Limbach Engine L2400DX-turbocharged | 118kW (160HP) at 3000rpm | Four Cylinder, Liquid Cooled
Description
Versatile and Efficient, The Advanced Design of the Limbach Engine L2400DX
The Limbach Engine L2400DX ย is a powerful and efficient turbocharged engine, designed for high-performance UAV and aircraft applications requiring reliable power at high altitudes. With advanced features such as electronic fuel injection, automatic altitude compensation, and liquid-cooled cylinder heads, this UAV Engine ensures optimal performance across varying environments.
Key Specifications:
- Maximum Power: 118 kW (160 HP) at 3000 RPM for high-performance applications
- Engine Type: Four-cylinder, horizontally opposed, with liquid-cooled cylinder heads, turbocharging, and wet sump pressure lubrication
- Bore and Stroke: 97 mm (3.82 in) bore and 82 mm (3.23 in) stroke
- Displacement: 2424 cmยณ (147.91 cubic inches) for ample power output
- Compression Ratio: 8:1 for efficient power and fuel use
- Ignition System: Electronic engine management with variable, memory-mapped firing point
- Spark Plugs: NGK DCPR 7 E with a 0.7 mm electrode gap
- Firing Order: 1 – 3 – 2 – 4, ensuring balanced firing and reduced vibration
- Fuel Injection: Equipped with 4 x Weber injectors for precise fuel management
- Fuel Requirements: Compatible with 98 RON unleaded gasoline or AVGAS 100 LL for versatile fueling options
- Fuel Pumps: Dual electric fuel pumps at 2.5 bar each for consistent fuel supply
- Starter: 12V, 1.0 kW starter with solenoid for reliable starts
- Generator: 14V, available in 33A or 55A options for additional electrical requirements
- Oil System: Maximum oil pressure of 7 bar, minimum of 1 bar at 2500 RPM, with a 3.5-liter oil capacity
- Cooling System: Max coolant temperature of 110ยฐC, with a capacity of approximately 3 liters
- Propeller Drive: Direct, anti-clockwise rotation with a hub designed for variable pitch propellers
- Dry Weight: 86 kg (excluding accessories), providing a balance of power and portability
- Fuel Consumption: 255 g/kWh at Wide Open Throttle (WOT) and 240 g/kWh at part throttle for efficient fuel use
With its turbocharging and dual ignition (DT) options, the L2400DX offers enhanced altitude performance, making it ideal for aviation enthusiasts and commercial operators looking for reliable, high-output engines with modern electronic control and efficient fuel use.
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Specifications
Specifications of Limbach Engine L2400DX turbocharged
| Maximum Power | 118 kW / 160 HP at 3000 rpm |
| Bore | 97 mm / 3.82 inch |
| Stroke | 82 mm / 3.23 inch |
| Displacement | 2424 cm3 / 147.91 cub. in. |
| Compression ratio | 8 : 1 |
| Ignition | Electronic engine management |
| Spark plugs | NGK DCPR 7 E |
| Electrode spacing | 0.7 mm |
| Firing Order | 1 – 3 – 2 – 4 |
| Firing point | variable, memory mapped |
| Injectors | 4 x Weber |
| Fuel min. octane | 98 RON (Unleaded) / AVGAS 100 LL |
| Air cleaner | LIMBACH |
| Fuel pump | 2 x electric 2.5 bar |
| Starter with solenoid | 12 V – 1.0 kW |
| Generator | 14 V – 33 / 55 A |
| Oil pressure | max. 7 bar; min. 1 bar at 2500 rpm |
| Oil capacity | 3.5 Itrs |
| Coolant temperature | max. 110 ยฐC |
| Coolant capacity | approx. 3 ltrs |
| Tachometer drive | electric signal |
| Propeller drive | direct, anti-clockwise |
| Propeller hub | for variable pitch propeller |
| Dry weight | 86 kg, plus accessories |
| Fuel consumption | 255 g/kWh at WOT 240 g/kWh at part throttle |
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