FBH 无人机
为严苛作业环境打造的先进空中解决方案
FBH 无人机是一款专为多元化商业与工业应用而设计的高性能空中平台。该系统提供强大的作业能力，旨在提升运营效率、保障作业安全，并为复杂的物流运输与监测任务提供多场景解决方案。
核心能力
作业优势
FBH 系统凭借以下显著优势脱颖而出：
从农业到应急救援，FBH 无人机均能提供卓越的性能表现、作业效率与安全保障。
强劲载荷能力
载重范围 100 公斤至 1500 公斤，可满足多种物料与设备的运输需求。
超长续航性能
标配 6 小时续航能力（支持定制扩展），大容量油箱保障持久作业。
可靠动力方案
可选配全球知名品牌的成熟汽车发动机配置，动力输出稳定可靠。
宽广性能边界
巡航速度达 120 公里/小时，最高作业海拔 5000 米，并具备实测抗风8级的作业稳定性。
集成智能安全系统
搭载AI驱动的智能飞行控制系统（SFCS），可在复杂环境中实现智能避障、自动导航与精准地形测绘。
多行业应用潜力
FBH 无人机为以下核心领域提供专业解决方案：
农业应用：提升作业效率与作业精度
- 高效日作业覆盖：单日作业能力达330公顷（约4950亩），支持播种、施肥、饲喂全流程作业。
- 智能物料播撒：支持0.5-10毫米粒径物料喷洒，强力下压风场设计确保农药有效穿透棕榈树等浓密作物冠层直达目标区域。
应急响应：关键空中支援
- 先进实时感知： 载热成像与多光谱传感器，动态探测火点位置、蔓延范围及温度分布。
- 强化灭火支持：支持森林网格化监测，并可挂载灭火弹进行空中投掷，提升响应安全性与扑救效能。
- 高清数据获取：8K超高清镜头结合AI智能识别，为关键决策提供高清晰度视觉信息支持
清洁应用：保障资产高效运行
- 安全无损清洁：无人机清洁方案能显著降低（如人工清洁导致的）面板微裂纹风险，提升作业人员安全性
- 适应严苛环境： 在偏远干旱、水资源匮乏的区域尤其高效，克服传统人工清洁限制。
物流运输：强劲空中配送
- 超大运载能力：单机载重高达1500公斤。
- 多场景适配：适用于物资投送、移动信号源架设、河堤加固支援及空中巡查等多样化任务。
- 自动化物流特性：集成自动抗摇摆系统、预设装卸点自主飞行及重量检测功能，优化作业流程。
- 编队协同作业：可多机编组执行货运任务，大幅提升总体运输量。
测绘应用：高精度空间数据采集
- 精细地形捕捉：依托先进地形测绘能力，结合8K超高清镜头与AI智能识别，为各类勘测需求生成高分辨率地图及三维模型。
- 广域高效覆盖：超长续航与强劲巡航速度相结合，实现大面积区域的高效测绘，适用于土地管理、工程规划及环境监测。
- 灵活传感器集成： 强大载荷能力支持集成多种专业测绘传感器（如激光雷达LiDAR、先进多光谱成像仪），满足定制化项目需求。
- 精准数据赋能决策：提供高精度地理空间数据，为基建工程、资源管理及地形分析提供关键决策依据。
技术规格
FBX-149
Series & Configuration
| Rated payload | 80 kg |
| Airframe | Tandem twin-rotor VTOL |
| Propulsion | Fuel-powered piston |
| Status | Product line |
性能数据
| Maximum range (no payload) | — |
| Cruise speed | — |
| Service ceiling at full payload | — |
| Operating altitude band | Below 3,000 m — standard low altitude |
Take-off & Landing
| Runway required | None — vertical take-off and landing |
| Minimum landing area | 20 × 20 m of level ground |
Flight Control & Safety
| Flight control | Redundant flight-control system |
| Engine configuration | Single- or twin-engine, selected by the risk profile of the route |
| Obstacle avoidance | Multi-modal sensing |
| Autonomy | AI-assisted flight control and navigation |
Fuel & Propulsion Roadmap
| Current fuel | Gasoline |
| 2028 | Diesel — raises energy density for long logistics and fire-suppression legs |
| 2030 | Hydrogen blend, then pure hydrogen |
Mission Configurations
| Cargo | Standard cargo bay; cold-chain cargo module |
| Lifting | Industrial lifting platform for sling loads |
| Public safety | Emergency response variant |
Ground Ecosystem
| Infrastructure | Smart vertiports and refuelling stations |
| Fleet | Cloud-based fleet management and dispatch |
| Support | Full-lifecycle maintenance programme |
Supplied With The Technical Brief
| On request | Maximum take-off weight, airframe dimensions, rotor diameter, endurance at rated payload, fuel capacity, wind-resistance rating, control-link range and positioning accuracy. We go through these on a call so the figures match the mission. |
FBH-300 PRO
Series & Configuration
| Rated payload | 300 kg |
| Airframe | Tandem twin-rotor VTOL |
| Propulsion | Aviation piston engine |
| Status | In commercial service since 2018 |
性能数据
| Maximum range (no payload) | — |
| Cruise speed | — |
| Service ceiling at full payload | — |
| Operating altitude band | Below 3,000 m — standard low altitude |
Take-off & Landing
| Runway required | None — vertical take-off and landing |
| Minimum landing area | 20 × 20 m of level ground |
Flight Control & Safety
| Flight control | Redundant flight-control system |
| Engine configuration | Single- or twin-engine, selected by the risk profile of the route |
| Obstacle avoidance | Multi-modal sensing |
| Autonomy | AI-assisted flight control and navigation |
Fuel & Propulsion Roadmap
| Current fuel | Gasoline |
| 2028 | Diesel — raises energy density for long logistics and fire-suppression legs |
| 2030 | Hydrogen blend, then pure hydrogen |
Mission Configurations
