Combines Internal Combustion and Electric Drive for Extended Range and Adaptability
| Component | Size | Material | Temperature Range |
|---|---|---|---|
| Internal Combustion Section | Refer to turboprop or piston engines | High-temperature alloy, aluminum alloy | 100°C to 1700°C |
| Electric Section | Refer to electric motors | Carbon fiber, copper, aluminum alloy | -50°C to 150°C |
| Energy Management | Controller 300×200×100mm | Electronic components, aluminum alloy | -40°C to 85°C |
| Integrated Piping System | Diameter 10–50mm | Stainless steel, composite materials | -50°C to 500°C |
Applicable Engine Type:
Hybrid engines (range-extending UAVs, electric general aviation aircraft, future eVTOLs)
System Components
- Engine Module: (Piston/Small Turbine)
- Motor Module: (High Power Density Electric Motor)
- Hybrid Controller
- Energy Storage Battery Pack & Energy Management System
Features Overview
- Seamless Power Transition
- Significant Fuel Savings and Range Advantages
- Ideal for Long-Endurance UAVs and Multirotor Manned Aircraft
- Multi-mode Switching Logic Configurable Based on Mission Scenarios
Technical Support
- Flight Mission Scenario Simulation & Modeling
- System-Level Energy Efficiency Optimization
- High-Reliability Electric Drive Design & Validation
- Health Management System Based on Fault Modes
Client Application Examples
- Hybrid UAV Helicopter with Over 10-Hour Endurance
- Core Propulsion System Supplier for an eVTOL Project
| 部件 | 尺寸 | 材料 | 耐温范围 |
| 内燃部分 | 参照涡轴或活塞发动机 | 高温合金、铝合金 | 100°C 至 1700°C |
| 电动部分 | 参照电动发动机 | 碳纤维、铜、铝合金 | -50°C 至 150°C |
| 能量管理 | 控制器 300×200×100mm | 电子元件、铝合金 | -40°C 至 85°C |
| 综合管路系统 | 直径 10-50mm | 不锈钢、复合材料 | -50°C 至 500°C |
适用发动机类型：混动发动机（增程无人机、电动通航飞机、未来 eVTOL）
主标题：混合动力系统方案
副标题：内燃+电驱动融合，为飞行平台拓展续航与适应性
系统组成：
- 发动机模块（活塞/小型涡轮）
- 电机模块（高功率密度电动机）
- 混动控制器
- 储能电池包与能量调度系统
特性概述：
- 动力切换平滑
- 节油与续航优势显著
- 适用于长航时无人机、多旋翼载人飞行器
- 可按任务场景设置多模式切换逻辑
技术支持：
- 飞行任务场景模拟建模
- 系统级能效优化
- 高可靠性电驱设计与验证
- 基于故障模式的健康管理系统
客户应用示例：
- 某混动无人直升机可巡航10小时以上
- 某eVTOL项目核心推进系统供应商