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airplane
...498is engine
498is engine
Engine
498ia
Type
opposed two cylinder two stroke boxer
Output
39Hp at 6700 rev/min
Total displacement
498 cm3
Cooling system
air > 25 m/sec
Max rpm
7000 rev/min
Min rpm
1800 to 2200 rev/min
Bore
75 mm
Stroke
56mm
Bore/stroke ratio
1,339
Compression ratio
11:1
Cylinders
light alloy metal ceramic plated castings
Cylinder heads
light alloy castings
Crankcase
machined from solid
Connecting rods
forged steel with caged needle bearings at both ends
Crankshaft
forget steel supported by special double-row ball bearings
Fuel metering
fuel injection on throttle body
Ignition system
programmed inductive discharging system managed by ECU
Spark plug
NGK CR8HIX
Exhaust system
stub
TBO
250 hours
ECU type

Self diagnostich - 28V

Communication from ECU to client system by
RS232
Operating temperature
-20 +55°C
Alternator / Starter
Brushless 28V-100A
Operating temperatures
Temperature under spark plug (CHT)
max 260° C
Exhaust gas temperature (EGT)
max 580° C
Acceleration
Operating (engine working)
launch 15g along propeller axis
Operating (engine working)
operation 7g along vertical and 1g along side axis
Non operating (engine non-working)
+- 15g along all axes
Rotation
counter clockwise(when looking on propeller side
Fuel
>=95 Oct. petrol/oil mixture 2% synthetic oil for 2 stroke engines
Weight with alternator
18,6Kg
Weight/power ratio
0.476
Specific consumption
Better than 330gr./Hp/h
Redundancy

                                                                   Double ignition, double pick up

PDF
PDF
PDF
498is
Self diagnostic ECU will communicate via RS232 any sensor failure.

Capability in case of pick up failure to switch to the second one without kill the engine.

Double ignition with 4 drivers and 4 coils.

New throttle body made in peek with servo integrated with stay in place in case of servo failure and alarm via RS232.

CHT and EGT integrated readable  with RS232 .

Fuel pump managed by ECU without fuel return.

Starter integrated by alternator