About: CNA C.II

An Entity of Type: mean of transportation, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org

The CNA C.II was a small, air-cooled, two cylinder horizontally opposed aircraft engine designed and built in Italy in the late 1930s.

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dbo:abstract
  • The CNA C.II was a small, air-cooled, two cylinder horizontally opposed aircraft engine designed and built in Italy in the late 1930s. (en)
dbo:wikiPageID
  • 35180218 (xsd:integer)
dbo:wikiPageLength
  • 3074 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1098956878 (xsd:integer)
dbo:wikiPageWikiLink
dbp:bore
  • 90.0
dbp:coolingsystem
  • Air (en)
dbp:displacement
  • 1.4
dbp:height
  • 526.0
dbp:length
  • 478.0
dbp:manufacturer
dbp:nationalOrigin
dbp:oilsystem
  • Wet sump; crankshaft fed pressurised oil by pump. (en)
dbp:power
  • rated 28 kW at 2,700 rpm at sea level (en)
dbp:produced
  • 1937 (xsd:integer)
dbp:ref
  • Jane's All the World's Aircraft 1938 (en)
dbp:stroke
  • 110.0
dbp:type
dbp:valvetrain
  • Large diameter overhead valves, one inlet and one exhaust per cylinder. Enclosed rocker gear operated by push-rods driven off upper crankcase camshaft. (en)
dbp:weight
  • dry 42 kg (en)
dbp:width
  • 856.0
dbp:wikiPageUsesTemplate
dcterms:subject
gold:hypernym
rdf:type
rdfs:comment
  • The CNA C.II was a small, air-cooled, two cylinder horizontally opposed aircraft engine designed and built in Italy in the late 1930s. (en)
rdfs:label
  • CNA C.II (en)
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