Engineering:Toaero UAV
From HandWiki
Revision as of 11:21, 4 November 2021 by imported>Rtextdoc (correction)
| UAV | |
|---|---|
| Role | |
| National origin | China |
| Manufacturer | Toaero |
| Designer | Toaero |
| First flight | 2014 |
| Introduction | 2014 |
| Status | In service |
| Primary user | China |
Toaero UAVs are Chinese UAVs developed by Tianjin Toaero Science and Technology Co., Ltd. (Toaero, 天津中翔腾航科技有限公司) for various applications such as aerial cinematography, photography, and survey missions.
Rotorcraft
Most UAVs developed by Toaero are rotorcrafts, including unmanned helicopters and unmanned multicopters
| Model | Toaero T50[1] | Toaero T100[2] | Toaero T-300[3] | Toaero X6[4] |
|---|---|---|---|---|
| Type: | Helicopter | Helicopter | Helicopter | Multicopter |
| Layout: | Conventional helicopter | Coaxial rotors | Coaxial rotors | Hexacopter |
| Landing gear: | Skids | Skids | Skids | Skids |
| Length (m): | 2.1 | — | 2.3 | 0.88 |
| Width (m): | 0.508 | — | 0.9 | 0.88 |
| Size with rotors fully extended (m): | — | — | — | 1.18 |
| Width between skids (m): | — | 0.8 | 1 | — |
| Height (m): | — | 1.3 | 1.6 | 0.49 |
| Max wind allowed for flight (km/h): | 43.2 | 60 – 70 | — | 38.5 |
| Max wind allowed for take-off & landing (km/h): | — | 36 | — | — |
| Temperature range for operation (°C): | - 20 to 50 | — | — | - 20 to 55 |
| Temperature range for storage (°C): | - 30 to 60 | — | — | - 20 to 65 |
| Relative humidity for operation (%) | 95 | — | — | — |
| Empty weight (kg): | 18 | 60 | < 120 | 4.2 (with battery) |
| Payload (kg): | 10 | 20 | 120 (payload + fuel) | 1.8 |
| Max payload (kg): | 13 | 25 | — | 2.3 |
| Take-off weight (kg): | — | 90 | 250 | 5 |
| Max speed (km/h): | 110 | 100 | 150 | 36 |
| Cruise speed (km): | 45 | 60 – 70 | 60 – 90 | 21.6 |
| Rate of climb (m/s): | 5 | — | — | 6 |
| Endurance (min): | 55 | 120 | > 240 | 25 (@ 6 kg take-off weight) |
| Ceiling (km): | — | 2.5 | 3.5 | |
| Typical operating altitude (m): | — | — | 300 | |
| Main rotor diameter (m): | 2.206 | 3 | 3.6 | 0.381 |
| Weight of rotor (g): | — | — | — | 13 |
| Tail rotor diameter (mm): | 403 | N/A | N/A | N/A |
| Remote control radius (km): | — | 70 – 100 | — | — |
| Max power consumption (kW): | — | — | — | 3 |
| Hovering power consumption (W): | — | — | — | 666 |
| Propulsion: | Internal combustion engine | Two 10 hp internal combustion engine | Two 35 hp internal combustion engine | Electric motor |
| EM Stator size (mm): | N/A | N/A | N/A | 40 x 12 |
| EM Kv (rpm/V): | N/A | N/A | N/A | 340 |
| EM max power (W): | N/A | N/A | N/A | 660 |
| EM weight (kg): | N/A | N/A | N/A | 135 |
| Battery: | N/A | N/A | N/A | 6S LiPo |
| Current (A): | N/A | N/A | N/A | 30 |
| Frequency (Hz): | N/A | N/A | N/A | 30 – 450 |
| Pwm Frequency (kHz): | N/A | N/A | N/A | 8 |
| Battery weight (kg): | N/A | N/A | N/A | 30 |
| Size of charger (mm): | N/A | N/A | N/A | 560 x 370 x 230 |
| Weight of charger (kg): | N/A | N/A | N/A | 11 |
| Size of container (mm): | N/A | N/A | N/A | 622 x 475 x 526 |
| Weight of container (kg): | N/A | N/A | N/A | 10.9 |
See also
List of unmanned aerial vehicles of the People's Republic of China
References
- ↑ "Toaero T50". http://www.toaero.com/T50.html. Retrieved 2014.
- ↑ "Toaero T100". http://www.toaero.com/T100.html. Retrieved 2014.
- ↑ "Toaero T300". http://www.toaero.com/T300.html. Retrieved 2014.
- ↑ "Toaero X6". http://www.toaero.com/X6.html. Retrieved 2014.
 |
