Junkers Jumo 205

Last updated
Jumo 205
Jumo205 cutview.JPG
Jumo 205 cutaway
Type Aircraft diesel engine
Manufacturer Junkers
First run1930s
Major applications Junkers Ju 86
Blohm & Voss BV 138
Blohm & Voss BV 222
Number builtca. 900 [1]
Developed from Junkers Jumo 204

The Jumo 205 aircraft engine was the most famous of a series of aircraft diesel engines produced by Junkers. The Jumo 204 first entered service in 1932. Later engines of this type comprised the experimental Jumo 206 and Jumo 208, with the Jumo 207 produced in some quantity for the Junkers Ju 86P and -R high-altitude reconnaissance aircraft, and the 46-meter wingspan, six-engined Blohm & Voss BV 222 Wiking flying boat. [2] All three of these variants differed in stroke and bore and supercharging arrangements. In all, more than 900 of these engines were produced, in the 1930s and through most of World War II.

Contents

Design and development

A similarly sectioned Junkers Jumo 207 aviation diesel engine Jumo 207 im Technikmuseum Hugo Junkers Dessau 2010-08-06 01.jpg
A similarly sectioned Junkers Jumo 207 aviation diesel engine

These engines all used a two-stroke cycle with 12 pistons sharing six cylinders, piston crown to piston crown in an opposed 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. The intake ports were located at one end of the cylinder, whereas the exhaust ports were at the other end. This made one piston effectively control the intake, and the other control the exhaust. [3] Two cam-operated injection pumps per cylinder were used, each feeding two nozzles, for four nozzles per cylinder in all.

As is typical of two-stroke designs, the Jumos used no valves, but rather fixed intake and exhaust port apertures cut into the cylinder liners during their manufacture, which were uncovered when the pistons reached a certain point in their strokes. 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 valveless 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 11° 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.

Some downside exists 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, somewhat offset upwards on the engine's front end. 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 engine's propeller.

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.

Because the temperature of the exhaust gases of the Jumo diesel engines was substantially lower than that of comparable carburettor engines, it was easier to add a turbocharger for higher altitudes. This was explored in the Jumo 207 which used the energy of the exhaust gases to increase the power at high altitudes. The turbocharger was combined with a mechanically driven blower, so that the turbocharger creates the first stage of compression, and the mechanical blower the second stage. At low load and startup, the turbocharger does not contribute to supercharging the engine, but the mechanical blower provides enough air for the engine to operate. At high load, however, the turbocharger receives sufficient quantities of exhaust gas, which means that it alone can provide enough supercharging without the need of the inefficient mechanical blower. The addition of the turbocharger to the mechanical blower made the engine more powerful without significantly increasing its specific fuel consumption. [4]

Variants

Jumo 205
Jumo 206
An experimental version. Development halted in favour of the Jumo 208.
Jumo 207A
High-altitude version with two inline centrifugal superchargers and a precooler.
Jumo 207 B-3 had an improved turbocharger and featured GM-1 nitrous oxide injection.
Jumo 207 C
optimised for medium altitude. Produced in small series for the Blohm & Voss BV 222.
Jumo 207 D
optimised for medium altitude. Cylinder diameter increased from 105 mm to 110 mm. Maximum power at ground level was 1,200 hp (880 kW). Prototypes only.
Jumo 207 E
similar to the 207 C but greater performance at high altitude. Project only.
Jumo 207 F
optimised for higher altitude. Two-stage turbocharger. Development stopped in 1942. [5]
Jumo 208
with greater displacement, resulting in a maximum power of 1,500 hp (1,100 kW) at medium altitude. Bench tested but not produced.
Jumo 218
A 12-cylinder version, the Jumo 218, was designed but never built.
Jumo 223
A single 24-cylinder four-crankshaft Jumo 223 was built and tested.
Jumo 224
Larger than the Jumo 223 by combining 4 Jumo 207 C engines.
CLM Lille 6As
A license-built version from CLM Lille, delivering 650 hp (480 kW) [6] [7] (CLM was the predecessor to the Indenor  [ fr ] engine maker, a sister company to Peugeot)
CLM Lille 6BrS
A developed version of the 6As used to power the Bernard 86 [7]

Applications

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, as with the Ju 86P and -R versions for high-altitude reconnaissance over the British Isles. In January 1940, the Luftwaffe tested the prototype Ju 86P with Jumo 207A-1 turbocharged diesel engines. It was far more successful as a power unit for airships, for which its characteristics were ideal, and for noncombat applications such as the Blohm & Voss Ha 139 airliner. Its more fuel-efficient operation lent itself for use on Germany's few maritime patrol flying-boat designs during World War II, such as the BV 138 and BV 222.

