|Type||Inline aircraft engine|
|Manufacturer||Junkers Motorenbau GmbH (Jumo)|
|Major applications||Junkers F.13|
|Developed into||Junkers L8|
The Junkers L 5 was a six-cylinder, water-cooled, inline engine for aircraft built in Germany during the 1920s. First run in 1925, it was a much enlarged development of the Junkers L2, in turn a licensed development of the BMW IV.
Design and development
The Junkers L5 was a development of Junkers' first water-cooled engine, the L2, but at four times the swept volume was a much more powerful engine. It was a water-cooled upright inline 6-cylinder unit, four-stroke and petrol-fuelled, with a capacity of nearly 23 litres. It adopted some of the L2 features, having twin exhaust and inlet valves in each cylinder driven by an overhead camshaft, twin spark plugs and twin magnetos. The splash component of the L2's lubrication was abandoned in favour of a completely forced recirculating system. The twin carburettors of the L2 were replaced with a single float chamber, dual-venturi model. Like the L2, the L5 was a direct drive engine.
The compression ratio of the standard version was 5.5:1, but variants had other ratios to cope with fuels with octane ratings between 76 and 95. The G series introduced carburettor heating together with an hydraulically damped mounting system. There were also choices of starting system, from inertial or compressed air systems to the traditional hand swinging.
The L5 proved to be reliable and became the engine of choice for most Junkers aircraft in the mid-1920s as well as powering aircraft from other German manufacturers. Many of these powered the Junkers F.13 and its derivatives like the W 33, which dominated world air transport in the mid-1920s.
The best demonstration of the reliability of the L5 was given by the unit which powered the single-engined W 33 Bremen in the first fixed wing east to west crossing of the Atlantic in April 1928. For this flight the compression ratio was raised to 7:1 to provide sufficient power for the heavily fuelled aircraft at take off. In July 1925 a W 33 powered by a L5 stayed aloft for 65 h 25 min, with a fuel consumption of 35.6 kg/h.
- L5 many variants including a variety of on compression ratios, power output levels and starting systems.
- L55 an upright V-12 built from two L5s on a common crankshaft.
- L8 a significant 1929 development with the same swept volume but cruising at 2,100 rpm and delivering 354 hp; take off power was 413 hp. The output was geared down at ratios between 2.47:1 and 1.44:1 to enhance propeller efficiency. Only a few were produced, powering early configurations of the Junkers G 38 as outer engines, with two L55s inboard.
- L88 an upright V-12 built from two L8s on a common crankshaft.
- Albatros L 73
- Albatros L 75
- Focke-Wulf A 32
- Heinkel HD 42
- Heinkel He 50
- Junkers F 13
- Junkers A 20
- Junkers A 35
- Junkers G 23
- Junkers G 24
- Junkers K 30
- Junkers G 31
- Junkers W 33
- Messerschmitt M 24
- Rohrbach Ro.VIII
Specifications (Jumo L 5)
Data from 
- Type: 6-cylinder liquid-cooled inline
- Bore: 160 mm (6.30 in)
- Stroke: 190 mm (7.48 in)
- Displacement: 22.92 l (1,398.66 cu in)
- Length: 1,750 mm (5.74 ft)
- Width: 650 mm (2.13 ft)
- Height: 1,265 mm (49.80 in)
- Dry weight: 334 kg (736.34 lb) dry
- Valvetrain: large single exhaust and single inlet valves driven by a single overhead camshaft shaft and gear driven from the crankshaft
- Supercharger: none
- Fuel system: single float, dual venturi carburettor; twin plugs per cylinder, twin magnetos
- Fuel type: 95 octane (dependent on compression ratio)
- Oil system: forced
- Cooling system: liquid
- Power output: Take-off - 260 kW (348.7 hp) at 1,450 rpm
- Cruise - 208.8 kW (280 hp)
- Compression ratio: 7:1
- Fuel consumption: 61.6 kg/h (136 lb/hr)
- Power-to-weight ratio: 1.22 kg/kW (2.01 lb/hp) @ cruise rpm
- Related lists
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