
Bas1c
amount and
t1m1ng
1gn1t1on
and
and
t1m1ng
f1xed
fuel
1nj8ct1on
f1xed
temp.
1nput
80°C
(176°F)
a1r
temp '.nput
20°C
(68°F)
a1r
temp.
20°C
(68°F)
'Jai\Je
ope111119
s1gnal
open
man1told
s1gnal
f1xed
1nHg)
s1gnal
f1xed
mmHg
(29 9
EGI)
1nput
signal
f1xed
smallest
fuel
InjeCtion
tmng
f1xed
smallest
fuel
InjeCtion
tmng
-
fuel injeCtion
1Qn1t1on
f1xed
1gn1-
1gn1-
1nput
f1xed
pressure
at
760
at
1nHg)
f1xed
open
amount
f1xed
open
amount
f1xed
---
Output
'
(Self-Diagnosis Checker or MIL)
signal
pattern
Jl
I
I
}~~L
I.
..
Jl
m
f\_~R
Ill
IUI
rJ~~l
JUII
Jlll[
Ilfl
---.
ITUI~~;~
nlln
J u u
~~c~---
~u~----
F2-25
Page 76
Output devices
Code
No.
25
Soleno1d valve (Pressure regulator control (PRC))
26
Step motor (Metenng
30 Split
31
32 Solenoid valve (Switch)
33
34
a1r
soleno1d valve
Solenoid valve (Relief)
Port
a1r
solenoid valve
Solenoid valve (Bypass
Output devices
011
pump)
a1r
control)
Output
(Self-Diagnosis Checker or MIL)
signal pattern
----
---
Irul
Jru~~n~
m~
rm~L
Jrull
Jf{ll1
Jl'lfilll
-
38
Soleno1d valve (Accelerated warm-up system (AWS) and
a1r