Simonini engines Italy, Simonini Victor 1 distributed
by Speedwing Aircraft.
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Schedule
thrusting curve, engine "Victor 1" matriculation number S002
Poly V belt reduction, ratio 1/2.4
Double blades pushing propeller (made on wood), 162x112 GT
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RPM.. |
Consumption L/HR.. |
Kg. de Thrusting.. |
Exhaust T°C.. |
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6150 |
10,4 |
134 |
584° |
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6000 |
10 |
126 |
564° |
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5500 |
8 |
104 |
546° |
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5000 |
6 |
86 |
555° |
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4500 |
3 |
56 |
550° |
Testing
conditions : T 12° C - P 1048 Mb UR 45%
Locality Torre Maina 04/02/2000
Altitude (S.L.M.) 300 mt.
Engine: Victor 1axc 80x76 382 cc rdc 9,5/1
Lamellar induction, double carburettor (Bing 36 mm.), aluminium
cylinders Nicasil ceramic filling.
Exhaust systems with indipendent resonance, maximum power 48 HP at
6000 rpm, couple at power speed 4,9 Kgm.
Poly V belt reduction with elastic joint/vibration damper, ratio
available 1/2,4, 1/2,76, 1/3,47, 1/4.
Flying consumption at 5200 rpm, 6 liters/hour.
Lubrication: premix 2,5 with leaded fuel, 3% with unleaded fuel
(SP).
Total weight with accessories, radiator, cooling liquid and
propeller 30 Kg.
Ducati's double electric start. |
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TECHNICAL DATA
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Displacement
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cm³
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362
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Bore
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mm
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80
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Stroke
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mm
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72
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Compression Ratio |
9,5/1
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Power
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Hp
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44
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kW
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32,75
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RPM
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6.200
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Weight of the engine with:
exhaust, air filter, radiator, propeller and liquid |
Kg 32
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Lamellar intake with Bing 36
carburettor |
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Alluminium cilinder with
Nikasil ceramic coating |
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Exhaust resonance system.
Poly-V belt reduction |
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Double Ducati electronic
ignition with alternator for recharge battery fly |
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Electric starter |
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Flying consumption at 5400
RPM, 5 liters/hour |
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Premix two stroke oil
gasoline, 2,5% oil by volume to leaded fuel, 3% oil by
volume to unleaded fuel. |
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REDUCTION RATIONS AVAIABLE
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1:270 Crown gear 183 mm / Pinion 68 mm
1:280 Crown gear 183 mm / Pinion 65 mm
1:300 Crown gear 183 mm / Pinion 61 mm
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| For more information contact: Speedwing
Aircraft Inc
2500 CH. De La Presqu'ile
L'Assomption Quebec
Canada J5W 3P3
450-589-1950 |
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