Quality Multi-Fuel Piston Aero Engine with High Power Density and Long Service Life for UAVs and eVTOL factory
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Quality Multi-Fuel Piston Aero Engine with High Power Density and Long Service Life for UAVs and eVTOL factory
Quality Multi-Fuel Piston Aero Engine with High Power Density and Long Service Life for UAVs and eVTOL factory
Quality Multi-Fuel Piston Aero Engine with High Power Density and Long Service Life for UAVs and eVTOL factory
Quality Multi-Fuel Piston Aero Engine with High Power Density and Long Service Life for UAVs and eVTOL factory
Quality Multi-Fuel Piston Aero Engine with High Power Density and Long Service Life for UAVs and eVTOL factory
Quality Multi-Fuel Piston Aero Engine with High Power Density and Long Service Life for UAVs and eVTOL factory
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Multi-Fuel Piston Aero Engine with High Power Density and Long Service Life for UAVs and eVTOL

Model Number: CU170,CU200,CUV3000,CUV4500,CUV6000,CU6000
Place of Origin: China
Certification: CAAC
Minimum Order Quantity: 12
Supply Ability: 1000

Product Details


Power Range: 10 KW To 350 KW Fuel Consumption: 15% -20% Lower
Flight Duration: Up To 12 Hours Operating Altitude: 6000 M To 8000 M
TBO: 300 H To 2000 H Displacement: 170 Ml To 6.0 L
Rated Power: 10 KW To 400 KW Engine Weight: ≤ 7.2 Kg To ≤ 440 Kg
Specific Fuel Consumption: ≤ 200 G/(kW*h) To ≤ 330 G/(kW*h) Cooling Method: Air Cooling, Liquid Cooling

Product Description

Multi-Fuel Piston Aero Engine Heavy-Duty Piston Aviation Power 2-4-6-8 Cylinder Engine
Technical Overview & Performance Features

This is our new style product line with advanced lightweight piston aero engines specially developed for low-altitude economy scenarios, including large UAVs, cargo drones, inspection platforms, and manned eVTOL aircraft. Covering a power range from 10 kW to 350 kW, our aviation power systems deliver high reliability, long endurance, and excellent environmental adaptability for commercial and industrial low-altitude aviation missions.

  • Wide Power Coverage & Modular Platform Design - The product portfolio covers micro, medium, and heavy power segments, including horizontally opposed twin-cylinder engines and turbocharged V6/V8 modular engines. It perfectly matches multi-rotor, fixed-wing, and vertical take-off and landing aircraft, supporting missions from small patrol UAVs to large heavy-cargo and long-endurance aerial platforms.
  • Outstanding Fuel Efficiency & Ultra-Long Endurance - Equipped with self-developed ECU electronic fuel injection and precision fuel supply control, the engines achieve 15% -20% lower fuel consumption than conventional aero piston engines. Optimized combustion strategy enables continuous stable output, supporting up to 12 hours of flight duration and ultra-long-distance cruising for logistics and inspection missions.
  • Multi-Fuel Compatibility & Strong Environmental Adaptability - Jumeirah aero engines support diversified fuel options, including aviation kerosene, diesel, and unleaded gasoline, greatly improving field supply convenience and operational flexibility. The power system maintains stable performance under extreme conditions of high altitude, low temperature, high humidity, and complex weather, adapting to all-region and all-weather low-altitude operations.
  • High Power Density & Lightweight Structure - Adopting advanced lightweight materials and optimized structural layout, the series features compact size and high power-to-weight ratio, surpassing most domestic peer products. The balanced horizontal opposed and V-type cylinder design effectively reduces vibration and noise, improving flight stability and passenger comfort for manned eVTOL applications.
  • High Reliability & Long Service Life - Derived from Jumeirah's mature industrial-grade power manufacturing system, the engines undergo ultra-long bench cycle verification with a TBO up to 300 hours and above. With standardized modular components, the series features low failure rates, easy maintenance, and mature supply chain support, significantly reducing operational and after-sales costs.
  • Intelligent Electronic Control & Strong Expandability - Supported by fully independent domestic ECU intelligent control technology, the system integrates real-time fault diagnosis, operational data monitoring, and redundant safety control functions. Standardized interfaces enable fast docking with flight control systems, battery management systems and hybrid range-extender architectures, facilitating intelligent and unmanned flight upgrades.
Typical Applications

Medium and large cargo UAVs, high-altitude plant protection drones, aerial survey & inspection aircraft, emergency rescue platforms, and 2-6 seat manned eVTOL low-altitude commuter aircraft.

