| No. | Item | Specification |
| 2-1 | Type of power plant | Engine Gasoline EFI 60CC / heavy oil |
| 2-2 | Type of control device | Micro servo |
| 3.Mechanical Specification |
|
| No. | Item | Specification |
| 3-1 | Fuselage Material | Carbon fiber, fiberglass, Kevlar, PVC, etc. |
| 3-2 | Landing gear mounting position | Below the rotor stick |
| 3-3 | Mission bin position | Directly below the center of gravity of the aircraft |
| 3-4 | Structure weight | 9000g（All structural and mounting parts included） |
| 3-5 | Maximum takeoff weight | Max taking off weight 40kg |
| 3-6 | Elevation of altitude | 5200m |
| 3-7 | Maximum leveling lift | 200km |
| 3-8 | Wind resistance in fixed wing mode | <6 Level （gust 7 Level ） |
| 3-9 | Max. wind resistance in rotary wing landing mode | <5 Level（gust 6 Level ） |
| 3-10 | UAV use environment | -20℃~45℃；light rain can flying(Safe running time greater than 10min) |
| 3-11 | Rotor emergency operation time | Not less than 6.5min Rotor battery independent power supply case (non-standard power configuration) |
| 3-12 | Takeoff and landing mode | Vtol(Oil electric mixture) |
| 3-13 | Vertical takeoff power blade size | 29inch |
| 3-14 | Fixed-wing tail thrust propeller | 23inch |
| 3-15 | Fixed-wing maximum thrust-to-weight ratio | 0.56 |
| 3-16 | Altitude performance | yes |
| 3-17 | Standard unladen takeoff weight | 31kg |
| 3-18 | Safety voltage when entering landing course | <44.4V (HV) |
| 3-19 | Wing mounting angle | 2° |
| 3-20 | Airspeed tube installation number | 2（Standard with single air speed tube opening） |
| 3-21 | Whether to support the system does not power to replace the power battery pack | YES（non-standard） |
| 3-22 | Type of flight control support | All flight controls that support composite wing control can be used for this type of UAS |
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Shenzhen XQPOWER Technology Co.,Ltd |
| UAV Specification of Product Page 3/3 |
| Product Name：3744mmmm Carbon Fiber UAV Platform |
| Model: FYD-U2037 |
| 4.Electrical Specification (Function of the Performance) |
|
| 4.Electrical Specification (Function of the Performance) |
|
| No. | Item |
|
| 4-1 | Maximum payload | Max load 18kg (payload & gasoline) |
| 4-2 | Oil tank | 10L/15L |
| 4-3 | Wing Load | 260g/dm2@31kg |
| 4-4 | Endurance | 1350km |
| 4-5 | Maximum control distance | 15h@3kg;10h@8kg（gasoline） |
| 4-6 | Standard Cruising Speed | 24~40m/s（100km/h） |
| 4-7 | Maximum Cruising Speed | 25m/s |
| 4-8 | Standard battery configuration | Vtol 6s8000 mah, avionics battery 3s 5300mah |
| 4-9 | Never exceed speed | 200m/h |
| 4-10 | Stall speed | 19m/s@31kg（18m/s@ roll 25°/pitch 15°） |
| 4-11 | Minimum circling radius | 200m@21m/s（roll 18°） |
无人机整机
无人机配件
无人机服务
设备与工具
