Limbach L2000 EB and L2400 EB Engine | Maximum HP (5 min) 87HP / 64kW / 3200rpm | Four Cylinder, Horizontally Opposed Air Cooled Engine

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Description

Versatile and Efficient, The Advanced Design of the Limbach L 2400 DT/ET Engine – turbocharged

The Limbach L2000 EB and L2400 EB engines are high-performance, four-cylinder, horizontally opposed, air-cooled engines designed for reliable power and efficiency in general aviation and UAV applications. With single magneto ignition, wet sump lubrication, and robust construction, these UAV Engineย provide steady power with low maintenance.

Engine Specifications
L2000 EB
  • Maximum Power (5 min): 80 HP (59 kW) at 3400 RPM
  • Continuous Power: 70 HP (51 kW) at 3000 RPM
  • Bore & Stroke: 90 mm (3.54 in) x 78.4 mm (3.09 in)
  • Displacement: 1994 cmยณ (121.68 cubic inches)
  • Compression Ratio: 8.4:1
  • Fuel Consumption: Approximately 12 liters per hour
  • Dry Weight: 76.5 kg
L2400 EB
  • Maximum Power (5 min): 87 HP (64 kW) at 3200 RPM
  • Continuous Power: 84.5 HP (62 kW) at 3000 RPM
  • Bore & Stroke: 97 mm (3.82 in) x 82 mm (3.23 in)
  • Displacement: 2424 cmยณ (147.91 cubic inches)
  • Compression Ratio: 8.5:1
  • Fuel Consumption: Approximately 14 liters per hour
  • Dry Weight: 82 kg
General Features
  • Ignition System: Slick 4330 magneto with LIMBACH harness
  • Spark Plugs: LIMBACH LB-N41.0
  • Firing Order: 1 – 3 – 2 – 4 with 30ยฐ BTDC firing point
  • Carburetion: 2 x Zenith 150 CD-3 carburetors
  • Fuel Requirements: 98 RON (unleaded) or AVGAS 100LL
  • Air Cleaner: 2 x LIMBACH
  • Fuel Pump: LIMBACH mechanical fuel pump
  • Starter: 12V, 1.1 kW with solenoid for reliable starting
  • Generator: 14V, available in 33A or 55A options
  • Oil System: Maximum oil pressure of 7 bar, minimum 1 bar at 2500 RPM, with a 3.5-liter oil capacity
  • Temperature Limits: Max oil temperature 120ยฐC, min 50ยฐC; max cylinder head temperature 250ยฐC
  • Propeller Drive: Direct, anti-clockwise with EB1 propeller hub for variable pitch propellers
  • Tachometer Drive: Mechanical
Both the L2000 EB and L2400 EB engines are versatile and suitable for various aircraft and UAV applications. With high power output and solid construction, these engines ensure reliable performance, while their air-cooled design reduces complexity and weight for operational efficiency.

 

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Limbach L2000 EB / L2400 EB โ€“ FAQ

1. What are the key technical specifications of these engines?
Both the L2000 EB and L2400 EB are four-cylinder, horizontally opposed, air-cooled gasoline engines built for UAVs and light aircraft.

  • L2000 EB: 80 HP (59 kW) @ 3400 RPM (max 5 min), 70 HP (51 kW) @ 3000 RPM (continuous), displacement 1994 cmยณ, compression 8.4:1, fuel use โ‰ˆ 12 L/h, dry weight 76.5 kg.

  • L2400 EB: 87 HP (64 kW) @ 3200 RPM (max 5 min), 84.5 HP (62 kW) @ 3000 RPM (continuous), displacement 2424 cmยณ, compression 8.5:1, fuel use โ‰ˆ 14 L/h, dry weight 82 kg.

2. What design and construction features are used?
Both engines feature aluminum alloy crankcases, forged crankshafts, and lightweight cylinder heads for strength and heat dissipation.
They employ wet-sump lubrication for stable oil supply and balanced crankshaft design for low vibration and long-term reliability.

3. What ignition and fuel systems do they use?
Each engine utilizes a Slick 4330 magneto ignition system with Limbachโ€™s proprietary spark-plug harness for dependable combustion.
They operate on AVGAS 100LL or MOGAS 95, using dual carburetors for uniform mixture and smooth power delivery across all engine speeds.

4. What performance benefits do the L2000 EB and L2400 EB provide?
These engines deliver high reliability, smooth operation, and efficient fuel consumption, ideal for long-endurance UAVs, aerial survey aircraft, and manned light platforms.
Their air-cooled design minimizes maintenance, while the magneto ignition provides power redundancy without requiring external electricity.

5. What are the available purchasing and payment options?
MotioNew provides these engines by quotation to account for configuration and export requirements.
Payments can be made through bank transfer, PayPal, or major credit cards, and bulk or OEM purchase agreements are available for UAV integrators and aerospace clients.

6. What documentation and compliance materials are provided?
Each engine includes technical manuals, installation and maintenance instructions, wiring diagrams, and performance data sheets.
Both models comply with civilian UAV export and aviation safety regulations and are approved for commercial and research applications only.
Use for military, warfare, or prohibited purposes is strictly forbidden. MotioNew provides technical assistance, spare parts, and after-sales support to ensure operational reliability.

Specifications

Specifications

Specifications of Limbach Engine Limbach L2000 EB and L2400 EB

L 2000 EB
Maximum HP (5 min)ย  80 hp / 59 kW / 3400 rpm
Continuous HPย  70 hp / 51 kW / 3000 rpm
Boreย  90 mm / 3.54 inch
Strokeย  78.4 mm / 3.09 inch
Displacementย 
1994 cm3 / 121.68 cub. in.
Compression ratioย  8.4 : 1
L 2400 EB
Maximum HP (5 min)ย  87 hp / 64 kW / 3200 rpm
Continous HPย  84.5 hp / 62 kW / 3000 rpm
Bore
97 mm / 3.82 inch
Strokeย  82 mm / 3.23 inch
Displacement
2424 cm3 / 147.91 cub. in.
Compression ratio
8.5 : 1
General Specifications
Ignition
Slick 4330
Harness
LIMBACH
Spark plugs
LIMBACH LB-N41.0
Firing Order
1 – 3 – 2 – 4
Firing point
30ยฐ BTDC
Carburetor
2 x ZE NITH 150 CD-3
Fuel min. octane
98 RON (Un lea ded) or AV GAS 100LL
Air cleaner
2 x LIMBACH
Fuel pump
LIMBACH
Starter with solenoid
12 V – 1.1 kW
Generator
14 V – 33 A or 14 V – 55 A
Oil pressure
max. 7 bar; min. 1 bar at 2500 rpm
Oil temperature
max. 120ยฐC; min. 50ยฐC
Oil capacity
3.5 ltrs
Cylinder head temp.
max. 250ยฐC
Tachometer drive
mechanical
Propeller drive
direct, anti-clockwise
Propeller hub
EB 1 for variable pitch
Dry weight approx.
76.5 kg L 2000 EB
82 kg L 2400 EB
Fuel consumption
should be individually established during flight tests, however, the aver age fuel consumption is approx.:
12 ltrs/hr L 2000 EB
14 ltrs/hr L 2400 EB

 

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Specification:

Engine Power

59kW

,

64kW

,

80HP

,

87HP

Engine Weight

76.5kg

,

82kg

Engine Displacement

1994cm3

,

2424cm3

Engine Bore

90mm

,

97mm

Engine Stroke

78.4mm

,

82mm