Product overview
The Anhui Lianghong Technology Co., Ltd VF-13E is a battery-powered flight platform for mapping, infrastructure inspection, logistics and wide-area monitoring. Its composite-wing architecture combines vertical-lift propulsion with fixed wings and a rear pusher propeller. During transition into forward flight, the wings take over lift, the VTOL motors power down and their propellers fold to reduce drag. A redundant flight controller manages this transition automatically. Vertical takeoff and landing allow operation without a runway, while the fixed wings provide the principal lift during level cruise.
Aircraft equipment includes factory-installed motors, electronic speed controllers and a flight controller. Camera or sensor integration requires secure mounting and proper data and power connections. Operation uses a remote controller and a tablet or laptop ground control station, supporting manual flight or uploaded autonomous missions. Return-to-launch brings the aircraft back to its recorded home point and transitions it into a vertical landing. Operating restrictions exclude precipitation, winds exceeding 10 m/s and poor visibility. Site selection requires an obstacle-free area with a minimum radius of 15 meters.
Maintenance includes inspection before each flight, scheduled work after every 50 flight hours or 3 months, and recommended major servicing after every 200 flight hours or 12 months. After motor disarm, shutdown proceeds from aircraft to remote controller to ground control station. Remove batteries after flight; if reuse is not planned within 24 hours, bring them to approximately 3.8V per cell for storage. The aircraft has a 12-month limited warranty for material and workmanship defects under normal use and in accordance with the provided operational guidelines. Batteries have separate 6-month manufacturing-defect coverage.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer and model | Anhui Lianghong Technology Co., Ltd VF-13E Electric Vertical Takeoff and Landing Fixed-wing UAV |
| Product type | Electric VTOL composite-wing flight platform |
| Power source | Battery powered |
| Lift architecture | Vertical lift systems support takeoff and landing; fixed wings provide the principal lift during level cruise.During takeoff, landing and level flight. |
| Cruise propulsion and folding propellers | VTOL motors power down and their propellers fold; a rear pusher propeller supplies forward thrust.As the wings generate sufficient lift during transition to fixed-wing flight. |
| Transition control | Redundant flight controller manages automated flight-mode transition. |
| Mission control modes | Manual remote control or autonomous execution of a pre-programmed flight plan uploaded to the ground control station. |
| Payload integration | Camera or sensor mounting requires secure attachment and proper data and power connections.With a camera or sensor payload. |
| Covered aircraft equipment | Main airframe structure, factory-installed motors, electronic speed controllers and flight controller. |
| Clear operating area | Minimum clear radius of 15 meters, free from obstacles. |
| Weather operating restrictions | Do not operate in precipitation, winds exceeding 10 m/s, or poor visibility. |
| GPS acquisition | Strong GPS signal, typically more than 10 satellites. |
| Sequential power down | After motor disarm, power off the VF-13E airframe first, then the remote controller, and finally the GCS. |
| Post-flight battery management | Remove the battery from the aircraft; discharge or charge it to approximately 3.8V per cell for storage.If the battery will not be reused within 24 hours. |
| Battery storage | Approx. 3.8V per cell; cool, dry location away from flammable materials, ideally in a fire-proof bag or container. |
| Standard warranty | 12-month limited warranty from purchase covering defects in materials and workmanship.Under normal use and in accordance with the provided operational guidelines. |
| Battery warranty | Separate 6-month warranty.Against manufacturing defects. |
| Routine maintenance interval | After every 50 flight hours or 3 months: inspect moving parts, servo connectors, motor bearings and critical fasteners; clean electrical connectors and update aircraft and GCS software. |
| Major service interval | After every 200 flight hours or 12 months: recommended authorized-service-center inspection, including vibration analysis, motor balancing, sensor calibration and avionics and propulsion stress testing. |
| Long-term aircraft storage | Clean and dry the UAV; remove batteries at storage voltage; store the aircraft and components in the original or equivalent hard-case in a cool, dry environment with stable temperature.For storage periods exceeding one month. |
Request a quote for VF-13E
Send your application, destination country and expected quantity to the ChinaDrone team. We can discuss product selection, configuration and sourcing from China.
Submit your procurement requirements ↗No account needed. A model number is optional. Your enquiry is handled by ChinaDrone.
