Feima V1 Hybrid VTOL Fixed-Wing UAV, Heavy-Lift Long-Endurance Survey & Remote Sensing Drone
Survey, Remote Sensing, Patrol,
Emergency Command & Logistics
Transportation
Product Overview
Feima V1 is a new-generation medium hybrid vertical takeoff and landing fixed-wing UAV. It adopts a blended-wing composite aerodynamic layout and hybrid architecture combining 8 VTOL rotors and a combustion propulsion engine. Built for long-range, heavy-payload and extreme-environment operations. Equipped with dual-redundant flight control, multi-sensor fusion navigation, optional wing anti-icing system and onboard power generation system. Supports quick-swap modular payload bays, compatible with heavy LiDAR, large-format survey cameras, long-range EO/IR gimbal, emergency communication equipment and logistics cargo pods. Perfect for large-scale 3D reconstruction, oil & gas pipeline inspection, power line patrol, plateau & polar scientific missions, disaster relief and material delivery.
40 kg
Max Payload
10 h
Max Endurance
1000 W
Power Supply Capability
VTOL
Vertical Takeoff & Landing
V1 Core Advantages
Up to 10 Hours Endurance
Hybrid fuel-electric power system delivers maximum 10-hour flight duration, greatly reduce takeoff frequency and transit work for ultra-large-area missions.
Max 40kg Mission Payload
MTOW 150kg, support heavy-duty payload combinations, compatible with multiple professional sensors and emergency delivery equipment.
8-Rotor VTOL, No Runway Needed
Vertical takeoff & landing on flat ground; automatically switch to fixed-wing cruise mode for long-distance efficient flight.
Airworthiness-Oriented Design
Developed following civil aviation airworthiness requirements, dual redundant flight control, multi-sensor fusion navigation for aviation-grade safety.
Extreme Environment Adaptability
Wing anti-icing coating, battery thermal management system, stably operate at -25℃ ~ +50℃, support plateau, cold region, polar mission.
1000W On-Board Power Supply
Integrated generator supplies power to payloads and charges airborne batteries in real time, ensuring continuous power supply during long missions.
Hybrid Power & Blended Wing-Body Platform
Advanced Composite Airframe
V1 adopts blended wing-body composite structure, optimized aerodynamic efficiency, equipped with 8 sets of vertical lift rotors + rear propulsion engine. Independent fuel-electric hybrid architecture separates lift and cruise power.
Hybrid Fuel-Electric Architecture
Aero-engine works as main power generator, provides continuous power supply; electric system controls vertical takeoff and landing. Real-time battery charging during cruise.
Explosion-Proof Fuel Tank System
Self-developed flexible fuel bladder + explosion-proof structure, adjustable fuel supply system, effectively improve safety during long-distance flight.
6.1m Large Wingspan
Large aspect ratio wing design, low cruise power consumption, maximize flight endurance, suitable for thousand-kilometer long-range missions.
Automatic Mode Switching
Complete automatic flight workflow: VTOL climb → switch fixed-wing cruise → mission execution → convert back to VTOL mode for autonomous landing.
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PRODUCT DESCRIPTION
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Dual Flight Control System
Adopting dual‑channel hot‑backup design, the flight control system communicates with onboard sensors, servos and ESCs for real‑time flight monitoring. Its arbitration unit switches control to the backup controller and initiates emergency return once the primary unit fails, improving flight safety.
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Wing Anti-Icing
The wing leading edge adopts IPN‑blended anti‑icing nanomaterial coating. It delivers strong hydrophobicity, higher density, surface hardness and stain resistance to lower ice adhesion, enabling reliable anti‑icing performance for UAVs in polar and frigid environments.
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Communication Link Encryption
The communication link uses software and hardware coupled encryption to ensure the security of data communication.
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Dual Differential Board
It adopts dual differential board and dual aerial antenna design, which support directional, satellite-based differential and Beidou-only functions.
Aviation-Grade Redundant Safety Architecture
V1 adopts full-link redundancy design for long-distance unattended missions in remote areas, greatly reducing flight risks in complex and unreachable terrain.
- Dual hot backup flight control system, seamless switching under single failure
- Multi-sensor fusion navigation: GNSS, IMU, radar, airspeed tube triple redundancy
- Independent long-range communication link, support remote monitoring over long distance
- Multiple automatic return strategies: low fuel, lost link, system abnormality
- Real-time flight status recording, full-process data logging
- Anti-icing system for wings, stable flight under low temperature icing risk
- Multi-layer fault detection and automatic fault isolation algorithm
Modular Payload Compatibility
Open standard payload interface, support single or combined sensor configuration, realize one platform for multiple missions.
Aerial Survey Camera / Oblique Camera
Large-area orthophoto mapping, city oblique 3D modeling, land resource survey
LiDAR Laser Radar System
Forest penetration survey, terrain mapping under vegetation, complex mountain point cloud collection
Hyperspectral / Multispectral Sensor
Ecological monitoring, water quality survey, mineral resource exploration, crop growth monitoring
EO/IR Triple Optical Pod
Long-distance patrol, forest fire prevention, border inspection, day & night surveillance
Emergency Communication Relay
Disaster area communication reconstruction, emergency command network coverage
Cargo Delivery Module
Remote emergency supplies transport, low-altitude logistics, mountain material delivery
Ground Station & Supporting Software
UAV Manager Professional
Professional desktop software for large-area remote sensing mission planning, flight monitoring and post-processing.
- Long-distance fixed-wing intelligent route planning
- 3D terrain following flight route design
- Real-time aircraft status & payload monitoring
- LiDAR, aerial image, hyperspectral data processing workflow
- POS data fusion, aerial triangulation & model generation
Customized Industrial Ground Station
Dedicated ground station hardware solution for long-endurance large platform, stable communication for long-distance mission.
- Multi-screen real-time payload video display
- Emergency flight parameter modification & mission control
- Offline map support for remote no-network areas
- Full flight log recording, fault diagnosis support
- Support remote technical debugging link
Wide Range of Industry Applications
Main Technical Specifications
| Item | Parameter |
|---|---|
| Aircraft Layout | 8-Rotor VTOL + Fixed-Wing Hybrid VTOL |
| Wingspan | 6.1 m |
| Max Takeoff Weight | 150 kg |
| Max Mission Payload | 40 kg |
| Max Endurance | Up to 10 h (depends on payload & wind) |
| Max Cruise Range | Approx. 1100 km |
| Cruise Speed | 120 km/h |
| Control Radius | Long-range customized data link |
| Max Takeoff Altitude | 4500 m ASL |
| Service Ceiling | 6000m |
| Power System | Fuel-electric hybrid, built-in generator, 1000W onboard power |
| Safety Design | Dual redundant flight control, multi-sensor fusion navigation |
| Takeoff & Landing | Fully automatic vertical takeoff & landing |
| Payload Interface | Universal standardized mounting interface |