|
|
 |
 |
For deltawing and ulm airplane |
| SCHEDULE
OF STATIC THRUST |
Engine VICTOR 1 matriculation
V102
Poly-V belt reduction
ratio 1:270
Double blade pushing propeller
wood made
162x112 GT |
| TESTING
CONDITIONS |
T 12°C
- P 1048 Mb - UR 45%
Locality Torre Maina 04/02/2000
Altitude (S.L.M.) 300 m |
| RPM |
Consumption
l/hr |
Kg
of thrust |
| 6150 |
8,8 |
126 |
| 6000 |
7,8 |
114 |
| 5500 |
6 |
94 |
| 5000 |
5 |
76 |
| 4500 |
3 |
45 |
|
|
|
TECHNICAL DATA
|
|
Displacement
|
cc
|
362
|
|
Bore
|
mm
|
80
|
|
Stroke
|
mm
|
72
|
| Compression Ratio |
9,5/1
|
|
Power
|
Hp
|
44
|
|
kW
|
32,75
|
|
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 |
11,04 |
3,58 |
| 3200 |
16 |
11,78 |
3,58 |
| 3500 |
20 |
14,72 |
4,08 |
| 4000 |
24 |
17,66 |
4,3 |
| 4500 |
31 |
22,81 |
4,87 |
| 5000 |
35 |
25,76 |
5,01 |
| 5500 |
38,8 |
28,56 |
5,01 |
| 6000 |
42 |
30,91 |
5,01 |
| 6200 |
43,5 |
32,02 |
5,01 |
| 6500 |
44,5 |
32,75 |
4,87 |
| 6700 |
40,6 |
29,88 |
4,3 |
|
|
