Quality Aero Turbogenerator Engine with Extreme Power Density Lightweight Integration and High-Altitude Adaptability for UAVs and eVTOL factory
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Quality Aero Turbogenerator Engine with Extreme Power Density Lightweight Integration and High-Altitude Adaptability for UAVs and eVTOL factory
Quality Aero Turbogenerator Engine with Extreme Power Density Lightweight Integration and High-Altitude Adaptability for UAVs and eVTOL factory
Quality Aero Turbogenerator Engine with Extreme Power Density Lightweight Integration and High-Altitude Adaptability for UAVs and eVTOL factory
Quality Aero Turbogenerator Engine with Extreme Power Density Lightweight Integration and High-Altitude Adaptability for UAVs and eVTOL factory
Quality Aero Turbogenerator Engine with Extreme Power Density Lightweight Integration and High-Altitude Adaptability for UAVs and eVTOL factory
Quality Aero Turbogenerator Engine with Extreme Power Density Lightweight Integration and High-Altitude Adaptability for UAVs and eVTOL factory
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Aero Turbogenerator Engine with Extreme Power Density Lightweight Integration and High-Altitude Adaptability for UAVs and eVTOL

Product Details


Total Engine Weight: ≤ 60 Kg (WD-200), ≤ 80 Kg (WD-300), ≤ 120 Kg (WD-500) Overall Dimensions: 1000*400*600 Mm (WD-200), 1200*500*750 Mm (WD-300), 1500*600*900 Mm (WD-500)
Rated Power: 200 KW (WD-200), 300 KW (WD-300), 500 KW (WD-500) Peak Power: 240 KW (WD-200), 350 KW (WD-300), 550 KW (WD-500)
Power-to-Weight Ratio: ≥ 4.0 KW/kg (WD-200), ≥ 4.38 KW/kg (WD-300), ≥ 4.58 KW/kg (WD-500) Output Voltage Range: 800 VDC
Overall Efficiency: > 85% (WD-200), > 88% (WD-300), > 89% (WD-500) Specific Fuel Consumption: 0.48 Kg/(kW·h) (WD-200), 0.45 Kg/(kW·h) (WD-300), 0.4 Kg/(kW·h) (WD-500)
Core Engine Speed: 54000–58000 Rpm (WD-200), 52000–56000 Rpm (WD-300), 44000–48000 Rpm (WD-500) Operating Temperature Range: -40 ~ 60 ℃
Maximum Flight Altitude: 8000 M (WD-200, WD-300), 10000 M (WD-500)

Product Description

Aero Turbogenerator Engine with Extreme Power Density & Lightweight Integration
Product Definition

An Aero Turbogenerator Engine is a high-power gas turbine-based range-extending power system specially developed for low-altitude aircraft, unmanned aerial vehicles (UAVs), and electric vertical take-off and landing (eVTOL) platforms.

It integrates a high-speed gas turbine core engine with an ultra-high-efficiency synchronous generator in a compact series layout. Unlike traditional turbojet engines that produce thrust directly, the turbogenerator converts fuel energy into high-quality continuous electric power to supply propulsion motors, airborne equipment, and battery charging for hybrid-electric aircraft.

Core Technical Advantages
  • Extreme Power Density & Lightweight Integration: Advanced turbine core and high-speed generator integrated structure provides extremely high power output within limited volume and weight.
  • Dramatically Extended Endurance & Payload Capacity: Compared with pure lithium battery electric propulsion of the same weight, increases flight range up to 6 times and improves payload capacity up to 3 times.
  • High-Altitude & Full-Environment Adaptability: Stable and reliable power generation at high altitude, low temperature, and low air density environments.
  • Intelligent Hybrid Power Support: Provides stable continuous power for AI autonomous flight systems, flight control units, sensors, and heavy-duty propulsion units.
  • High Reliability & Industrial-Grade Durability: Mature gas turbine architecture with fewer vibrating moving parts and advanced thermal management design.
  • Wide Application Compatibility: Applicable to fixed-wing UAVs, hybrid-wing aircraft, helicopters, and multi-rotor eVTOLs for range extension, payload enhancement, and full-aircraft power supply.
Industry Differentiation

Turbojet Engine: Produces jet thrust for high-speed flight

Turbogenerator Engine (Our Product): Produces large continuous electric power for hybrid-electric long-endurance flight

This core difference makes our aero turbogenerator the ideal next-generation power solution for low-altitude economy and long-endurance unmanned aviation.

Product Series Overview

The WD-200, WD-300 and WD-500 aero turbogenerator engines are advanced aviation power units independently developed by our company. Tailored for civil aircraft in the low-altitude economy, they fill the domestic market gap for 200 kW, 300 kW and 500 kW aero turbogenerator engines.

These products adopt high-performance general core engines self-developed by Star Aero Engine. They feature an innovatively designed series power architecture combining aero-engine and ultra-high-speed generator. Widely applicable to fixed-wing, hybrid-wing, helicopter, eVTOL and other medium-to-large manned and unmanned aircraft.

Technical Parameters
Basic Parameters
Parameter Item Unit WD-200 Aero Turbogenerator Engine WD-300 Aero Turbogenerator Engine WD-500 Aero Turbogenerator Engine
Total Engine Weight kg ≤ 60 ≤ 80 ≤ 120
Overall Dimensions mm 1000*400*600 1200*500*750 1500*600*900
Rated Power kW 200 300 500
Peak Power kW 240 350 550 (5 minutes)
Power Performance
Parameter Item Unit WD-200 WD-300 WD-500
Power-to-Weight Ratio kW/kg ≥ 4.0 ≥ 4.38 ≥ 4.58
Output Voltage Range VDC 800 VDC 800 VDC 800 VDC
Overall Efficiency (at rated condition) % > 85 > 88 > 89
Efficiency & Fuel Consumption
Parameter Item Unit WD-200 WD-300 WD-500
Specific Fuel Consumption kg/(kW·h) 0.48 0.45 0.4
Endurance @ 50% Load h 8 10 12
Operating Parameters
Parameter Item Unit WD-200 WD-300 WD-500
Core Engine Speed Range rpm 54000–58000 52000–56000 44000–48000
Cooling Method - Lubricant liquid cooling + auxiliary air cooling Lubricant liquid cooling + auxiliary air cooling Lubricant liquid cooling + auxiliary air cooling
Start-up Time s < 30 (One-touch electric start) < 30 (One-touch electric start) < 30 (One-touch electric start)
Noise Level @ 10m dB(A) 95 98 102
Operating Temperature Range -40 ~ 60 -40 ~ 60 -40 ~ 60
Environment & Reliability
Parameter Item Unit WD-200 WD-300 WD-500
Maximum Flight Altitude m 8000 8000 10000
MTBF (Mean Time Between Failures) h > 600 > 600 > 1000
Maximum Take-off Weight Ton 2–4 4–6 6–10
Typical Application Scenarios
Model Application Scenarios
WD-200 Short & medium haul logistics / Inspection patrol
WD-300 Regional logistics / Emergency rescue
WD-500 Heavy cargo transport / Long-endurance missions

Product Highlights

Aero turbogenerator engines with extreme power density (4.0-4.58 kW/kg) extend flight range 6x and payload 3x vs pure electric. High-altitude capable, 8000-10000m operation, 600-1000h MTBF. Ideal for UAVs/eVTOLs in logistics, inspection, and rescue.

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