L2400DT
Limbach L2400DT Turbo Charger Avaiation Engine UAV Engine Manned Aircraft Engine Helicopter Engine Gyrocopter Engine 130HP
Product ID: Limbach L2400DT
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DESCRIPTION：
Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual ignition system,Turbo Charger,automatic altitude compensation, wet sump pressure lubrication
FEATURERS：
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.
TECHNICAL DATA:
Maximum Power 96 kW / 130 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
APPLICATION:
Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship.
Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual ignition system,Turbo Charger,automatic altitude compensation, wet sump pressure lubrication
FEATURERS：
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.
TECHNICAL DATA:
Maximum Power 96 kW / 130 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
APPLICATION:
Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship.
Main Products
Limbach Aircraft Engine,UAV Engine,Aviation Engine,Helicopter Engine