| Cargo | Standard cargo bay; cold-chain cargo module |
| Lifting | Industrial lifting platform for sling loads |
| Public safety | Emergency response variant |
Ground Ecosystem
| Infrastructure | Smart vertiports and refuelling stations |
| Fleet | Cloud-based fleet management and dispatch |
| Support | Full-lifecycle maintenance programme |
Supplied With The Technical Brief
| On request | Maximum take-off weight, airframe dimensions, rotor diameter, endurance at rated payload, fuel capacity, wind-resistance rating, control-link range and positioning accuracy. We go through these on a call so the figures match the mission. |
FBH-300
Series & Configuration
| Rated payload | 300 kg |
| Airframe | Tandem twin-rotor VTOL |
| Propulsion | Automotive-derived hybrid piston |
| Status | Prototype verified in flight, May 2026 |
性能数据
| Maximum range (no payload) | 500 km |
| Cruise speed | 120 千米/小时 |
| Service ceiling at full payload | 5,000 米 |
| Operating altitude band | Below 3,000 m — standard low altitude |
Take-off & Landing
| Runway required | None — vertical take-off and landing |
| Minimum landing area | 20 × 20 m of level ground |
Flight Control & Safety
| Flight control | Redundant flight-control system |
| Engine configuration | Single- or twin-engine, selected by the risk profile of the route |
| Obstacle avoidance | Multi-modal sensing |
| Autonomy | AI-assisted flight control and navigation |
Fuel & Propulsion Roadmap
| Current fuel | Gasoline |
| 2028 | Diesel — raises energy density for long logistics and fire-suppression legs |
| 2030 | Hydrogen blend, then pure hydrogen |
Mission Configurations
| Cargo | Standard cargo bay; cold-chain cargo module |
| Lifting | Industrial lifting platform for sling loads |
| Public safety | Emergency response variant |
Ground Ecosystem
| Infrastructure | Smart vertiports and refuelling stations |
| Fleet | Cloud-based fleet management and dispatch |
| Support | Full-lifecycle maintenance programme |
Supplied With The Technical Brief
| On request | Maximum take-off weight, airframe dimensions, rotor diameter, endurance at rated payload, fuel capacity, wind-resistance rating, control-link range and positioning accuracy. We go through these on a call so the figures match the mission. |
FBH-500
Series & Configuration
| Rated payload | 500 kg |
| Airframe | Tandem twin-rotor VTOL |
| Propulsion | Hybrid aviation piston |
| Status | Product line |
性能数据
| Maximum range (no payload) | 500 km |
| Cruise speed | 120 千米/小时 |
| Service ceiling at full payload | 5,000 米 |
| Operating altitude band | Below 3,000 m — standard low altitude |
Take-off & Landing
| Runway required | None — vertical take-off and landing |
| Minimum landing area | 20 × 20 m of level ground |
Flight Control & Safety
| Flight control | Redundant flight-control system |
| Engine configuration | Single- or twin-engine, selected by the risk profile of the route |
| Obstacle avoidance | Multi-modal sensing |
| Autonomy | AI-assisted flight control and navigation |
Fuel & Propulsion Roadmap
| Current fuel | Gasoline |
| 2028 | Diesel — raises energy density for long logistics and fire-suppression legs |
| 2030 | Hydrogen blend, then pure hydrogen |
Mission Configurations
| Cargo | Standard cargo bay; cold-chain cargo module |
| Lifting | Industrial lifting platform for sling loads |
| Public safety | Emergency response variant |
Ground Ecosystem
| Infrastructure | Smart vertiports and refuelling stations |
| Fleet | Cloud-based fleet management and dispatch |
| Support | Full-lifecycle maintenance programme |
Supplied With The Technical Brief
| On request | Maximum take-off weight, airframe dimensions, rotor diameter, endurance at rated payload, fuel capacity, wind-resistance rating, control-link range and positioning accuracy. We go through these on a call so the figures match the mission. |
