DESCRIPTIONï¼
Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual ignition system, automatic altitude compensation, wet sump pressure lubrication
FEATURERSï¼
1.Liquid cooled cylinderheads, electronic fuel injection and dual ignition system. 2,The ratio of power weight is higher. 3.Extremely low failure rate.
TECHNICAL DATA:
Maximum Power 74 kW / 100 HP at 3000 rpm Displacement 2424 cm3 / 147.91 cub. in. Compression ratio 9.5 : 1 Ignition Electronic engine management Fuel min. octane 98 RON (Unleaded) / AVGAS 100 LL Dry weight 76 kg, plus accessories Fuel consumption 265 g/kWh at WOT,245 g/kWh at part throttle.
APPLICATION:
Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship.
OTHER INFORMATION:
We can provide propellers, generators(for UAV), start-generators and other accessories.