Product overview
The Guangdong Fanya Technology EM-100L/KPH is a heavy-lift flight platform for aerial supply transport, emergency rescue support, illumination, communications relay, and firefighting munition delivery. Its carbon-fiber body carries four arms and eight propellers, with removable arms for transport and whole-aircraft rain and water protection. Wheelbase is ≤1950mm, while folded dimensions are less than 770×720×780mm. The aircraft and accessories necessary for flight can be packed into one protective case, and deployment time is specified as less than 1min.
The twin-engine gasoline-electric range-extender system combines a 20L fuel tank with two flight-battery groups that support charging during flight. Maximum payload is greater than 41kg, with a rated mission payload of ≥30kg. Endurance depends on loading: greater than 2h unloaded and greater than 50min with 30kg aboard. Maximum takeoff weight is greater than 100kg at sea level, with a standard takeoff weight of 90–93kg under the same condition. The operating temperature range is −20°C to 50°C, and maximum flight altitude is 2000m.
Mission integration centers on interchangeable electro-optical pods and quick-release support for descent equipment, searchlights, release devices, firefighting munitions, and MESH networking equipment. These are supported configurations; parachute descent is explicitly optional. The handheld ground station integrates control, data, and video links, with video up to 1080p@60fps and a 5.46-inch touchscreen. Ordinary-signal control distance is 15km; relay-assisted flight distance is separately specified as greater than 100km, alongside a 30km range specification. Automated functions include route planning, orbiting, return along the original route, and configurable flight boundaries.
Specifications
| Specification | Value & conditions |
|---|---|
| Aircraft architecture | Twin-engine gasoline-electric hybrid flight platform; carbon-fiber body, four arms and eight propellers, removable arms, and whole-aircraft rain and water protection. |
| Wheelbase | ≤1950mm |
| Wind resistance | Maximum wind resistance: ≥force 7. |
| Range | 30km |
| Propeller dimensions | 42.3×16.5inch |
| Takeoff weights | Maximum takeoff weight: greater than 100kg; standard takeoff weight: 90–93kg.At sea level. |
| Maximum endurance | Greater than 2hUnloaded. |
| Loaded endurance | Greater than 50minWith a 30kg payload. |
| Payload capacity | Maximum payload: greater than 41kg; rated mission payload: ≥30kg. |
| Cruising speed | 5m/s |
| Maximum flight speed | Greater than 8m/s |
| Maximum flight altitude | 2000m |
| Fuel capacity | 20L |
| Power system and cooling | Twin-engine range-extender power system; maximum engine power: 14.8kw; cooling described as four-engine independent water-radiator cooling. |
| Operating temperature | −20°C to 50°C |
| Deployment time | Less than 1min |
| Folded dimensions | Less than 770×720×780mmAircraft folded. |
| Positioning | Dual-redundant GPS; support for dual-antenna direction finding and RTK. |
| Control and relay distances | Remote-control distance with ordinary signal: 15km; flight distance using signal relay: greater than 100km.Ordinary signal for 15km; signal relay for flight distance greater than 100km. |
| Mission applications | Aerial cargo transport, controlled descent of supplies at rescue sites, soft landing of supplies, emergency illumination, aerial lighting guidance, communications relay, emergency rescue, firefighting munition delivery, and mesh networking. |
| Fuel and battery management | Ground-station display of remaining fuel, fuel percentage, and battery status; two flight-battery groups support charging during flight. |
| Transport configuration | Aircraft and accessories necessary for flight can be stored together in one protective case. |
| Automated flight functions | One-button takeoff and landing, route planning, point-directed flight, point-of-interest orbiting, intelligent return, and return along the original route. |
| Flight protection and redundancy | Broken-propeller protection; optional parachute descent; orbiting around a defined point and radius; automatic switching to redundant sensors upon sensor failure.Parachute descent is optional. |
| Flight-area restrictions | Configurable circular or polygonal flight boundaries and minimum or maximum flight altitude; warning and hover/return when approaching a prohibited area.When approaching a prohibited flight area. |
| Mission equipment integration | Support for an autonomously controlled remote intelligent descent system. |
| Payload interchange and expansion | Interchangeable electro-optical pods; quick-release installation support for remote intelligent descent equipment, firefighting munitions, searchlights, release devices, and MESH networking equipment; expansion support for higher-power link equipment. |
| Handheld ground control station | Integrated data, remote-control, and video links; video up to 1080p@60fps; 5.46-inch LCD touchscreen with 600nit brightness and 1080p resolution. |
| Control interfaces and live information | Interconnected dual controls with synchronized video and flight data; route and mission planning; altitude, speed, location, and flight-parameter settings; HDMI, AV, and SDI video outputs; BeiDou, GPS, and GLONASS compatibility; autonomous travel to entered latitude/longitude coordinates. |
| Engine service interval and restart | Industrial aviation engines described as maintenance-free within 300 hours; restart after an engine stops in flight. |
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