Product overview
The Yifei Zhineng Lightning F38 combines vertical takeoff and landing with fixed-wing cruise for long-distance, wide-area tasks in power utilities, firefighting, public security and environmental protection. Its quick-release construction supports transport and field assembly, while runway-independent operation broadens launch and recovery options. The 3800mm-span aircraft uses an integrally molded carbon-fiber composite structure with a beam framework and semi-rigid shell. All avionics sit within the smooth fuselage. Payload capacity is specified by mass at 6kg.
The standard package supplies a flight platform with an airframe, controller, one 30AH propulsion battery, charger, four motors, four propellers, installation tools, customized onboard wiring, documentation and a customized packing case. Its GOE412 wing, developed from CLARK-Y, combines sweep, a 2° incidence angle and no dihedral with an inverted-V tail. Maximum endurance is 240 minutes for the unladen aircraft; empty weight excludes the battery. Operating limits include a 36kg maximum takeoff weight, Force 7 wind resistance and a -20°C to 50°C ambient range. Aircraft parameters can be customized, with the delivery contract determining the agreed configuration.
Specifications
| Specification | Value & conditions |
|---|---|
| Aircraft type | Vertical takeoff and landing fixed-wing UAV |
| Wingspan | 3800mm |
| Fuselage length | 2100mm |
| Fuselage material | Carbon-fiber composite |
| Maximum endurance | 240minUnladen aircraft. |
| Empty weight | 28kgExcluding battery. |
| Maximum payload | 6kg |
| Maximum takeoff weight | 36kg |
| Cruising speed | 80km/h |
| Maximum level-flight speed | 95km/h |
| Maximum climb speed | 5m/s |
| Maximum descent speed | 3m/s |
| Maximum flight radius | 300km |
| Maximum takeoff altitude | 5500m above sea level |
| Wind resistance | Force 7 |
| Ingress protection | IP55 |
| Operating ambient temperature | -20°C to 50°C |
| Airframe | 1 setStandard supplied configuration. |
| Remote controller | 1 unitStandard supplied configuration. |
| Propulsion battery | 1 battery, 30AHStandard supplied configuration. |
| Charging equipment | 1 unitStandard supplied configuration. |
| Motors | 4 CW/CCW motors, EF MotorStandard supplied configuration. |
| Propellers | 4 CW/CCW propellers, EF PropellerStandard supplied configuration. |
| Installation tools | 1 tool kitStandard supplied configuration. |
| Onboard wiring harness | 1 customized setStandard supplied configuration. |
| Product documentation | 1 set containing a certificate of conformity and operating manualStandard supplied configuration. |
| Packing case | 1 customized caseStandard supplied configuration. |
| Propulsion, deployment and intended tasks | All-electric compound-wing VTOL aircraft combining multirotor takeoff and landing with fixed-wing flight, without requiring a dedicated runway. |
| Structure and avionics integration | Integrally molded carbon-fiber composite construction combines a beam framework and semi-rigid shell; all avionics are integrated inside the smooth, unified fuselage. |
| Aerodynamic geometry | GOE412 airfoil developed from CLARK-Y; swept wing with elliptical spanwise layout, 2° incidence and no dihedral. Ailerons occupy 15% of wing area and 50% of wing length. Center of gravity is at 30% chord. The inverted-V tail has an area equivalent to 15% of wing area, with mixed-control surfaces occupying 20% of V-tail area. |
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