|
|
 |
 |
For deltawing and ulm airplane
|
| SCHEDULE
OF STATIC THRUST |
Engine VICTOR 1 PLUS
matriculation V103
Poly-V belt reduction
ratio 1:270
Double blade pushing propeller
wood made
162x114 GT |
| TESTING
CONDITIONS |
T 10°C
- P 1048 Mb - UR 45%
Locality Torre Maina 12/11/2001
Altitude (S.L.M.) 300 m |
| RPM |
Consumption
l/hr |
Kg
of thrust |
| 6150 |
9,2 |
134 |
| 6000 |
8 |
126 |
| 5500 |
6 |
104 |
| 5000 |
4,5 |
86 |
| 4500 |
3 |
56 |
|
|
|
TECHNICAL DATA
|
|
Displacement
|
cc
|
382
|
|
Bore
|
mm
|
80
|
|
Stroke
|
mm
|
76
|
| Compression Ratio |
9,5/1
|
|
Power
|
Hp
|
48
|
|
kW
|
35
|
|
RPM
|
6.200
|
| Weight of the engine ready to fly |
Kg 32
|
| Lamellar intake with Bing 36
carburetor |
| Alluminium cylinder with Nikasil
ceramic coating |
| Exhaust resonance system. Poly-V
belt reduction |
| Double Ducati Electronic ignition
with alternator to recharge battery in fly |
| Electric starter |
| Flying consumption at 5400
RPM 6 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
|
|
1:270 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
|
|
|
| POWER
AND TORQUE |
 |
| RPM |
Hp |
kW |
Kgm |
| 3000 |
15,6 |
11,48 |
3,72 |
| 3200 |
17,28 |
12,72 |
3,87 |
| 3500 |
20,3 |
14,94 |
4,15 |
| 4000 |
25,6 |
18,84 |
4,58 |
| 4500 |
31,5 |
23,18 |
5,01 |
| 5000 |
36,65 |
26,97 |
5,23 |
| 5500 |
41,8 |
30,76 |
5,44 |
| 6000 |
45,6 |
33,56 |
5,44 |
| 6200 |
47,12 |
34,68 |
5,44 |
| 6500 |
47,45 |
34,92 |
5,23 |
| 6700 |
45,6 |
33,56 |
4,87 |
| |
|
|
