DESCRIPTION:
Two-cylinder, two-stroke boxer engine, air cooling, electric fuel oil injection system, suitable for industrial use.
TECHNICAL DATA:
Electric Fuel Injection System
Power: 18 kw(24 hp) / 7500 rpm
Displacement: 274 cm3
Weight: 7.0 kg
Fuel: 90 RON (unleaded) / AVGAS 100 LL - oil mixture
1:25 for mineral oil or 1:50 for synthetic oil
Optional accessories:Electric starter,Shielded ignition leads,Exhaust stacks (stainless steel 150mm long, 2 needed),Generator 28V/1200W,Generator coupling kit (engine side),Certificate of Conformance / Test - run
USAGE:
UAV(Fixed wing,Helicopter,Multirotor and airship),Manned Aircraft.
OTHER INFORMATION:
We can also provide propellors,generators and other spares for all our engines.
L550EF
DESCRIPTION:
Four-cylinders,two-stroke boxer engine,air cooling,electric fuel injection system,suitable for industrial use.
TECHNICAL DATA:
Power: 53hp(39kw)@7500rpm
Displacement: 548 cm3
Weight: 15.0 kg
Fuel: 90 RON (unleaded) / AVGAS 100 LL - oil mixture
1:25 for mineral oil or 1:50 for synthetic oil
Optional accessories:Electric starter,Shielded ignition leads,Exhaust stacks (stainless steel 150mm long, 4 needed),Generator 28V/1200W,Generator coupling kit (engine side),Certificate of Conformance / Test - run
USAGE:
UAV(Fixed wing,Helicopter,Multirotor and airship),Manned Aircraft.
OTHER INFORMATION:
We can also provide propellors,generators and other spares for all our engines.
L550E
DESCRIPTION:
Four-cylinder,two-stroke boxer engine,air cooling,4 carburators,solid magneto ignition suitable for industrial use.
Displacement: 548 cm3
4 Carburators
Weight: 18.3 kg with solid magneto
Fuel: 90 RON (unleaded) / AVGAS 100 LL - oil mixture
1:25 for mineral oil or 1:50 for synthetic oil
Optional accessories:Electric starter,Shielded ignition leads,Exhaust stacks (stainless steel 150mm long, 4 needed),Generator 28V/1200W,Generator coupling kit (engine side),Certificate of Conformance / Test - run
USAGE:
UAV(Fixed wing,Helicopter,Multirotor and airship),Manned Aircraft.
OTHER INFORMATION:
We can also provide propellors,generators and other spares for all our engines.
Limbach Engine Genuine Parts,Limbach Engine Original Parts,Limbach Spare Parts
Shield Ignition Line
Generator
Starter
Starter Wheel
Fuel Pump
Fuel Filter
Air Filter
Carburator
Cushion Pad
Exhaust Pipe
Generator Shaft Coupling
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.
DESCRIPTIONï
Four cylinders,horizontally opposed engine,aircooled,single magneto ignation,wet sump pressure lubrication
FEATURERSï
1.The ratio of power weight is higher.
2.Extremely low failure rate.
3.Turbo charger,full take off power up to 3500 meters.
TECHNICAL DATA:
Maximum Power 64 kW/87 HP at 3200 rpm
Displacement 2424 cm3 / 147.91 cub. in.
Compression ratio 8.5:1
Two carburetors
Fuel min. octane 98 RON (Unleaded) / AVGAS 100 LL
Dry weight 82 kg, plus accessories
Fuel consumption 14L/hour
APPLICATION:
Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship.
OTHER INFORMATION:
We can provide propellers, generators(for UAV), start-generators and other accessories.
Product Featureï
1,Designed for unmanned aerial vehicle (uav)
2,The ratio of power weight is higher
3,Extremely low failure rate
Product Specificationï
Power: 16 kW / 7200 rpm
Displacement: 274 cm3
Weight: 7.8 kg with magneto ignition
Fuel: 90 RON (unleaded) / AVGAS 100 LL - oil mixture
1:25 for mineral oil or 1:50 for synthetic oil
Optional accessories:Electric starter,Shielded ignition leads,Exhaust stacks (stainless steel 150mm long, 2 needed),Generator 28V/1200W2,Generator coupling kit (engine side),Certificate of Conformance / Test - run
Application:
Remote control airship,fix wing plane,helicopter,sailship etc.
Other Information:
We can also provide propellors for L275E engine,such as 27*20,28*20,34*10,34*12,also we can provide generator and other accessories.
DESCRIPTION
Four cylinders,horizontally opposed engine,aircooled,single magneto ignation,wet sump pressure lubrication
FEATURERS
1.The ratio of power weight is higher.
2.Extremely low failure rate.
TECHNICAL DATA:
Maximum Power 44 kW/60 HP at 3600 rpm
Displacement 1680 cm3 / 102.52 cub. in
Compression ratio 8:1
Two carburetors
Fuel min. octane 98 RON (Unleaded) / AVGAS 100 LL
Dry weight 73 kg, plus accessories
Fuel consumption 10L/hour
APPLICATION:
Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship.
OTHER INFORMATION:
We can provide propellers, generators(for UAV), start-generators and other accessories.
DESCRIPTION
Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual ignition system, 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 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.
APPLICATION:
Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship.
OTHER INFORMATION:
We can provide propellers, generators(for UAV), start-generators and other accessories.
DESCRIPTIONï
Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual ignition system, automatic altitude compensation, wet sump pressure lubrication
FEATURERSï
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.
DESCRIPTIONï¼?
Four cylinders,horizontally opposed engine,aircooled,single magneto ignation,wet sump pressure lubrication
FEATURERSï¼?
1.The ratio of power weight is higher.
2.Extremely low failure rate.
3.Turbo charger,full take off power up to 3500 meters.
TECHNICAL DATA:
Maximum Power 64 kW/87 HP at 3200 rpm
Displacement 2424 cm3 / 147.91 cub. in.
Compression ratio 8.5:1
Two carburetors
Fuel min. octane 98 RON (Unleaded) / AVGAS 100 LL
Dry weight 82 kg, plus accessories
Fuel consumption 14L/hour
APPLICATION:
Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship.
OTHER INFORMATION:
We can provide propellers, generators(for UAV), start-generators and other accessories.
