| Name |
index |
Remark |
| Architecture |
Hybrid multi-rotor |
Six-axis twelve-rotor, turboshaft generator |
| Payload |
200KGLimit 250KG |
200KG load capacity, maximum load capacity 250KG |
| Range |
350KM |
Flight radius 175KM, total range not less than 300KM |
| Duration |
3.5H |
Cruising time 3.5 to 6 hours |
| Flight speed |
100KM/H |
Economic cruising speed 100KM/H |
| Engine model |
—— |
|
| Communication link |
80KM |
Private network communication |
| Deployment and retraction time |
45Min |
The time for unfolding and retracting is 45 minutes |
| 200KG load-carrying hybrid multi-rotor technology evaluation |
| Name |
Weight(kg) |
Remark |
| Engine assembly |
35 |
Combined weight of turboshaft generator, propeller, installation accessories, etc. |
| Fuel tank 650L |
80 |
Total weight of fuel tank and 100L fuel |
| Multi-rotor power |
50 |
12 sets of motors, six-axis twelve-rotor, each set weighs about 4kg |
| Multi-rotor battery |
40 |
Battery weight 40KG, capacity 30Ah, 400V, high rate lithium battery, spare emergency battery |
| chassis |
15 |
Casing and related accessories assembly |
| Load |
200 |
Load 200kg |
| gross weight |
420 |
Estimated weight, actual weight may vary |
| Engine fuel consumption |
|
|
| Total hovering power |
85KW |
|
| Fuel consumption-L |
1L/H |
The fuel consumption in cruising mode is about 430L per hour |
| Flight time |
1.5H |
Theoretically calculated full load endurance time is 6 hours |
| Current |
200A |
When the whole machine is 3500kg, it is calculated based on the motor parameters, each motor is 390A, and there are 12 motors |
| Pure electric flight time |
5Min |
According to the battery capacity of 100Ah and the current, the theoretical flight time is about 10 minutes. |
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