145 Horsepower Military Aero Engine ZS145HT

Vue d'ensemble

Case：AR500C Altitude unmanned helicopter ZS aero engine C145HT ased on the proven concept of the ZS aero engine C145, Four-stroke, four cylinders, horizontally opposed turbocharging, air intake system with inter-cooler, Dual constant depression carburetors. the takeoff altitude can be up to 5000 meters, the critical pressurization altitude can be up to 6000 meters, and the maximum operating altitude can be up to 10000 meters. The PA powertrain system of C145HT can provide OEM with a power system integration solution based on "C145 + propeller + cooling system + engine control"，The best power and high reliability. Customized development can be carriedout according to customer requirements,such as integrated matching of high-powergenerators. 700kg-1600kg fixed wing UAV, 600kg UAVHelicopters and rotorcraft, etc. Max power: 105/5800 kW/rpm Max Continuous power: 90/5500 kW/rpm Propeller speed reduction gearbox Min. 95# RON gasoline or Avgas SFC at cruise: 285 g/kW.h

Spécifications techniques

Caractéristiques principales : EIGHT KG, Engine with propeller speed reduction gearbox i = 2.43 80, Overload clutch 1.6, Engine suspension frame 2.3, 106.6 kW 145 hp / 5800 rpm, 189 Nm 4900 rpm, MAX RPM 5800 rpm, BORE STROKE, 86 mm 61.0 mm, DISPLACEMENT FUEL, 1417 cm ³ Min. RON 95 Mogas/ 100LL Avgas, Case AR500C Altitude unmanned helicopter, Dry weight 80 kg, Max power 105/5800 kW/rpm, Max Continuous power 90/5500 kW/rpm, SFC at cruise 285 g/kW. h.

Spécifications techniques

Aéronefs compatibles

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Documentation

Pièces détachées compatibles

145 Horsepower Military Aero Engine ZS145HT

Case：AR500C Altitude unmanned helicopter

Commande minimum

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