|
|
 |
 |
The most performant engine |
| SCHEDULE
OF STATIC THRUST |
Engine MINI 2 PLUS
matriculation M2210
Poly-V belt reduction, ratio 1:230
Double blade pushing propeller
wood made
126 GT |
| TESTING
CONDITIONS |
T 2°C -
P 1048 Mb - UR 46%
Locality Torre Maina 18/02/2001
Altitude (S.L.M.) 300 m |
| RPM |
Consumption
l/hr |
Kg
of thrust |
| 7200 |
5,8 |
86 |
| 7000 |
5,6 |
82 |
| 6800 |
5,4 |
78 |
| 6600 |
5,2 |
72 |
| 6400 |
4 |
66 |
| 6000 |
3,5 |
58 |
| 5500 |
2,5 |
48 |
| 5000 |
2,2 |
44 |
| 4500 |
2 |
31 |
| 4000 |
1,5 |
28 |
|
 |
 |
FLY PRODUCTS
1° PREMIO MIGLIORE
PARAMOTORE 2002-2004 |
 |
 |
|
|
TECHNICAL DATA |
|
Displacement |
cc |
202 |
|
Bore |
mm |
66,4 |
|
Stroke |
mm |
58 |
| Compression Ratio |
10,5/1 |
|
Power |
Hp |
26 |
|
kW |
19 |
|
RPM |
7.500 |
| Weight of the engine ready to fly |
Kg |
18.3 |
| Lamellar intake with Walbro
WB 37 carburetor |
| Alluminium cylinder with Nikasil
coating |
| Air-cooling |
| Exhaust resonance system. Poly-V
belt reduction |
| Electronic ignition with alternator
to recharge battery in fly |
| Electric starter |
| Flying consumption at 5000
RPM, 2,2 liters/hour |
| Premix two stroke oil gasoline,
2,5% oil by volume to leaded fuel, 3% oil by volume to
unleaded fuel |
|
REDUCTION RATIO AVAIABLE |
|
1:226 Crown gear 129 mm / Pinion 57
mm
1:230 Crown gear 129 mm / Pinion 56 mm
1:234 Crown gear 129 mm / Pinion 55 mm
1:242 Crown gear 129 mm / Pinion 53,3 mm |
|


|
| POWER
AND TORQUE |
 |
| RPM |
Hp |
kW |
Kgm |
| 3000 |
9 |
6,62 |
2,15 |
| 3500 |
11,2 |
8,24 |
2,29 |
| 4000 |
12,8 |
9,42 |
2,29 |
| 4500 |
14,4 |
10,6 |
2,29 |
| 5000 |
16,5 |
12,14 |
2,36 |
| 5500 |
18,7 |
13,76 |
2,36 |
| 6000 |
21 |
15,46 |
2,51 |
| 6500 |
22,75 |
16,74 |
2,51 |
| 7000 |
24,5 |
18,03 |
2,51 |
| 7500 |
25,5 |
18,77 |
2,43 |
| 7800 |
24,9 |
18,33 |
2,29 |
| |
|
|
|
|
|