Robin EH17-2, EH25-2 Service Manual

CONTENTS
Section Title
1
.
2
3
.
4
.
5
.
6
.
7
.
8
.
Page
4-1 4-2 4-3
4-4
4-5 4-6 4-7 4-8 4-9 4-1
0
4-1
1
4-1
2
4-1 3 4-1 4 4-1
5
4-1 6 4-1 7
I.
SPECIFICATIONS
~~ ~ ~~~ ~ ~ ~~ ~~ ~~~ ~~~~ ~~ ~~~ ~ ~
Model
EH12-2B
EH
12-2
EHl2-2D EH12-2BS
EH12-2DS
TY
Pe
X
Bore Piston Displacement
Max.
Nem (kaf*m)/rDm
I
Direction Cooling system Valve Arrangement
Lubrication Lubricant Capacity of Lubricant
I
Carburetor
Stroke
Torque
of
Rotation
~~ ~ ~~~~~ ~~ ~
Air-Cooled, 4-Cycle, Single-Cylinder, Horizontal
x
43 rnm (2.36 x 1.57 in.)
60
cm3
(7.38 cu.in.)
As
Viewd From
Splash Type
L
(0.16
U.S.
I
52)
15 (1
Counterclockwise
~~ ~
Automobile
/1300
Oil
SAE
121
Forced Air Cooling
Overhead Valve
#20, #30 or 1 OW-30 ; Class SE, SF
0.6
Horizontal Draft, Float Type
P.T.O.
P.T.O.
gal.)
Shaft, Gasoline Engine
7.5 (0.76) /2600 Shaft Side
or
higher
I
Fuel
I
Fuel Feed System Fuel Tank Capacity
I
Spark Plug Charging Capacity
I
Speed Reduction Governor System
Dry
Weight
Length
I
310 g/KW*h (230 gr/HP*h) At Continuous Rated Output
~~~~~~~ ~~
I
-
Recoil Starter Starting System
2:l Cam Shaft Drive
15.5 kg (34.2Ib.)
299 mm (1 1.77 in.)
Recoil and Electric
Starter
I
18.0 kg (39.7 Ib.)
I
299 mm (1 1.77 in.) I 297 mm (1 1.69 in.) I 297 mm(ll.69 in.)
Automobile Gasoline
~ ~~~
Gravity Type
U.S.
3.6 L (0.95
Flywheel Magneto (Solid State) Ignition System
NGK BGES
12V - 1.3A
Centrifugal Flyweight System
gal.)
-
Recoil
I
15.0 kg (33.1 Ib.)
330mrn (12.99in.) 366 mm (14.41 in.)
Starter
12V
Starter
Recoil and Electric
I
17.5 kg (38.6Ib.)
341 mm (13.43in.) 366 mm (14.41 in.)
-
1.3A
-1-
Model
EH17-2B
EH17-2BS
EH17-2
EH17-2D
EH17-2DS
TY
Pe
X
Bore
Compression Ratio 8.5
Output
Kw
Max.
Nom
Direction of Rotation
I
Cooling system
I
Valve Arrangement
I
Lubrication Lubricant
Capacity of Lubricant
Stroke
(HP)/rpm
Torque
(kgf*m)/rpm
Continuous Max.
~ ~~ ~~ ~
Air-Cooled, 4-Cycle, Single-Cylinder, Horizontal
~~ ~~
(3.5)
2.6
I I
I
I
I
Automobile Oil
~~ ~~~~ ~ ~
67
/
1500 2.9 (4.0) / 1800
4.4 (6.0) /2000
21.4 (2.1 8) Counterclockwise
/
1300
~~~~~~~ ~
SAE
#20, #30
Horizontal Draft, Float Type Carburetor
x
49
mrn
172 cm3 (10.50 cu.in.)
As
Viewd From P.T.O. Shaft Side
Forced
~~
Overhead Valve
Splash Type
L
0.65
(0.17
P.T.O.
