Limbach L2400DX Turbo Charger Avaiation Engine UAV Engine Manned Aircraft Engine

DESCRIPTION：

Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual ignition system, automatic altitude compensation, wet sump pressure lubrication

1.Liquid cooled cylinderheads, electronic fuel injection and dual ignition system. 2,The ratio of power weight is higher. 3.Extremely low failure rate. 4.Turbo charger,full take off power up to 3500 meters.

Maximum Power 118 kW / 160 HP at 3000 rpm Displacement 2424 cm3 / 147.91 cub. in. Compression ratio 8 : 1 Ignition Electronic engine management Fuel min. octane 98 RON (Unleaded) / AVGAS 100 LL Dry weight 86 kg, plus accessories Fuel consumption 255 g/kWh at WOT,240 g/kWh at part throttle.

Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship.

We can provide propellers, generators(for UAV), start-generators and other accessories.