Junkers Jumo 205
|Jumo 205 cutaway|
|Type||Aircraft Diesel engine|
|Major applications||Junkers Ju 86
Blohm & Voss BV 138
Blohm & Voss BV 222
|Developed from||Junkers Jumo 204|
The Junkers Jumo 205 aircraft engine was the most famous of a series of Diesel engines that were the first, and for more than half a century the only, successful aircraft Diesel engines. The Jumo 204 first entered service in 1932. Later engines in the series were styled Jumo 206, Jumo 207 and Jumo 208, and differed in stroke and bore and supercharging arrangements. In all more than 900 of these engines were produced.
Design and development
These engines all used a two-stroke cycle with twelve pistons sharing six cylinders, piston-head to piston-head in an opposed piston configuration. This unusual configuration required two crankshafts, one at the bottom of the cylinder block and the other at the top, geared together. The pistons moved towards each other during the operating cycle. Intake and exhaust manifolds were duplicated on both sides of the block. There were two cam-operated injection pumps per cylinder, each feeding two nozzles, for 4 nozzles per cylinder in all.
As is typical of two-stroke designs, the Jumos used fixed intake and exhaust ports instead of valves, which were uncovered when the pistons reached a certain point in their stroke. Normally such designs have poor volumetric efficiency because both ports open and close at the same time and are generally located across from each other in the cylinder. This leads to poor scavenging of the burnt charge, which is why valve-less two-strokes generally produce smoke and are inefficient.
The Jumo solved this problem to a very large degree through clever arrangement of the ports. The intake port was located under the "lower" piston, while the exhaust port was under the "upper". The lower crankshaft ran eleven degrees behind the upper, meaning that the exhaust ports opened and, even more importantly, closed first, allowing proper scavenging. This system made the two-stroke Jumos run as cleanly and almost as efficiently as four-stroke engines using valves, but with considerably less complexity.
There is some downside to this system as well. For one, since matching pistons were not closing at quite the same time, but one ran "ahead" of the other, the engine could not run as smoothly as a true opposed style engine. In addition, the power from the two opposing crankshafts had to be geared together, adding weight and complexity, a problem the design shared with H block engines.
In the Jumo, these problems were avoided to some degree by taking power primarily from the "upper" shaft. All of the accessories, such as fuel pumps, injectors and the scavenging compressor, were run from the lower shaft, meaning over half of its power was already used up. What was left over was then geared to the upper shaft, which ran the propellers. In all, about three-quarters of the power to the propellers came from the upper crankshaft.[dubious ]
In theory, the flat layout of the engine could have allowed it to be installed inside the thick wings of larger aircraft, such as airliners and bombers. Details of the oil scavenging system suggest this was not possible and the engine had to be run "vertically", as it was on all designs using it.
A twelve cylinder version, the Jumo 218, was designed but never built, while a single 24-cylinder 4-crankshaft Junkers Jumo 223 was built and tested.
The Jumo 204 and 205 were licensed to Napier & Son, who built a small number as the Napier Culverin just prior to the war. After the war, they mounted three Culverins in a triangle layout to produce the Napier Deltic, which was for some time one of the most powerful and compact diesel engines in the world. Work on this engine started in 1947 and engines were running by 1950.
The Jumo 205 powered early versions of the Junkers Ju 86 bomber, but was found too unresponsive for combat and liable to failure at maximum power, common for combat aircraft. Later versions of the design also used the engine for extreme high-altitude use. It was far more successful as a power unit for airships, for which its characteristics were ideal, and for non-combat applications such as the Blohm & Voss Ha 139 airliner.
- Blohm & Voss BV 138
- Blohm & Voss Ha 139
- Blohm & Voss BV 222
- Dornier Do 18
- Dornier Do 26
- Junkers Ju 86
Specifications (Jumo 205D)
Data from 
- Type: Six-cylinder 12-piston liquid-cooled opposed piston inline two-stroke diesel engine
- Bore: 105 mm (4.13 in)
- Stroke: 160 mm (6.3 in)
- Displacement: 16.63 L (1,015 in³)
- Length: 76.5 in (1,934 mm)
- Width: 21.54 in (547 mm)
- Height: 52.17 in (1,325 mm)
- Dry weight: 595 kg (1,312 lb)
- Supercharger: Spülgebläse
- Fuel system: Fuel injection
- Fuel type: Diesel
- Oil system: Forced with one pressure and two scavenge pumps
- Cooling system: Liquid-cooled
- Power output: 880 PS (868 hp, 647 kW at 2,800 rpm
- Specific power: 39.0 kW/L (0.86 hp/in³)
- Compression ratio: 17:1
- Power-to-weight ratio: 1.09 kW/kg (0.66 hp/lb)
Other notable opposed piston engines
- Commer TS3 "The Commer Knocker" commercial vehicle engine.
- Leyland Motors L60 tank engine, used in the Chieftain tank. Similar in layout to the Junkers Jumo 205 and Napier Culverin.
- Rolls-Royce K60 engine, smaller and improved version of the L60 used in the FV430 series armoured fighting vehicles and Swedish tank Strv 103.
- Napier Deltic.
- Soviet engine 5TDF used on tank T-64.
- Soviet engine 6TD used on tanks T-80UD, T-84 and Al-Khalid.
- Fairbanks Morse 38 8 1/8
- Jane's 1989, p. 294.
- Jane's Fighting Aircraft of World War II. London. Studio Editions Ltd, 1989. ISBN 0-517-67964-7
|Wikimedia Commons has media related to Junkers Jumo 205.|
- Multi-crankshafts opposed piston engines (french)
- description and cutaway view
- Royal Air Force Museum - Jumo 205
- OpposedPistonEngines.com's Jumo 205 Page
- OpposedPistonEngines.com's Jumo 207 Page