Heavy Fuel Aircraft Piston Engine

• Customization: Available
• Transport Package: Box
• Origin: China
• Model NO.: Engine

Product Description

Product Description

 

 Heavy Fuel Aircraft piston Engine

 The self-developed and produced DLE120HD two-stroke water-cooled drone engine adopts water-cooling device with special design, and the DLE engine is characterized by light weight, high power, low temperature and long life. The DLE engines water temperature does not exceed 80C° can effectively guarantee the continuous high power output of the engine. Eliminate the air-cooled engine due to high temperatures resulting in short life, unstable output power and other issues, the engine power of 7.2 kilowatts, the entire generator system using automatic control with the battery pack, composed of oil and electricity hybrid closed-loop control system. And with the self-developed DLE120MA plant protection UAV, the take-off weight can reach 53KG, and the operating load can reach 20kg, which breaks through the unprecedented large load and high efficiency performance. At the same time, DLE has also launched the 70MU UAV with long flight time, which can stay in the air for up to 6 hours, bringing a new concept and change in the field of unmanned aerial vehicles.
 
  Over the years, DLE Engine China has always been adhering to the conscientious and responsible, customer first purpose, is committed to the highest performance and cost-effective engine into the aviation, UAV, water sports and other areas of the market and to promote it, and we hope that through our efforts to contribute to the powerful China's aviation and UAV plant protection business a modest effort.
 

 

Product Description of C145HT-engine
C145HT- engine is a maximum 145hp aero-piston engine developed by Zongshen AeroDynamics, the engine form is four-stroke four-cylinder horizontally opposed, the maximum take-off altitude of this engine is 5000m, the critical pressurization altitude is 6000m, and the maximum use altitude is 8000m. Its target TBO time is 2000h, with high performance, high power-to-weight ratio, high reliability, and good high-altitude adaptability. Its target TBO time is 2000h, with high performance, high power-to-weight ratio, high reliability and good adaptability at high altitude, it is mainly used in medium and large fixed-wing, helicopter and rotorcraft.

Customized development at the request of customer requirements 

Product Advantages of C145HT- engine
High performance: Maximum take-off power up to 105kW, maximum continuous power 95kW.
High reliability: target TBO time 2000h.
Convenient and efficient after-sales support: 24h service response system, providing specialized product maintenance, repair services and training, technical support services.
High power-to-weight ratio: adopting the lightweight design concept based on reliability, applying new materials and new technology, the net weight of the whole machine is lower than 80kg, and the power-to-weight ratio reaches 1.31kW/kg.
Good high-altitude adaptability: Equipped with exhaust gas turbocharger, the maximum take-off altitude can reach 5000m, the critical pressurization altitude can reach 6000m, and the maximum use altitude can reach 8000m.

Technical Parameters of C145HT-I engine
    Engine type: four-stroke four-cylinder horizontally opposed
    Displacement: 1417ml
    Dimension: 750mm×580mm×550mm
    Net weight: 80kg
    Maximum power: 105/5800kW/rpm
    Maximum continuous power: 95/5500kW/rpm
    Power to weight ratio: 1.31kW/kg
    Compression ratio: 9.8:1
    Starting method: Electric start
    Ignition: Dual capacitor ignition
    Fuel supply: Carburetor
    Fuel Type: No.95 gasoline
    Supercharging method: Exhaust gas turbocharging    Exhaust gas turbocharging

Limbach L550E Specifications 
Type: Four cylinder, two stroke aircraft engine
Bore: 66 mm (2.60 in)
Stroke: 40 mm (1.57 in)
Displacement: 548 cc (33.4 cu in)
Length: 300 mm (11.8 in)
Width: 410 mm (16.1 in)
Height: 301 mm (11.9 in)
Dry weight: 16 kg (35 lb)
Components
Fuel type: 90 RON octane unleaded petrol or 100 LL Avgas
Oil system: oil mixture lubrication, 25:1 fuel to oil ratio for mineral oil, 50:1 for synthetic oil
Cooling system: air
Performance
Power output: 37 kW (50 hp)