(2.64
X
1.93 in.)
2.6
Air
Cooling
~_____
or
1OW-30 ; Class
U.S.
gal.)
Shaft, Gasoline Engine
.
(3.5)
/3000 2.9 (4.0) /3600
4.4 (6.0) /4000
1
0.7
(1
-09) / 2600
_____
~ ~
SE,
SF
or higher
Fuel Fuel Consumption Rate Fuel Feed System Fuel Tank Capacity
Spark
Charging Capacity
I
Starting System Speed Reduction
Plug
Dry
Weight
Dimensions
Length
Width
Height 380mm (14.96in.)
310g/KW-h (230 gr/HP*h) At Continuous Rated Output
-
2:l
Cam Shaft Drive
16.5 kg (36.4 Ib.)
mm
mm
(1 1.85 in.) (12.99in.)
301
Automobile Gasoline
Gravity Type
3.6 L (0.95
Flywheel Magneto (Solid State)
12V - 1.3A
NGK
US.
B6HS
gal.)
-
-
Centrifugal Flyweight System Governor System
19.0
kg (41.9
mrn
341
rnrn
380rnm (14.96in.) 380mm (14.96in.)
Ib.)
(1
1.85 in.)
(13.43in.) 330
16.0 kg (35.3
299
mm
rnm
330
Ib.)
(1 1.77 in.) 301 (12.99in.)
18.5 kg
299 mm(ll.77in.)
341 380rnm (14.96in.:
12V
rnm
-
1.3A
(40.8
Ib.)
(13.43in.:
-2-
Model
EH25-2
6
EH25-26s
EH25-2
~~~~~~ ~~ ~
EH25-2D
EH25-2DS
TY
Pe
x
Bore Piston Displacement Compression Ratio
output
Kw
Max.
Nom (kgf*m)/rpm Direction
Cooling system
Valve Arrangement
Lubrication
Capacity of Lubricant Carburetor
Fuel
Stroke
(HP)hm
Torque
of
Rotation
Continuous Max.
Air-Cooled, 4-Cycle, Single-Cylinder, Horizontal P.T.O. Shaft, Gasoline Engine
75 X 57
mm
(2.95
251
cm3 (15.31 cu.in;)
X
2.24 in.)
8.5
(5.5)
/3000 4.7 (6.4) /3600
(8.5)
SE,
SF
/4000
/
2600
or
higher Lubricant
6.3
16.6 (1.69)
I
4.0
(5.5)
I1
500
4.7 (6.4) / 1800
(8.5)
6.3
33.1 (3.38)
Automobile Oil SAE #20, #30 or
/2000
/
1300
Counterclockwise As Viewd From P.T.O. Shaft Side
Horizontal Draft, Float Type
4.0
Forced Air Cooling
Overhead Valve
Splash Type
1
OW-30 ; Class
1
.O
L
(0.26
U.S.
gal.)
~ ~~~ ~ ~ ~ ~~~~~
Automobile Gasoline Fuel Consumption Fuel Feed System Fuel Tank Capacity Ignition System Spark Plug Charging Capacity
Starting System Recoil Starter Speed Reduction
Governor System Dry Weight
Dimensions
Rate
I
Length
Width
Height
31
-
I
2:l Cam Shaft Drive
I
24.0 kg (52.9
333mm (13.11 in.) 380mm (14.96in.)
440mm
Ib.)
(17.32in.)
0
g/KW*h (230 gr
6.0
Flywheel Magneto (Solid State)
12V - 1.3A
Recoil and Electric
Starter
Centrifugal Flyweight System
28.0 kg (61.7 Ib.) 333mm (13.11 in.) 380mm
440mm
(14.96in.) (17.32in.)
/
HP-h)
At Continuous Rated Output
Gravity Type
L
(1
59
U.S.
NGK
B6HS
I
Recoil
23.0
gal.)
kg
-
Starter
(50.7
Ib.)
