Versatile and Efficient, The Advanced Design of the Limbach Engine L550EF
The Limbach Engine L550EF is a compact, high-performance, two-cycle engine designed for UAVs and light aircraft applications. This UAV Engine is equipped with an electronic engine management system and automatic altitude compensation, the L550EF delivers consistent power and efficiency at various altitudes, making it an excellent choice for demanding aviation applications.ย
Key Specifications:
Power Output: 50 HP at 7000 RPM, providing reliable, high-performance power for diverse UAV and light aircraft applications
Bore and Stroke: 66 mm (2.60 in) bore and 40 mm (1.57 in) stroke for a balanced performance
Displacement: 548 cmยณ (33.44 cubic inches) to deliver a powerful thrust-to-weight ratio
Weight: Lightweight at 15 kg, maximizing aircraft agility and endurance
Crankcase: Durable, die-cast aluminum
Crankshaft: Seven-piece assembled design for reliable, long-term performance
Pistons: Casted aluminum alloy for efficient, lightweight operation
Cylinders: Cast aluminum with silicone carbide-coated barrel, enhancing wear resistance
Timing: ECU-controlled variable timing for optimized performance across varying RPM and altitude
Engine Management System: Computer-controlled 12V system with automatic altitude compensation
Fuel Compatibility: Runs on 90-octane gasoline, mixed with synthetic two-cycle oil at a 50:1 ratio
Starter (Optional): 12V starter available for easy ignition
Generator (Optional): 12V or 14V generator available for additional power needs
The Limbach L550EFโs advanced electronic management and altitude compensation provide seamless operation in changing environments. This engine is particularly suited for UAV operators and aviators seeking a lightweight, powerful engine with modern control features and consistent performance.
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Specifications
Specifications of Limbach Engine L550EF
Performance
50 HP at 7000 rpm
Bore
66 mm / 2.60 inch
Stroke
40 mm / 1.57 inch
Displacement
548 cm3 (33.44 cu. inches)
Weight
15 kg
Crankcase
Aluminium, die casted
Crankshaft
seven piece assembled
Pistons
casted aluminum alloy
Cylinders
Casted aluminum, silicone carbide coated barrel
Timing
variable (ECU-controlled)
Engine management system
12V, computer controlled
Altitude compensation
Automatic via ECU
Fuel
90 octane (regular) gasoline, mixed with synthetic two-cycle oil to the ratio of 50:1
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