FBH-1000
Series & Configuration
| Rated payload | 1,000 kg |
| Airframe | Tandem twin-rotor VTOL |
| Propulsion | Hybrid aviation piston |
| Status | Product line |
性能数据
| Maximum range (no payload) | — |
| Cruise speed | — |
| Service ceiling at full payload | — |
| Operating altitude band | Below 3,000 m — standard low altitude |
Take-off & Landing
| Runway required | None — vertical take-off and landing |
| Minimum landing area | 20 × 20 m of level ground |
Flight Control & Safety
| Flight control | Redundant flight-control system |
| Engine configuration | Single- or twin-engine, selected by the risk profile of the route |
| Obstacle avoidance | Multi-modal sensing |
| Autonomy | AI-assisted flight control and navigation |
Fuel & Propulsion Roadmap
| Current fuel | Gasoline |
| 2028 | Diesel — raises energy density for long logistics and fire-suppression legs |
| 2030 | Hydrogen blend, then pure hydrogen |
Mission Configurations
| Cargo | Standard cargo bay; cold-chain cargo module |
| Lifting | Industrial lifting platform for sling loads |
| Public safety | Emergency response variant |
Ground Ecosystem
| Infrastructure | Smart vertiports and refuelling stations |
| Fleet | Cloud-based fleet management and dispatch |
| Support | Full-lifecycle maintenance programme |
Supplied With The Technical Brief
| On request | Maximum take-off weight, airframe dimensions, rotor diameter, endurance at rated payload, fuel capacity, wind-resistance rating, control-link range and positioning accuracy. We go through these on a call so the figures match the mission. |
FBX-149
|
FBH-300 PRO
|
FBH-300
|
FBH-500
|
FBH-1000
|
|
|---|---|---|---|---|---|
| Series & Configuration | |||||
| Rated payload | 80 kg | 300 kg | 300 kg | 500 kg | 1,000 kg |
| Airframe | Tandem twin-rotor VTOL | ||||
| Propulsion | Fuel-powered piston | Aviation piston engine | Automotive-derived hybrid piston | Hybrid aviation piston | Hybrid aviation piston |
| Status | Product line | In commercial service since 2018 | Prototype verified in flight, May 2026 | Product line | Product line |
| 性能数据 | |||||
| Maximum range (no payload) | — | — | 500 km | 500 km | — |
| Cruise speed | — | — | 120 千米/小时 | 120 千米/小时 | — |
| Service ceiling at full payload | — | — | 5,000 米 | 5,000 米 | — |
| Operating altitude band | Below 3,000 m — standard low altitude | ||||
| Take-off & Landing | |||||
| Runway required | None — vertical take-off and landing | ||||
| Minimum landing area | 20 × 20 m of level ground | ||||
| Flight Control & Safety | |||||
| Flight control | Redundant flight-control system | ||||
| Engine configuration | Single- or twin-engine, selected by the risk profile of the route | ||||
| Obstacle avoidance | Multi-modal sensing | ||||
| Autonomy | AI-assisted flight control and navigation | ||||
| Fuel & Propulsion Roadmap | |||||
| Current fuel | Gasoline | ||||
| 2028 | Diesel — raises energy density for long logistics and fire-suppression legs | ||||
| 2030 | Hydrogen blend, then pure hydrogen | ||||
| Mission Configurations | |||||
| Cargo | Standard cargo bay; cold-chain cargo module | ||||
| Lifting | Industrial lifting platform for sling loads | ||||
| Public safety | Emergency response variant | ||||
| Ground Ecosystem | |||||
| Infrastructure | Smart vertiports and refuelling stations | ||||
| Fleet | Cloud-based fleet management and dispatch | ||||
| Support | Full-lifecycle maintenance programme | ||||
| Supplied With The Technical Brief | |||||
| On request | Maximum take-off weight, airframe dimensions, rotor diameter, endurance at rated payload, fuel capacity, wind-resistance rating, control-link range and positioning accuracy. We go through these on a call so the figures match the mission. | ||||
