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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.

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rdf:type
rdfs:label
  • Junkers Jumo 204 (en)
  • Junkers Jumo 204 (it)
rdfs:comment
  • 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. (en)
  • Lo Junkers Jumo 204 era un motore aeronautico a ciclo Diesel a due tempi, con 6 cilindri a doppio albero a gomiti e pistoni contrapposti, progettato e realizzato dall'azienda tedesca Junkers Flugzeug und Motorenwerke AG nel 1931. Fu il primo motore aeronautico a ciclo Diesel prodotto in serie. (it)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/Jumo205_cutview.jpg
dct:subject
Wikipage page ID
Wikipage revision ID
Link from a Wikipage to another Wikipage
Link from a Wikipage to an external page
sameAs
specfuelcon
  • at max continuous (en)
stroke
  • x2 (en)
dbp:wikiPageUsesTemplate
thumbnail
manufacturer
power
  • :* at 1,700 rpm at sea level :* at 1,600 rpm at sea level (en)
ref
  • Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944, Der Flugmotor. Bauteile und Baumuster, and Schweitzer (en)
type
weight
  • dry, unequipped (en)
has abstract
  • 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. (en)
  • Lo Junkers Jumo 204 era un motore aeronautico a ciclo Diesel a due tempi, con 6 cilindri a doppio albero a gomiti e pistoni contrapposti, progettato e realizzato dall'azienda tedesca Junkers Flugzeug und Motorenwerke AG nel 1931. Fu il primo motore aeronautico a ciclo Diesel prodotto in serie. (it)
compression
coolingsystem
  • liquid-cooled (en)
developed into
first run
fuelsystem
  • direct injection through four nozzles per cylinder (en)
fueltype
  • Diesel fuel (en)
oilcon
  • at max continuous (en)
oilsystem
  • dry sump, pressure feed with scavenge (en)
power/weight
  • *B.M.E.P.: *Reduction gear: 0.695:1 (en)
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page length (characters) of wiki page
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is Link from a Wikipage to another Wikipage of
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