~~~ ~~
-
12V
1
Starter
Recoil and Electric
1.3A
-
27.0 kg (59.5
332mm(l3.07in.) 332mm (13.07in.)
380mrn (14.96in.) 380mm (14.96in.)
440mm
(17.32in.) 440mm (17.32in.)
Ib.)
-3-
2-1
MAXIMUM OUTPUT
The maximum output is the output of an engine with its throttle valve fully opened under the condition that all the moving parts are properly
A
new engine may not produce full maximum output while its moving parts are still not broken-in.
2-2
CONTINUOUS
RATED
OUTPUT
worn
in after the initial break-in period.
The continuous rated output is the output
favorable from the view point
is
When the engine
installed
of
engine’s life and fuel consumption.
on
a certain equipment,
of
an engine at optimum governed speed which is most
it
is
recommended that the continuous output
required from the engine be kept below this continuous rated output.
2-3
MAXIMUM
The maximum torque
TORQUE
is
the torque at the output shaft when the engine is producing maximum output at
certain revolution.
-4-
2-4
PERFORMANCE CURVES
8
0
EHlPD,
B
HP
4
3
kW
2
for
B
type
+
3
l2
n
+
3
0
1
0
1
2000
(1
000)
REVOLUTION
3000
(1
500)
-
r.p.m.
4000
(2000)
-5-
0
EH17D,
6
for
B
tvDe
N.m
kgfam
(1
000)
REVOLUTION
3000
(1
500)
-
-6-
4000
(2000)
r.p.m.
EH25D,
B
kW
HP
-6
8
7
I
t:
$4
I-
&
5
4
r
"
I
I I
"
I
I
I
MAXIMUM
I
I
MAXIMUM
I
I
I
I
I
"-
I
TORQUE
I
HORSEPOWER
RECOMMENDED
1
AL\
I I
I I
'(NET)
I
16.5
15.5
14.5
N.m
(33)
(31)
(29)
c
kgf-m
1.7
(3.4)
1.6
(3.2)
1.5
(3.0)
1.4 (2.8)
2
1
0
2000
(1
000)
I
i
REVOLUTION
3000
(1
500)
-
-7-
'
r.p.m.
4000
(2000)
3.
FEATURES
1.
The overhead valve design offers
a
compactness, light weight and ideal combustion characteristics
resulting in more power from Iess fuel and prolonged engine life.
2.
An
optimum lubrication and better tilted operation thanks to upright cylinder design.
3.
A crossflow arrangement
of
intake and exhaust ports ensures stable performance under high ambient
temperature.
4.
The automatic decompressiom system lightens conventional
5.
An easy operation thanks to integrated engine control system. Improved throttle mechanism
6.
Combustion and mechanical noises have been analyzed acoustically and improved for better tonal
SV
engines.
is
adopted for easy starting.
the
recoil pull force by
40%
quality and lower engine noise.
7.
Optimally designed reciprocating parts reduce the vibration level of the engine. equips single through-balancer shaft as an option.
4.
GENERAL DESCRIPTION
4-1
CYLINDER
AND
CRANKCASE
OF
ENGINE COMPONENTS
comparing to the
EH25-2
engine
,
,
The cylinder and crankcase
is
single piece aluminum diecasting. The cylinder liner, made of special cast iron,
is
molded into the aluminum casting.
The crankcase has a mounting surface. on the output
shaft side, where the main bearing cover is attached.
4-2
MAIN
The main bearing cover which
BEARING
is
mounted on the output shaft side of the
COVER
is
an aluminum diecasting,
crankcase. Remove the main bearing cover to inspect the inside
of
the engine. The pilots and bosses are machined on the cover for direct mounting of the engine onto such machines
as
generators and pumps.
Oil gauge (fillers) are on both sides of the cover for easy maintenance.
Fig.
/"-
\
4-1
/"
-8-
OIL GAUGE
Fig.