Applications list

Specifications (Jumo 205E)

Data from Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944 [8]

General characteristics

Components

Performance

  • 700 PS (690 hp; 515 kW) at 2,500 rpm (5 minutes) at sea level
  • 630 PS (621 hp; 463 kW) at 2,420 rpm (30 minutes) at sea level
  • 560 PS (552 hp; 412 kW) at 2,250 rpm (max. continuous) at sea level
  • 500 PS (493 hp; 368 kW) at 2,000 rpm (cruise) at sea level

Other notable opposed-piston engines

See also


Related Research Articles

<span class="mw-page-title-main">Two-stroke engine</span> Internal combustion engine type

A two-strokeengine is a type of internal combustion engine that completes a power cycle with two strokes of the piston during one power cycle, this power cycle being completed in one revolution of the crankshaft. A four-stroke engine requires four strokes of the piston to complete a power cycle during two crankshaft revolutions. In a two-stroke engine, the end of the combustion stroke and the beginning of the compression stroke happen simultaneously, with the intake and exhaust functions occurring at the same time.

<span class="mw-page-title-main">Napier Nomad</span> British diesel aircraft engine

The Napier Nomad is a British diesel aircraft engine designed and built by Napier & Son in 1949. They combined a piston engine with a turbine to recover energy from the exhaust and thereby improve fuel economy. Two versions were tested, the complex Nomad I which used two propellers, each driven by the mechanically independent stages, and the Nomad II, using the turbo-compound principle, coupled the two parts to drive a single propeller. The Nomad II had the lowest specific fuel consumption figures seen up to that time. Despite this the Nomad project was cancelled in 1955 having spent £5.1 million on development, as most interest had passed to turboprop designs.

<span class="mw-page-title-main">BMW 801</span> German aircraft engine developed by BMW during World War II

The BMW 801 was a powerful German 41.8-litre (2,550 cu in) air-cooled 14-cylinder-radial aircraft engine built by BMW and used in a number of German Luftwaffe aircraft of World War II. Production versions of the twin-row engine generated between 1,560 and 2,000 PS. It was the most produced radial engine of Germany in World War II with more than 61,000 built.

<span class="mw-page-title-main">Napier Deltic</span> Opposed-piston engine used in marine, firefighting and BR locomotive applications

The Napier Deltic engine is a British opposed-piston valveless, supercharged uniflow scavenged, two-stroke diesel engine used in marine and locomotive applications, designed and produced by D. Napier & Son. Unusually, the cylinders were disposed in a three-bank triangle, with a crankshaft at each corner of the triangle.

<span class="mw-page-title-main">Opposed-piston engine</span> Combustion engine using disks compressing fuel in the same cylinder

An opposed-piston engine is a piston engine in which each cylinder has a piston at both ends, and no cylinder head. Petrol and diesel opposed-piston engines have been used mostly in large-scale applications such as ships, military tanks, and factories. Current manufacturers of opposed-piston engines include Cummins, Achates Power and Fairbanks-Morse Defense (FMDefense).

<span class="mw-page-title-main">Blohm & Voss BV 138</span> 1937 flying boat family by Blohm & Voss

The Blohm & Voss BV 138Seedrache was a trimotor flying boat designed and built by the German aircraft manufacturer Blohm & Voss. It served as the Luftwaffe's primary seaborne long-range maritime patrol and naval reconnaissance aircraft operated by the Luftwaffe during the Second World War.

<span class="mw-page-title-main">Junkers Jumo 222</span>

The Jumo 222 was a German high-power multiple-bank in-line piston aircraft engine from Junkers, designed under the management of Ferdinand Brandner of the Junkers Motorenwerke.

<span class="mw-page-title-main">Junkers Jumo 204</span>

The Jumo 204 was an opposed-piston, inline, liquid-cooled 6-cylinder aircraft Diesel engine produced by the German manufacturer Junkers. It entered service in 1932. Later engines in the series, the Jumo 205, Jumo 206, Jumo 207 and Jumo 208, differed in stroke, bore, and supercharging arrangements.

<span class="mw-page-title-main">Junkers Jumo 211</span> German inverted V-12 aircraft engine

The Jumo 211 was a German inverted V-12 aircraft engine, Junkers Motoren's primary aircraft engine of World War II. It was the direct competitor to the Daimler-Benz DB 601 and closely paralleled its development. While the Daimler-Benz engine was mostly used in single-engined and twin-engined fighters, the Jumo engine was primarily used in bombers such as Junkers' own Ju 87 and Ju 88, and Heinkel's H-series examples of the Heinkel He 111 medium bomber. It was the most-produced German aero engine of the war, with almost 70,000 examples completed.

<span class="mw-page-title-main">BMW 803</span>

The BMW 803 was a German aircraft engine, an attempt by BMW to build a high-output aircraft engine by coupling two BMW 801 engines back-to-back, driving contra-rotating propellers. The result was a 28-cylinder, four-row radial engine, each comprising a multiple-bank in-line engine with two cylinders in each bank, which, due to cooling concerns, were liquid cooled.

