Product overview
The Lyncon Technology FCDH-36(S)A combines a vertical-takeoff-and-landing fixed-wing UAV with an automated enclosure for recurring inspection missions. Its applications include border inspection, range patrol, oil pipeline inspection and power infrastructure inspection. The system supports unattended operation at the deployment site, with remote control, autonomous departure, inspection, precision recovery and automatic charging. Real-time monitoring and data return connect operations with cloud analysis and management, while automatic temperature regulation supports the enclosure’s role as the aircraft’s operating base.
The enclosure opens through doors on both sides of its top, with an opening time of ≤90 seconds. Its deployed dimensions reach ≤4600 × 5670 × 1600 mm, and the permitted stored-aircraft envelope is ≤4000 × 2400 × 900 mm. The aircraft has a 3.8 m wingspan and 2.3 m length, with a 36 kg maximum takeoff weight and 10 kg maximum payload capacity. Ethernet serves the enclosure, while the aircraft’s standard integrated video and data RF link is specified at 80 km.
The configuration includes RTK differential GNSS, backup single-point GNSS and triple-redundant key flight sensors. Preflight alarms and expired component life limits prevent takeoff; low battery can trigger return or diversion to an emergency landing site. Loaded cruise endurance/range is ≥2 h / 200 km, while the ≥75 km operating radius requires line of sight without interference. Environmental limits differ between components: the enclosure operates from -20°C to 60°C and the aircraft from -20°C to +55°C. Contact charging takes two hours, and the enclosure’s UPS supports ≥8 hours of operation during a power outage.
Specifications
| Specification | Value & conditions |
|---|---|
| Closed dimensions (L × W × H) | ≤4600 mm × 2650 mm × 2650 mmEnclosure closed. |
| Deployed dimensions (L × W × H) | ≤4600 mm × 5670 mm × 1600 mmEnclosure deployed. |
| Enclosure opening arrangement | Doors open on both sides of the top. |
| Enclosure lid opening time | ≤90 s |
| Enclosure weight | ≤5000 kg |
| Maximum stored UAV dimensions | ≤4000 mm × 2400 mm × 900 mm |
| Charging method and duration | Contact charging; 2 hours. |
| Enclosure ingress protection | IP65 |
| Enclosure operating temperature | -20°C to 60°C |
| UPS operating duration | ≥8 hoursDuring a power outage. |
| Landing guidance | Supports RTK precision positioning and landing. |
| Enclosure communications | Ethernet |
| Environmental monitoring | Temperature, humidity, wind direction, wind speed and rainfall monitoring. |
| System communication distance / operating radius | ≥75 kmLine of sight, without interference. |
| Aircraft dimensions | Wingspan: 3.8 m; length: 2.3 m. |
| Maximum takeoff weight | 36 kg |
| Maximum payload capacity | 10 kg |
| Cruise endurance / range | ≥2 h / 200 kmWith payload. |
| Aircraft communications link | Integrated video and data RF link; standard 80 km link.Standard equipment. |
| Flight operating radius | ≥75 kmLine of sight, without interference. |
| Maximum cruise speed | 130 km/h |
| Economical cruise speed | 85 km/h to 95 km/h |
| Data link range | ≥80 km |
| Takeoff and landing wind resistance | Grade 6During takeoff and landing. |
| Cruise wind resistance | ≥Grade 7During cruise. |
| Positioning accuracy | Less than 0.5 mDuring takeoff and landing. |
| Aircraft operating temperature | -20°C to +55°C |
| Automated inspection functions | Unattended site operation, remote control, autonomous takeoff, intelligent inspection, precision return to the enclosure, automatic charging and temperature regulation, real-time operational monitoring and data return, and cloud analysis and management. |
| Navigation and sensor redundancy | Triple-redundant gyroscopes, accelerometers, magnetic sensors, airspeed sensors and barometers; standard RTK differential GNSS with backup single-point GNSS.RTK differential GNSS supplied as standard; single-point GNSS serves as backup. |
| Flight protection and recovery architecture | Preflight self-check and servo, motor and airframe life monitoring; more than 1000 configurable emergency landing sites; automatic low-battery return or diversion; two independent propulsion systems for vertical takeoff/landing and gliding flight; landing capability with one rotor pair stopped; gliding mode following loss of multirotor control.Preflight abnormalities or component life limits inhibit takeoff; low battery triggers return or diversion; loss of multirotor control triggers gliding mode. |
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