4-2
OIL
GAUGE
4-3
CRANKSHAFT
The crankshaft is forged carbon steel, and
W
pin is induction-hardened.
the
crank
B
TYPE
The output end of the shaft has a crankshaft gear, and balancer gear for
EH25-2
which are pressed into
position.
D
TYPE
Fig.
4-3
44
CONNECTING
ROD
AND
PISTON
The connecting rod is an aluminum alloy diecasting,
and
its
large and smalI ends function as bearings. The piston two compression rings and one
is
an aluminum alloy casting, and carries
oil
ring.
4-5
PISTON RINGS
The piston rings are made The profile of the top ring second ring has a tapered The
oil
ring consists
of
special cast iron.
is
barrel face and the
face.
of
a cutter ring and a
coil
expander for better sealing and less oil consumption.
-9-
I
fig.
4-4
TOP
RING
fig.
SECOND
OIL
4-5
RING
RING
4-6
CAMSHAFT
The camshaft
for
the D-type engine is made
of
special cast iron and camshaft gears are casted to-
gether
in
one piece. Both sides of the shaft fit into the plane bearings on the crankcase and main bearing cover. The camshaft for the B-type engine is made of forged carbon steel and also functions as PTO shaft. The cam gear bearings are employed
is
press fitted on the shaft and the ball
on
both sides for supporting
the shaft.
4-7
VALVE ARRANGEMENT
The intake valve is located
on
flywheel side
of
the
cylinder head. The hard alloy valve seats axe molded in the cylinder head and stellite is fused to the exhaust valve face. The cylinder baffle leads cooling air to the exhaust valve area for the optimum cooling.
B
Fig.
TYPE
4-6
n
D
lYPE
INTAKE
/
4-8
CYLINDER HEAD
The cylinder head is an aluminum die casting which
utilizes wedge
type
combustion chamber
for
the
highest combustion efficiency.
-
10
Fig.
4-7
Fig.
4-8
-
4-9
GOVERNOR SYSTEM
The governor
is
a centrifugal flyweight type which ensures constant operation at the selected speed against load variations. The governor gear with governor weights is installed
on the main bearing cover.
4-10
COOLING SYSTEM
The large fins on the flywheel provide sufficient cooling air capacity
for
the inlet and exhaust area and cylinder. The cylinder baffle helps the cooling air flow effi­ciently.
4-1
1
LUBRICATION
All the rotating and sliding parts are splash­lubricated by the oil scraper on the connecting rod.
/
GOVERNOR
GEAR
Fig.
4-9
4-1
2
-IGNITION SYSTEM
The ignition system is a transistor controlled mag­neto ignition system which cosists of a flywheel and an ignition coil with a built in transistor. This system has an ignition timing advance for easy starting.
-
11
-
OIL
SCRAPER
Fig.
Fig.
4-10
4-1
7
4-13
The engines are equipped with a horizontal draft carburetor that has a float controlled fuel system and a The carburetors are calibrated carefully for easy starting, good acceleration, low fuel consumption and sufficient output.
CARBURETOR
fixed
main jet.
4-14
The air cleaner is a element type is available.
AIR
CLEANER
single
CLEANER CASE
Single
4-15
Unbalanced inertia force which rotates at the same speed with the crankshaft to effectively reduce vibration.
BALANCER
(Option
urethane foam element system.
element type
Fig.
4-
1
3-
I
for
EH25-2)
is
balanced by the balancer
As
an option, heavy duty type with
Double element type
Fig.
4-
13-2
BALANCER
a
CLEANER COVER
I
double
-
-
12-
Fig.
4-14
4-16
DECOMPRESSION
An
automatic decompression mechanism which
SYSTEM
opens exhaust valve before the piston reaches com­pression top
is
assembled on the camshaft for easy
starting.
AUTOMATIC
DECOMPRESSOR
Fig.
4-14
SYSTEM
-
13-
4-1
7
SECTIONAL
VIEW
OF
ENGINE
FUEL
TANK
FLYWHEEL
-
14-
MAIN
BEARING
COVER
a
ROCKER
ARM
PUSH ROD
-
15
-
5.