CU170 & CU200 Engine Specifications
Item CU170 CU200
Applicable Fuel Aviation kerosene, diesel Aviation kerosene, diesel
Engine Type Horizontally Opposed, 2-Cylinder Horizontally Opposed, 2-Cylinder
Cooling Method Air Cooling Air Cooling
Fuel Supply Type Cylinder Direct Injection Cylinder Direct Injection
Displacement (ml) 170 200
Rated Power / Speed [kW/(r/min)] 10 / 7500 12 / 7500
Dry Weight of Engine (kg) ≤ 7.2 ≤ 8.5
Power-to-Weight Ratio (kW/kg) ≥ 1.38 ≥ 1.41
Cruise Specific Fuel Consumption [g/(kW*h)] ≤ 330 ≤ 330
Maximum Ceiling Altitude (m) 6000 6000
TBO (Time Between Overhauls) (h) ≥ 300 ≥ 300
CUV3000 & CUV4500 Engine Specifications
Item CUV3000 CUV4500
Applicable Fuel Diesel, Aviation Kerosene Diesel, Aviation Kerosene
Engine Type Inline 4-Cylinder V6 Cylinder
Displacement (L) 3.0 4.5
Intake Type Turbocharged Turbocharged
Cooling Method Liquid Cooling Liquid Cooling
Fuel Supply Type High-Pressure Common Rail EFI High-Pressure Common Rail EFI
Rated Power / Speed [kW/(r/min)] 140 / 2800 255 / 3000
Engine Dry Weight (kg) (Without Reduction Gearbox) ≤ 280 ≤ 380
Cruise Specific Fuel Consumption [g/(kW*h)] ≤ 205 ≤ 200
Maximum Ceiling Altitude (m) 6000 6000
TBO (Time Between Overhauls) (h) ≥ 2000 ≥ 2000
Core Term Explanation
  • High-Pressure Common Rail EFI: High-precision electronic fuel injection system, realizing precise fuel metering and low fuel consumption.
  • Turbocharged Intake: Effectively boosts intake efficiency, maintains stable power output at high altitude.
  • Liquid Cooling: Stable and efficient heat dissipation, suitable for long-time continuous full-load operation.
  • TBO: Time Between Overhauls, a core reliability index for aviation power equipment.
CUV6000 & CU6000 Engine Technical Parameters
Item CUV6000 CU6000
Applicable Fuel Diesel, Aviation Kerosene Aviation Kerosene, Diesel
Engine Type V8 Cylinder V12 Cylinder
Displacement (L) 6.0 6.0
Intake Type Turbocharged Turbocharged
Cooling Method Liquid Cooling Liquid Cooling
Fuel Supply Type High-Pressure Common Rail EFI High-Pressure Common Rail EFI
Rated Power / Speed [kW/(r/min)] 350 / 3000 400 / 4000
Engine Dry Weight (kg) ≤ 440 (Without Reduction Gearbox) ≤ 400
Power-to-Weight Ratio (kW/kg) -- ≥ 1.0
Cruise Specific Fuel Consumption [g/(kW*h)] ≤ 210 ≤ 215
Maximum Ceiling Altitude (m) 8000 8000
TBO (Time Between Overhauls) (h) ≥ 2000 ≥ 2000

Product Highlights

Heavy-duty piston aero engines (10-350kW) for UAVs & eVTOLs. Multi-fuel compatible with 15-20% lower fuel consumption, 300-2000h TBO, and superior high-altitude performance. Lightweight design ensures reliability for cargo, inspection & manned aircraft.

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