Limbach L2400
The Limbach L 2400 are a series of German piston aero-engines designed and built by Limbach Flugmotoren. It is a four-cylinder, four-stroke air-cooled flat piston engine typically between 93-130 hp (69.4-97 kW) power output.[1][2]
| Limbach L 2400 | |
|---|---|
| Type | Piston aircraft engine |
| National origin | Germany |
| Manufacturer | Limbach Flugmotoren |
| First run | c.1984 |
| Major applications | Stemme S10 |
Variants
- L 2400 DE3.X
- Dual ignition system. 90 hp (67 kW)[1]
- L 2400 DF
- Certified in March 2001, has an electronically controlled fuel injection and double ignition system. Tractor type engine with alternator in the front and starter in the back.[3]
- L 2400 DT
- Certified in September 2001, has an electronically controlled fuel injection and double ignition system. Tractor type engine with alternator in the back and starter in the back.[3]
- L 2400 EB
- Certified in June 1985, has a carburettor and magneto ignition system. Two carburettors in the back, alternator in the back and starter in the back. 87 hp (65 kW)[1][3]
- L 2400 EE
- Certified in July 1999, has a carbuettor and magneto ignition system. Two carburettors in the back, alternator in the front and starter in the front.[3]
- L 2400 EF
- Certified in February 1997, has an electronically controlled fuel injection and ignition system. Tractor type engine with alternator in the front and starter in the back.[3]
- L 2400 EFI
- Fully electronic fuel injection. 100 hp (75 kW)[1]
- L 2400 EO.X
- Single ignition system. 87 hp (65 kW)[1]
- L 2400 ET
- Certified in September 2001, has an electronically controlled fuel injection and ignition system. Tractor type engine with alternator in the back and starter in the back.[3]
Applications
Specifications (L 2400 EF)
Data from L2400 series data sheet[3]
General characteristics
- Type: Four-cylinder, four-stroke air-cooled flat piston engine
- Bore: 97 mm (4 in)
- Stroke: 82 mm (3 in)
- Displacement: 2,424 cm³
- Length: 620 mm (24 in)
- Width: 788 mm (31 in)
- Height: 380 mm (15 in)
- Dry weight: 76 kg (168 lb)
Components
Performance
- Power output: 62 kW at 3,000 rpm
- Compression ratio: 9.5:1
References
Notes
- Purdy, p. 76
- Taylor 1996, p. 569
- "Type-Certificate Data Sheet L2400 series engines" (PDF). EASA. 4 August 2006. Archived from the original (PDF) on 23 December 2009. Retrieved 2009-08-29.
Bibliography
- Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 72. BAI Communications. ISBN 0-9636409-4-1
- Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1-85753-198-1.
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