<span class="mw-page-title-main">Junkers Jumo 213</span> WW2 Aircraft Engine

The Junkers Jumo 213 was a World War II-era V-12 liquid-cooled aircraft engine, a development of Junkers Motoren's earlier design, the Jumo 211. The design added two features, a pressurized cooling system that required considerably less cooling fluid which allowed the engine to be built smaller and lighter, and a number of improvements that allowed it to run at higher RPM. These changes boosted power by over 500 hp and made the 213 one of the most sought-after Axis engine designs in the late-war era.

<span class="mw-page-title-main">Daimler-Benz DB 603</span> German aircraft engine

The Daimler-Benz DB 603 was a German aircraft engine used during World War II. It was a liquid-cooled 12-cylinder inverted V12 enlargement of the 33.9 Liter DB 601, which was in itself a development of the DB 600. Production of the DB 603 commenced in May 1942, and with a 44.5 liter displacement figure, was the largest displacement inverted V12 aviation engine to be produced and used in front line aircraft of the Third Reich during World War II.

<span class="mw-page-title-main">Aircraft diesel engine</span> Aircraft engine operating on the Diesel principle

The aircraft diesel engine or aero diesel is a diesel-powered aircraft engine. They were used in airships and tried in aircraft in the late 1920s and 1930s, but were never widely adopted until recently. Their main advantages are their excellent specific fuel consumption, the reduced flammability and somewhat higher density of their fuel, but these have been outweighed by a combination of inherent disadvantages compared to gasoline-fueled or turboprop engines. The ever-rising cost of avgas and doubts about its future availability have spurred a resurgence in aircraft diesel engine production in the early 2010s.

<span class="mw-page-title-main">Two-stroke diesel engine</span> Engine type

A two-stroke diesel engine is a diesel engine that uses compression ignition in a two-stroke combustion cycle. It was invented by Hugo Güldner in 1899.

<span class="mw-page-title-main">Napier Culverin</span> 1930s British aircraft piston engine

The Napier Culverin was a licensed built version of the Junkers Jumo 204 six-cylinder vertically opposed liquid-cooled diesel aircraft engine built by D. Napier & Son. The name is derived from the French word, culverin, for an early cannon or musket. First flown in 1938, the engine went into limited production, with testing carried out on a Blackburn Iris V biplane flying-boat aircraft and Fairey IIIF biplane.

The Detroit Diesel Series 110, with 110 cubic inches (1.8 L) displacement per cylinder, was introduced in 1945 as more-powerful alternative to the existing Series 71 engines. It was used in a variety of applications, including construction equipment, marine propulsion and power generation. The most popular use was in the Budd RDC self-powered rail car. It was also heavily used in Euclid construction machinery. In 1951 a marine version was also introduced.

The Junkers L88 was Junkers' first geared V-12 engine, appearing c.1930 and based on a pair of 6-cylinder L8s. In 1932 a supercharger was added. It was used in the world's second working pressurised aircraft, the Junkers Ju 49 and, for a while, in the large G 38 airliner and its Japanese built military version.

The Michel engine was an unusual form of opposed-piston engine. It was unique in that its cylinders, instead of being open-ended cylinders containing two pistons, were instead joined in a Y-shape and had three pistons working within them.

The Blohm & Voss BV 237 was a German proposed dive bomber with an unusual asymmetric design based on the Blohm & Voss BV 141.

The Diesel Air Dair 100 is an opposed-piston diesel aircraft engine, designed and produced by Diesel Air Ltd of Olney, Buckinghamshire for use in airships, home-built kitplanes and light aircraft. The prototype was built in the 1990s and exhibited it at PFA airshows. Although Diesel Air engines have been fitted to an AT-10 airship and to a Luscombe 8A monoplane, production numbers have been very limited.

References

  1. Konrad Reif: Dieselmotor Management – Systeme, Komponenten, Steuerung und Regelung, 5th edition, Springer, Wiesbaden 2012, ISBN 978-3-8348-1715-0, p. 102
  2. "Smithsonian National Air & Space Museum - Junkers Jumo 207 D-V2 In-line 6 Diesel Engine". airandspace.si.edu. Smithsonian Institution. 2016-03-20. Archived from the original on 2017-12-29. Retrieved December 29, 2017.
  3. Paul Henry Schweitzer: Scavenging of two-stroke cycle Diesel engines, Macmillan, New York 1949, p. 8
  4. Paul Henry Schweitzer: Scavenging of two-stroke cycle Diesel engines, Macmillan, New York 1949, p. 19
  5. Reinhard Mueller (2006) Junkers Flugtriebwerke.
  6. "POWER at the SALON j Detailed Review of the British and Continental Engines at the Show : A Remarkable Variety of Types". Flight. 26 November 1936. p. 577. Retrieved 14 March 2015.
  7. 1 2 "Characteristiques et Description du Moteur Type Lille 6Brs de 600CV" (in French). Retrieved 6 November 2017.
  8. Schneider, Helmut (Dipl.Ing.) (1944). Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944 (in German) (Facsimile reprint 1986 ed.). Leipzig: Herm. Beyer Verlag. p. 396. ISBN   381120484X.

Further reading