DISASSEMBLY
5-1
PREPARATIONS AND SUGGESTIONS
1)
When disassembling the engine, memorize the locations
reassembed correctly. If yor are uncertain
AND
REASSEMBLY
of
identifying some parts, it
of
attached to them.
2)
Have boxes ready to keep disassembed parts by group.
3)
To
prevent losing and misplacing, temporarily assemble each group
4)
Carefully handle disassembed parts, and clean them with washing oil
5)
Use
the correct tools in the correct way.
5-2
SPECIAL
Tool
TOOLS
No.
Tool
individual parts
is
of
disassembed parts.
if
necessary.
Use
so
that they can be
suggested that tags be
209
Market
-
95004-
parts
07
Flywheel
Flywheel puller
FLYWHEEL PULLER
puller with
bolt
For For
pulling
pulling
off
off
FLYWHEEL
the flywheel the flywheel
PULLER
EH25-2
EH12-2,
EH17-2
/"-
Fig.
-
16
5-1
-
5-3
DISASSEMBLY PROCEDURES
Step
1
Part
to
remove
(1)
Remove
(2)
To
gauge.
oil
drain
plug
and drain oil. Oil drain
discharge oil quickly, remove oil
Remarks Procedures
Be careful gasket.
not
to
lose the
14mm
Tool
box
I
wrench
Fig. 5-2
-
17
-
GASKET
I
DRAIN
PLUG
Step
2
Part
Fuel
to
remove
tank
Procedures
1
(1)
Close
fuel
valve.
(2) Disconnect fuel hose between fuel strainer
and carburetor.
(3)
Remove fuel M6X14mm bolt M8X20mm bolt
tank
from cylinder
*.--
0-
head.
4pcs. (EH12-2,17-2) 4pcs. (EH25-2)
~ ~ ~~ ~~
Wipe
Remarks
off
spilt
thoroughly.
fuel
1
Omm
socket
Tool
(1
2mm)
wrench
I
(EH12-2,
(EH25-2)
FUEL
HOSE
17-2)
-
-*
Fig.
18
5-3
-
Step
I
Part
to
remove
I
Procedures
I
Remarks
I
Tool
Recoil starter
housing
I
5
Oil sensor (Option)
I
(1)
Remove recoil M6
X
8mm
(1)
Remove blower housing
M6X
i2mm
(1)
Remove oil sensor probe. to damage stick and sensor since these are sensitive and
result.
from
blower housing.
flange
bolt
-
-
4pcs.
from
crankcase.
flange bolt 4pcs.
Be
an
erratic operation
careful not
may
BLOWER
1
Omm
lOmm
HOUSING
box
box
wrench
wrench
Fig.
-
19
5-4
-
)art
to remove
Procedures
Remarks
Tool
Muffler cover, Muffler and Exhaust pipe cover
(1) Remove muffler cover
cover.
M6X
lOmm flange
(2) Remove
cylinder head. M8 nut 2pcs. M6 (EHl2-2,17-2)
M8X
muffler
X
12mm
flange bolt
16mm flange
and
bolt
from crankcase and
bolt
exhaust pipe
0..
Spcs.
-
1
PC.
-
1 pc.
(EH25-2)
I
Be careful muffler gasket.
not
to
8mm, lOmm
lose
12mm socket wrench
and
M8
NUT
:
2
pcs.
MUFFLER
c
COVER
Fig.
-
20.-
5-5
Procedures
Remarks
Tool
Control
box
and Electric (Option)
(1)
Disconnect wires. blue light blue black
(2)
Remove black wires from electric starter.
(3)
Remove control
(4)
Loosen
1
(diode rectifier
***
1
two
)
1
(diode rectifier
(magnetic switch)
box.
bolts
and
remove electric
)
starter.
M8
bolt 2pcs.
Fastened together with fuel
tank.
12mm socket wrench
to
-
21
-
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