Junkers Jumo 204

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Jumo 204
Jumo205 cutview.JPG
Cut away view of a Jumo 205, a decreased capacity version of the Jumo 204
Type Aircraft Diesel engine
Manufacturer Junkers
First run 1929
Developed into Junkers Jumo 205

The Junkers Jumo 204 was the second in a series of German aircraft Diesel engines. The Jumo 204 first entered service in 1932. Later engines in the series were designated Jumo 205, Jumo 206, Jumo 207 and Jumo 208, they differed in stroke and bore and supercharging arrangements.

Design and development[edit]

Development of the Junkers diesel engines started in the 1920s with the Junkers Fo3 and Junkers Fo4/Junkers SL1. The Fo4 was re-designated Junkers 4, which in turn was re-designated Junkers 204 by the Reichsluftfahrtministerium (RLM).[1]

These engines all used a two-stroke cycle with six cylinders and twelve pistons, in an opposed piston configuration with 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 ports were duplicated at both ends of the block. There were two cam-operated injection pumps per cylinder, each feeding two nozzles, totaling four nozzles per cylinder.

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 run smoky and are inefficient.

The Jumo 204 solved this problem to a very large degree through a better 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 first, allowing proper scavenging. This system made the two-stroke Jumos run as cleanly as four-stroke engines using valves, but with considerably less complexity.

The Jumo 204 (originally designated Jumo 4) was test flown in early 1929 installed in a Junkers G 24.[2]

The Jumo Fo3 and 204 were licensed to Napier & Son, who built a small number as the Napier Culverin just prior to the war. Late in 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.

Variants[edit]

Data from Junkers Aircraft & Engines 1913-1945.[1]

Mo3
A research diesel engine for test bed use only, the Mo3 was a four cylinder, (eight piston), opposed-piston engine designed to run horizontally. Tested from 1913, the problems found in testing the Mo3 were progressively solved after WWI with the Fo3 and later opposed piston diesels.
Fo3
From 1924, Junkers experimented with the Fo3, A vertical 5-cyl. opposed-piston diesel, which ran on a test bed in the summer of 1926, developing 620 kW (830 hp) at 1,200 rpm. Mostly successful, the Fo3 did highlight the need for accurate dynamic balancing of the rotating components.
Fo4
(a.k.a. SL1) The Fo4, benefiting from the experience gained with the Fo3, was a six-cylinder opposed-piston diesel engine, tested from 1928 and flown in the nose of a Junkers G.24 from 30 August 1929.
Jumo 4
After the successful bench runs and flight tests, the Fo4 was refined into the certicated Jumo 4, enjoying limited success powering re-engined Junkers F24kay airliners of Deutsche Luft Hansa, remaining in service until 1939.
Jumo 204
Later production of refined Jumo 4s, designated Jumo 204 in three sub-variants: 204A, 204B,and 204C, differing in airscrew drive arrangements.

Applications[edit]

Specifications (Jumo 204)[edit]

General characteristics

  • Type: Six-cylinder 12-piston liquid-cooled opposed piston inline two-stroke diesel engine
  • Bore: 120 mm (4.72 in)
  • Stroke: 210 mm (8.27 in)
  • Displacement: 28.5 l (1,739 in³)
  • Length: 1,260 mm (49.61 in)
  • Width: 510 mm (20.08 in)
  • Height: 1,510 mm (59.45 in)
  • Dry weight: 750 kg (1,653 lb)

Performance

See also[edit]

References[edit]

Notes[edit]

  1. ^ a b Kay, Anthony L. (2004). Junkers Aircraft & Engines 1913-1945. London: Putnam Aeronautical Books. ISBN 0851779859. 
  2. ^ Gunston 1989, p.86.
  3. ^ Single engine prototypes
  4. ^ "Longer Range of Diesel Plane Cuts Fuel Cost" Popular Mechanic, December 1935

Bibliography[edit]

  • Kay, Anthony L. (2004). Junkers Aircraft & Engines 1913-1945. London: Putnam Aeronautical Books. ISBN 0851779859. 
  • Gunston, Bill (1989). World Encyclopaedia of Aero Engines (2nd edition ed.). Cambridge, England: Patrick Stephens Limited. ISBN 1-85260-163-9. 
  • Jane's Fighting Aircraft of World War II. Military Press. 1994. ISBN 978-0517679647. 

External links[edit]