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Junkers Jumo 204

Aircraft Engines

The Junkers Jumo 204 was an opposed-piston, inline, liquid-cooled six-cylinder aircraft diesel engine built by the German manufacturer Junkers. It descended from the company's earlier Fo3 and Fo4 diesel engines, and the Fo4 was redesignated Jumo 204 by the Reich Air Ministry, whose numbering gave Junkers Motoren the first digit 2. The engine used a two-stroke cycle with twelve pistons working in six cylinders and two geared crankshafts, one at the bottom of the block and one at the top. It was test flown in early 1929 in a Junkers G 24 and entered service in 1932. The later Jumo 205, 206, 207 and 208 differed in stroke, bore and supercharging, and the design was also licensed to Napier, which built a few as the Culverin.

Facts
Classification
Fuel or Cycle
Diesel 1
Fuel or Cycle
Two-stroke 1
Configuration
Opposed-Piston 1
Year
1929 1
Cylinder Count
6 1
Connections

Of Make

Source Junkers Jumo 204 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Junkers Jumo 204 (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
produced by the German manufacturer Junkers
Sources
1. Junkers Jumo 204 (Wikipedia)
  • Lead
    was an opposed-piston, inline, liquid-cooled 6-cylinder aircraft Diesel engine
  • Lead, fuel or cycle
    liquid-cooled 6-cylinder aircraft Diesel engine
  • Design and development
    These engines used a two-stroke cycle with six cylinders and twelve pistons
  • Design and development, year
    The Jumo 204 (originally designated Jumo 4) was test flown in early 1929 installed in a Junkers G 24.
  • Lead, manufacturer
    produced by the German manufacturer Junkers
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