Vertical Take-off and Landing Fixed Wing Drone; Payload 5 Kilograms; 10 Hours Flight Time

• Height: Medium Altitude
• Operating Radius: Medium Range
• Size: Miniature
• Usage: Industrial
• Structure: Fixed-Wing UAV
• Power: Battery
• Model NO.: HF101A-C
• Maximum Take-off Weight: 45kg
• Maximum Load Capacity: 5kg
• Transport Package: Packing
• Specification: Aviation box packaging
• Trademark: HFHW
• Origin: China
• Production Capacity: 1000

Product Description

1. Features

It is easy to assemble and maintain, with its good adaptability to environment and stable flying, it is wide used in various fields.  

• Easy to assemble and maintain.
• 

It is developed and researched in accordance with applicability with the concept of module design, integration design and lightweight design.   

1. With module design, it's easy to set and disassemble
2. It is able to take off and landing vertically without runway
3. System monitoring, transport, and support can be achieved through one vehicle
4. it can be operated without topographic and environmental limitation
5. Spared gears and devices are prepared in vehicle that makes it convenient to change and fix anytime and anywhere

• good adaptability to environment and stable flying

1. Through the testing of operating in extreme temperature, vibrating, impacting and strong wind, it proves its good adaptability to environment.
2. With adopting carbon fiberreinforcedresin matrix composites materials, it has strong resistant to corrosion.  
3. It adopts LE adaptive flying control algorithm with great robustness, controlling accuracy and stability.
4. it can be operated in hostile environment with high working efficiency

• Wide used in various fields

It is able to take off and landing vertically without runway. It can carry goods with heavy weight and attach different payload to finish various tasks. With its good adaptability to environment, it can be operated without topographic and environmental limitation.   

 

1. Parameter

The maximum take-off weight	45kg
The maximum payload	5kg
Dimension (outline)	2m×4m×0.6m
Dimension (for packaging)	1.5m×0.5m×0.6m
Power	gas-electric hybrid
Speed of fixed wings	100km/h -120km/h
Duration	8h(gasoline),10h(heavy oil)
Rising limitation	5000m
Take-off and landing approach	vertical take-off and landing
Picture transmission system	100km(inter-visible,no covering)
Navigation	GPS( can choose multimode )+ MIMU
Storage temperature	-40ºC~+55ºC
Operating temperature	-45ºC~+65ºC
Take-off time(stretching time is included)	≤10min
Field	10*10m platform for take-off and landing, grassland, sand land.
Weather requirement	It can operate under strong breeze, light rain and light snow

 

1. UAV platform

Aircraft platform is used for UAV to carry payload to targets areas and it is able to detect and monitor. It consists of a body part, power equipment, flying control system, navigation system and electric equipment.

1. It adopts the structure with upper single-wings and two-tails brace with four motors, reversed V-shaped tail and backward pushing engine. It can achieve vertical take-off and cruising through four motors that pass power to propellers, and it can also achieve vertical landing through fixed wings flying mode.It is able to obtain high life-drag ratio to realize aerodynamic efficiency,longer endurance time and faster flying speed  if  flying with this mode.
2. Quadrotor lift system is consists of lithium batteries, electronic speed controllers, electromotors and propellers.Lithium batteries output power that provides voltage to speed controller which can access to flight controlling system. DC connector switch is controlled by flight controlling system. Then, voltage is inputted into electromotors that drive propellers to work, which helps UAV to achieve vertical take-off.  
3.   It adopts oil-driven engine to produce horizontal thrust. This engine is specially designed for aircraft with high power-to-weight ratio and stability, it can dissipate heat very well during its operation. With its electric starting system, the UAV can achieve dual function,not only to start the engine, but also can generate electricity after the engine starts to charge rotor wings. In addition, gasoline 3w70 and heavy oil share the same interface, it enable to change easily
   Photoelectric pod
   
4. It adopts two axis gyroscope-stabilized platform with a conducting ring, which can achieve 360° rotating. It consists of visible light camera with 30x optical zoom, long-wave IR imaging module without cooling system and laser range finder. It is widely use on aircraft for detection,identification, tracking and locating, which can achieve aerial mapping, monitoring and investigation.
   With its compact and light structure,it is able to be assembled on various UAV and vessels to realize the application on sea and air.
   Parameter:

   Visible light camera: pixels	pixels	1920×1080
   	focal length	4.3mm~129mm,30x optical zoom
   	horizon field of view	63.7º~2.3º
   long-wave IR imaging without cooling system:pixels	pixels	640×512
   	pixel size	12um
   	NETD	40mk
   	focal length	63mm/F0.83
   	field of view	6.9º×5.5º
   laser ranging	accuracy	±2m
   	distance	50~4000m
   Servo platform	Angular accuracy	≤2mrad
   	angular accuracy	≤100μrad(1σ)(2°/1Hz,1°/2Hz swing)
   	Maximum angular velocity	≥50°/s
   	Maximum angular acceleration	≥90°/s²
   Dimension	≤Φ170mm×221mm
   weight	≤2.4kg
   operating temperature	-20ºC~60ºC

   
    Ground controlling devise.
   The ground controlling devise consists of controlling software for ground and payload. It can read data of aircraft and payload through the connection with ground terminal. With this feature, it can make instructions, monitor flight, obtain payload information and images in real time, and draw flying routes.