C145HT-Ⅰ Engine

Übersicht

Product Description of C145HT- Ⅰ engine C145HT-Ⅰ 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- Ⅰ 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 Dimension: 750mm 580mm 550mm Maximum power: 105/5800kW/rpm Maximum continuous power: 95/5500kW/rpm Power to weight ratio: 1.31kW/kg Starting method: Electric start

Technische Daten

Wichtige technische Daten: High performance Maximum take-off power up to 105kW, maximum continuous power 95kW., High reliability target TBO time 2000h., 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, Applications of C145HT-I engine 700kg~1600kg fixed wing UAV, etc..

Technische Daten

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