Unmanned helicopter

Unmanned helicopter
This aircraft model is lightweight and can carry various spectral gimbals such as visible light and infrared, airborne LiDAR, laser irradiators, LED lighting, and other onboard equipment. It can achieve visible light and infrared detection, laser modeling, laser ranging, providing target coordinates, target tracking, and aerial evidence collection. It can also be equipped with flight testing equipment to meet testing needs. The aircraft can output a maximum power of 500W and 28V, which can meet the aerial power supply needs of various devices. External electrical equipment does not require batteries, effectively reducing equipment weight and thus obtaining longer aerial residence time, significantly improving the efficiency of equipment and aircraft work.
This aircraft model has the characteristics of long hovering time, fast flight speed, and strong wind resistance. The aircraft has a self weight of 36 kilograms, an external fuel tank of 16L, and a maximum endurance time of over 5 hours. At the same time, this model can be equipped with fully independently developed gasoline engines and heavy oil engines, meeting the needs of different fields of application. Among them, heavy oil engines can be widely used in flammable and explosive fields such as forest patrols, oil and gas fields, maritime affairs, and oil and gas pipeline inspections.
The maximum flight altitude of this model is 3500 meters, with a maximum flight speed of over 100 kilometers per hour. It has a wind resistance of 6 levels and superior performance, reaching the world's advanced level.
This aircraft model can perform beyond visual range operations and can fly in the air through network, achieving relay operations. By using the joint flight of the operating aircraft and relay aircraft, it can achieve mission flights in complex geographical environments such as low altitude operations in mountainous areas and low altitude operations on the sea surface. On the flight control system, a highly integrated design scheme with small size and strong modularity has been implemented. The main control adopts an integrated damping structure, sensors adopt dual redundancy hot backup mode, independent external GPS+magnetic compass module, built-in 8G data storage space, supporting track point flight, block/strip mapping route flight, jumping point, guidance, temporary route flight, online speed and altitude adjustment, pre flight inspection function, engineering mode parameter adjustment, data playback function, semi physical simulation function, and pod control. Technical parameters of KYK60 multifunctional unmanned helicopter: 1. Boundary dimensions (excluding main rotor): 2280 x 645 x 720mm (length x width x height) 2. Main rotor diameter: 2680mm 3. Tail rotor diameter: 470mm 4. Empty takeoff weight: 36kg (excluding fuel) 5. Maximum takeoff weight: 70kg (sea level altitude, ambient temperature 20 ℃, ground effect hovering) 6. Maximum flight speed: 30m/s (calm wind, sea level altitude, ambient temperature 20 ° ℃) 7. Maximum altitude: 3500m (empty load, a small amount of fuel) 8. Maximum load: 35kg (including fuel, sea level altitude) 9. Fuel capacity: external fuel tank 16L10. Work Temperature: -20 ℃ to 50 ℃ 11 Fuel consumption: No load: 41.6ml/min (at sea level, ambient temperature of 20 ℃)
Full load: 83.3ml/min (mission load 20kg, sea level altitude, ambient temperature 20 ℃) 12 engine type: two-stroke horizontally opposed twin cylinder
Working volume: 170CC
Cylinder diameter: 52mm
Travel: 40mm
Ignition method: CDI electronic ignition
Starting method: electric start
Rated power: 10kW@8500rpm
Rated speed: 7800rpm
Cooling method: water cooling
Fuel: 92 # or above gasoline
Mixing ratio: 40:1