Limbach L 2400 DT/ET Engine – turbocharged | 96kW (130HP) at 3000rpm | Liquid Cooled Cylinderheads
Description
Versatile and Efficient, The Advanced Design of the Limbach L 2400 DT/ET Engine – turbocharged
The Limbach L 2400 DT/ET is a high-performance, four-cylinder, horizontally opposed engine featuring liquid-cooled cylinder heads, electronic fuel injection, and automatic altitude compensation. Designed for UAVs and light aircraft, it offers smooth and powerful performance with efficient fuel consumption. This UAV Engine model includes dual ignition, enhancing reliability and performance in demanding conditions.
Key Specifications:
- Maximum Power: 96 kW (130 HP) at 3000 RPM, providing robust performance for various applications
- Engine Type: Four-cylinder, horizontally opposed, with liquid-cooled cylinder heads, wet sump pressure lubrication, and electronic engine management
- Bore and Stroke: 97 mm (3.82 in) bore and 82 mm (3.23 in) stroke
- Displacement: 2424 cm³ (147.91 cubic inches)
- Compression Ratio: 8:1 for a balanced combination of power and fuel efficiency
- Ignition System: Electronic engine management with variable, memory-mapped firing point (dual ignition on DT model)
- Spark Plugs: NGK DCPR 7 E with 0.7 mm electrode gap
- Firing Order: 1 – 3 – 2 – 4, providing balanced operation and reduced vibration
- Fuel Injection: 4 x Weber injectors for precise fuel management
- Fuel Requirements: 98 RON unleaded gasoline or AVGAS 100 LL
- Fuel Pump: Dual electric fuel pumps at 2.5 bar each
- Starter: 12V, 1.0 kW with solenoid for reliable starting
- Generator: 14V, 55A to support electrical requirements
- Oil System: Maximum oil pressure of 7 bar, minimum 1 bar at 2500 RPM, with a 3.5-liter oil capacity
- Cooling System: Max coolant temperature of 110°C, with an approximate 3-liter coolant capacity
- Propeller Drive: Direct, anti-clockwise rotation, suitable for variable pitch propellers
- Dry Weight: 86 kg (excluding accessories)
- Fuel Consumption: 255 g/kWh at Wide Open Throttle (WOT) and 240 g/kWh at part throttle for efficient fuel use
The L2400 DT/ET engine’s combination of liquid cooling, advanced electronic controls, and dual ignition (on DT) make it a powerful and efficient choice for high-altitude and demanding aerial applications, with reliable performance and flexibility to meet diverse operational needs.
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Specifications
Specifications of Limbach Engine L 2400 DT/ET
| Maximum Power | 96 kW / 130 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 – 55 A |
| Oil pressure | max. 7 bar; min. 1 bar at 2500 rpm |
| Oil temperature | max. 120 °C; min. 50 °C |
| Oil capacity | 3.5 Itrs |
| Coolant temperature | max. 110 °C |
| 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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