115 Horsepower Military Aero Engine ZS115HT

Übersicht

ZS115HT is a 115 horsepower aviation piston engine. This engine is successfully installed in domestic multiple UAVs and rotorcrafts, it has completed the 8800 meter high altitude flight test, The maximum takeoff height of the engine is 5000 meters, the critical boost height is 7500 meters, and the maximum use height is 10000 meters,it offers more performance at high altitudes and the best power to weight ratio at 1.13kW/kg, Cylinder heads is liquid-cooled and cylinders is air-cooled, four-stroke, four cylinders, horizontally opposed turbocharged. Customized development can be carriedout according to customer requirements,such as integrated matching of high-powergenerators. 700kg-1200kg fixed wing UAV, 500kg UAVHelicopters and rotorcraft, etc. Max power: 84.5/5800 kW/rpm Max Continous power: 73.5/5500 kW/rpm External characteristic curve Height characteristic curve

Technische Daten

Wichtige technische Daten: WEIGHT KG, Engine with propeller speed reduction gearbox i = 2.43 84.5, Overload clutch 1.6, Engine suspension frame 2.3, 84.5 kW 124.6 hp / 5800 rpm, 140 Nm 4900 rpm, MAX RPM 5800 rpm, BORE STROKE, 79.5 mm 61.0 mm, DISPLACEMENT FUEL, 1211 cm³ Min. RON 95 Mogas/ 100LL Avgas, Dry weight 74.5 kg, Max power 84.5/5800 kW/rpm, Max Continous power 73.5/5500 kW/rpm.

Technische Daten

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