Tianyan Engineering UAV

ianyan Engineering UAV
The Tianyan Engineering UAV is an unmanned aerial vehicle system that adopts a quadcopter aerodynamic design, can take off and land vertically, and has autonomous navigation. It is equipped with different mission equipment to complete various aerial tasks such as aerial reconnaissance, communication relay, power high-voltage line installation, radar calibration flight, power transmission and transformation line inspection, targeted object delivery, aerial surveying and commercial film and television aerial photography. Most of the body is made of carbon fiber materials, while the rest is processed from aviation aluminum. Carbon fiber materials have lighter weight and higher strength. The drone can be manually controlled for flight through a remote control, or it can be piloted automatically using GPS and Beidou navigation systems. It has multiple flight modes such as manual remote control, fixed-point hovering, route flying, pointing to where to fly, and circling around points of interest.
The Tianyan Engineering drone adopts a quick disassembly and assembly structural design, cleverly allowing users to complete the assembly and disassembly of the aircraft within 10 minutes. The disassembled aircraft is more conducive to packaging and transportation, and based on the modular design concept, it can flexibly replace onboard mission equipment to adapt to different mission requirements.
As an electric unmanned aerial vehicle, the Tianyan Project drone has very low power consumption. A set of onboard batteries can support a range of up to 60 minutes (depending on the mission payload and surrounding environment), and the replacement of onboard batteries can be completed in no more than 1 minute.   
The Tianyan project drone also has excellent flight safety design and data security design, with multiple protection modes to ensure the safety of the aircraft.
Technical Specifications
Number parameter project parameter value
Length 1.3 meters
2 Width 1.3 meters
3. Height 0.48 meters
4 Maximum mission payload of 7kg
5. Maximum cruising speed of 50km/h
Wind resistance level 6
7 maximum flight time of 65 minutes
Measurement and control distance of 10km
9 Environmental requirements: Resistance to moderate rain
10 working temperature -20 ° C -+60 ° C
11. Vertical takeoff and landing methods
12 control modes: autonomous route/fixed-point hovering/designated flight/manual remote control/interest point circling/intelligent following