Product overview
The droneyee ZV15E is a hybrid-wing UAV system intended for sustained work over large areas, including inspection, search and reconnaissance. It combines electric vertical takeoff and landing with ultralight carbon-fiber composite construction. Deployed dimensions are 3010 × 1630 × 540 mm, with a ±10 mm tolerance, and maximum takeoff weight is 17.5 kg. Its modular payload mounting supports changing between monitoring, aerial surveying and emergency tasks. Maximum payload is 3 kg; the configuration is an equipped flight platform with onboard computing, networking and flight-control software.
The onboard computer provides up to 40T of computing capacity for airborne processing, target recognition, tracking and autonomous mission planning. Multiple AI-version ZV15E aircraft can form an autonomously controlled swarm, with a stated coordination count of 16 aircraft. The accompanying software handles mission areas, targets, terrain-following routes, payload control and aircraft health. An airborne networking module connects the aircraft to the manufacturer's cloud platform for remote takeoff and landing, control from multiple terminals, cloud data processing and mission updates. Avionics incorporate redundant flight-control sensors, multiple satellite-positioning systems and emergency protection mechanisms.
Endurance depends on payload: the unloaded figure is 360 min, also expressed as 6 h, while a 1 kg payload pod reduces it to 5.5 h. Standard communication distance is 50 km under unobstructed line-of-sight conditions without interference. Maximum speed is 120 km/h, service ceiling is 7000 m, and takeoff and landing elevation is 5500 m. Operating temperature spans -25 °C to 60 °C. Wind resistance is Force 5 for takeoff and landing and Force 6 in cruise; light-rain flight is supported. Single-person deployment is ≤3 min, while deployment and packing time is separately specified as ≤5 min.
Specifications
| Specification | Value & conditions |
|---|---|
| Product type | ZV15E hybrid-wing UAV system and long-endurance flight platform. |
| Takeoff and landing | Electric vertical takeoff and landing. |
| Deployed dimensions | 3010 × 1630 × 540 mm (±10 mm). |
| Maximum payload | 3 kg. |
| Unloaded endurance | 360 min.Unloaded. |
| Endurance by payload configuration | 6 h unloaded; 5.5 h with a 1 kg payload pod.Unloaded or carrying a 1 kg payload pod, respectively. |
| Service ceiling | 7000 m. |
| Deployment time | ≤3 min with one person.Single-person deployment. |
| Deployment and packing time | ≤5 min. |
| Rain operation | Can fly safely in light rain.Light rain. |
| Maximum takeoff weight | 17.5 kg. |
| Maximum flight speed | 120 km/h. |
| Communication distance | 50 km.Standard configuration; line of sight without interference. |
| Operating elevation | 5500 m.Takeoff and landing. |
| Wind resistance | Force 5 during takeoff and landing; Force 6 during cruise.Takeoff and landing versus cruise. |
| Operating temperature | -25 °C to 60 °C. |
| Coordinated aircraft count | 16 aircraft. |
| Structural material | Ultralight carbon-fiber composite construction. |
| Empty-weight reduction | Approximately 30% lower empty weight.Compared with a conventional composite fuselage. |
| Onboard computing | Equipped with an onboard computer providing up to 40T of computing capacity. |
| Autonomous processing and missions | Supports real-time airborne data processing, autonomous mission flight, mission-target decisions, target recognition, target tracking and autonomous mission planning. |
| Autonomous swarm operation | Supports autonomous swarm control and coordinated flight for wide-area searches, multipoint reconnaissance and collaborative inspection.Multiple AI-version ZV15E aircraft. |
| Avionics safeguards | Redundant flight-control sensors, multiple satellite-positioning systems and multiple emergency protection mechanisms. |
| Supplied flight-control software | Professional flight-control software supports mission-area management, target setting, terrain-following route planning, payload control and aircraft health management. |
| Network equipment and remote functions | Equipped with an airborne networking module; supports remote takeoff and landing, data access from multiple terminals, remote control, cloud processing and remote mission updates.Remote functions operate with the manufacturer's cloud platform. |
| Payload integration | Modular mounts accommodate interchangeable mission payloads for monitoring, aerial surveying and emergency applications.With suitable mission payloads installed. |
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