| Limbach L 2400 | |
|---|---|
| Type | Piston aircraft engine |
| National origin | Germany |
| Manufacturer | Limbach Flugmotoren |
| First run | c.1984 |
| Major applications | Stemme S10 |
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.
Variants
- L 2400 DE3.X
- Dual ignition system. 90 hp (67 kW)
- 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.
- 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.
- 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)
- 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.
- 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.
- L 2400 EFI
- Fully electronic fuel injection. 100 hp (75 kW)
- L 2400 EO.X
- Single ignition system. 87 hp (65 kW)
- 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.
Applications
Specifications (L 2400 EF)
Data from L2400 series data sheet
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
See also
Related lists
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 29 August 2009.
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.
| Limbach Flugmotoren aero engines | |
|---|---|
| Piston engines | |