Turbine Electric Engine with Hybrid Propulsion System - High Efficiency, Low Operating Costs, and STOL Capability
Product Details
| Power Output: | 400-1300kw | Overall Pressure Ratio: | 8 |
|---|---|---|---|
| Turbine Inlet Temperature(℃): | 1000 | Thrust-Specific Fuel Consumption(kg/kW/h): | 0.44 |
| Weight(kg): | 120 | Dimensions(Length×Width ×Height)mm: | 1050*520*480 |
| Rated Speed(rpm) 57000: | 57000 | Power Output(kW): | Maximum Continuous 300,Peak 350 |
| Pressure Ratio: | 8 | Inlet Temperature: | 1000℃ |
| Fuel Consumption: | 0.44 Kg/kW/h | Weight: | 120 Kg |
| Dimensions: | 1050×520×480 Mm | Rated Speed: | 57000 Rpm |
| Max Power: | 350 KW | Range: | 1000 Km |
Product Description

Advanced hybrid propulsion system based on a turboshaft/turboprop engine core, delivering output power of 300-1000 kW
- High Efficiency and Long Lifespan: The engine operates at the optimal operating point, resulting in high efficiency and extended service life
- Safety: Supports distributed power installation, providing higher redundancy and enhanced safety
- Long Range and High Speed: Range capability up to 1000 km, effectively overcoming range anxiety associated with electric power systems
- Low Operating Costs: Based on the engine's higher Time Between Overhaul (TBO) and extended lifespan, maintenance costs are significantly reduced over the entire lifecycle
- Short Takeoff and Landing (STOL): Utilizes peak power of the electric propulsion system during takeoff and landing, enabling operations on extremely short runways and significantly reducing airport facility requirements
- Conventional Takeoff and Landing (CTOL)
- Short Takeoff and Landing (STOL)
- Vertical Takeoff and Landing (VTOL)
Product Highlights
Hybrid turbine electric engine (300-1000 kW) with high efficiency, 1000km range, low operating costs, and STOL capability. Ideal for CTOL/STOL/VTOL applications with superior safety and lifecycle savings.
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