变模态飞行器Variable-Mode Vehicles
一套动力
两种飞行模态One vehicle,
two flight modes
火箭动力垂直起降,固定翼涡喷巡航 —— 同一架飞行器在两种模态之间转换。尾座式布局,起降不需要跑道。Rocket-powered vertical takeoff, fixed-wing turbojet cruise — one airframe transitions between the two. A tail-sitter layout means no runway is required.
第一阶段平台First Platform
200 kg 级变模态验证平台200 kg variable-mode demonstrator
配 6 kN 挤压式发动机,用于验证火箭动力垂直起降的总体构型、推力矢量姿态控制与模态转换算法,并同步预研测试系统。当量小、试验成本低,可以在短周期内多次飞行、快速迭代。Powered by a 6 kN pressure-fed engine, it validates the rocket-powered VTOL layout, thrust-vector attitude control and mode-transition algorithms while the test infrastructure is developed alongside. Small scale keeps test costs low, so it can fly often and iterate fast.
- 最大起飞重量Max takeoff mass
- 0.2t
- 巡航速度Cruise speed
- 500km/h
- 升限Service ceiling
- 5km
- 快速试验Fast test cadence 小当量、低成本,多次实验快速迭代。Small charge, low cost, many flights and quick iteration.
主力产品Flagship Product
10 吨级混合动力运输飞行器10-tonne hybrid-powered transport
面向高原、火场、海上、极地等特殊环境的大载重任务 —— 垂直起降、点对点直航,落地不需要跑道。Built for heavy-payload missions into hard places — plateaus, fire grounds, open water, polar terrain. Vertical takeoff, point-to-point direct routing, no runway at either end.
- 最大起飞重量Max takeoff mass
- 10t
- 巡航速度Cruise speed
- 800km/h
- 巡航高度Cruise altitude
- 5km
- 最大航程Max range
- 1000km
- 货舱容积Cargo volume
- 8.3m³
- 吨公里成本Cost per tonne-km
- 1–2¥
- 推力更强More thrust 高推重比动力:液氧甲烷推进、高室压设计。High thrust-to-weight propulsion: methalox, high chamber pressure.
参数对比Benchmark
与同级倾转旋翼飞行器对照Against a same-class tiltrotor
| 参数Parameter | 某倾转旋翼飞行器A tiltrotor aircraft | 本项目飞行器This project | 项目优势Where we gain |
|---|---|---|---|
| 最大起飞重量Max takeoff mass | 6 吨(2 吨运力)6 t (2 t payload) | 10 吨(1.5 吨运力)10 t (1.5 t payload) | 运载比成本是前者的 1/3Payload-cost ratio one third of the other |
| 巡航速度Cruise speed | 550 公里/小时550 km/h | 800 公里/小时800 km/h | 混合动力货运无人机在速度和载荷上具有明显优势A hybrid-powered freight UAV wins clearly on speed and load |
| 最大航程Max range | 4000 公里4000 km | 1000 公里1000 km | 面向 1000 公里以内的支线与应急任务Sized for regional and emergency missions inside 1000 km |
| 货舱容积Cargo volume | 7.6 立方米7.6 m³ | 8.3 立方米8.3 m³ | 货舱容积更大,更适合重型货物运输A bigger hold suits heavy freight better |
航程一项本项目并不占优 —— 10 吨级平台的设计任务是 1000 公里以内的支线直航与应急投送,不是洲际转场。Range is the one row we do not win. The 10-tonne platform is designed for direct regional runs and emergency delivery inside 1000 km, not for intercontinental ferry flights.
成本对比Cost Comparison
造价降 97%,吨公里成本降 66%97% off the airframe, 66% off the tonne-kilometre
口径:条形长度按数值等比绘制,区间值取中位(吨公里成本 3–4 元取 3.5,1–2 元取 1.5)。单机售价 5000 万元 → 150 万元,油耗运营成本 3–4 元/吨公里 → 1–2 元/吨公里。数据为公司内部设计指标与测算,非第三方实测结果。Basis: bar lengths are drawn to scale, with ranges taken at their midpoint (¥3–4 as 3.5, ¥1–2 as 1.5). Unit price falls from ¥50M to ¥1.5M; fuel and operating cost from ¥3–4 to ¥1–2 per tonne-kilometre. Figures are internal design targets and estimates, not third-party measurements.
技术架构Architecture
两台飞行器,同一套架构Two vehicles, one architecture
200 kg 级与 40 吨级共用一套动力、控制与平台架构 —— 验证机上跑通的东西,直接放大到运输机。The 200 kg demonstrator and the 40-tonne transport share one propulsion, control and platform stack, so what the demonstrator proves scales straight into the freighter.
- 动力系统Propulsion 液氧甲烷火箭发动机 · 深度节流与快速响应 · 多次点火、重复使用Methalox rocket engine · deep throttling with fast response · multi-start and reusable
- 控制系统Control 推力矢量控制(TVC) · 自适应飞行控制 · 自主导航与精准着陆Thrust vector control (TVC) · adaptive flight control · autonomous navigation and precision landing
- 飞行平台Platform 尾座式总体布局 · 高强轻量化结构 · 模块化可扩展平台Tail-sitter layout · high-strength lightweight structure · modular and extensible
-
01
更灵活More flexible
全域快速部署:尾座式起降、无需跑道、复杂环境适应。Rapid deployment anywhere: tail-sitter takeoff and landing, no runway, tolerant of hard environments.
-
02
更精准More precise
精准姿态控制:推力矢量、自主飞控、组合导航。Precise attitude control: thrust vectoring, autonomous flight control, integrated navigation.
-
03
成本更低Lower cost
低成本运营:重复使用、模块维护、快速周转。Low-cost operation: reuse, modular servicing, fast turnaround.