This HTML5 document contains 51 embedded RDF statements represented using HTML+Microdata notation.

The embedded RDF content will be recognized by any processor of HTML5 Microdata.

Namespace Prefixes

PrefixIRI
dctermshttp://purl.org/dc/terms/
dbohttp://dbpedia.org/ontology/
foafhttp://xmlns.com/foaf/0.1/
n13https://global.dbpedia.org/id/
dbthttp://dbpedia.org/resource/Template:
rdfshttp://www.w3.org/2000/01/rdf-schema#
rdfhttp://www.w3.org/1999/02/22-rdf-syntax-ns#
owlhttp://www.w3.org/2002/07/owl#
wikipedia-enhttp://en.wikipedia.org/wiki/
dbphttp://dbpedia.org/property/
dbchttp://dbpedia.org/resource/Category:
provhttp://www.w3.org/ns/prov#
xsdhhttp://www.w3.org/2001/XMLSchema#
wikidatahttp://www.wikidata.org/entity/
dbrhttp://dbpedia.org/resource/

Statements

Subject Item
dbr:Franklin_O-540
rdfs:label
Franklin O-540
rdfs:comment
The Franklin O-540 (company designation 8AC) was an American air-cooled aircraft engine that first ran in the early-1940s. The engine was of eight-cylinder, horizontally-opposed layout and displaced 540 cu in (9 L). The power output was nominally 300 hp (224 kW).
dcterms:subject
dbc:Boxer_engines dbc:1940s_aircraft_piston_engines dbc:Franklin_aircraft_engines
dbo:wikiPageID
38380267
dbo:wikiPageRevisionID
1035210174
dbo:wikiPageWikiLink
dbr:Flat-eight_engine dbr:List_of_aircraft_engines dbr:Continental_Tiara_series dbr:Franklin_Engine_Company dbr:Flat-6 dbc:Boxer_engines dbr:Lycoming_O-540 dbr:Northrop_N-9M dbc:1940s_aircraft_piston_engines dbr:Aircraft_engine dbc:Franklin_aircraft_engines dbr:Engine_displacement dbr:Piston
owl:sameAs
wikidata:Q48834721 n13:4WxuH
dbp:similarEngines
*Continental T8-450 *Lycoming O-540
dbp:stroke
4.0
dbp:wikiPageUsesTemplate
dbt:Infobox_Aircraft_Engine dbt:Refbegin dbt:Refend dbt:Convert dbt:Reflist dbt:Aircontent dbt:Short_description dbt:Pistonspecs dbt:Fact dbt:US_military_piston_aeroengines dbt:Franklin_aeroengines
dbp:nationalOrigin
United States
dbp:manufacturer
dbr:Franklin_Engine_Company
dbp:power
300
dbp:type
dbr:Aircraft_engine dbr:Piston 8
dbp:weight
438.0
dbo:abstract
The Franklin O-540 (company designation 8AC) was an American air-cooled aircraft engine that first ran in the early-1940s. The engine was of eight-cylinder, horizontally-opposed layout and displaced 540 cu in (9 L). The power output was nominally 300 hp (224 kW).
dbp:bore
4.625
dbp:coolingsystem
Air-cooled
dbp:displacement
537.6
dbp:firstRun
1942
dbp:lists
*List of aircraft engines
prov:wasDerivedFrom
wikipedia-en:Franklin_O-540?oldid=1035210174&ns=0
dbo:wikiPageLength
2892
foaf:isPrimaryTopicOf
wikipedia-en:Franklin_O-540