Gnome Delta (original) (raw)

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dbo:abstract The Gnome 9 Delta was a French designed, nine-cylinder, air-cooled rotary aero engine that was produced under license in Britain. Powering several World War I era aircraft types it produced 100 hp (75 kW) from its capacity of 16 litres (980 cu in). (en) Гном 9 Delta (также известен как Gnome type 9A, Gnome 100 л. с. или Гном-100) — французский 9-цилиндровый авиационный поршневой ротативный двигатель воздушного охлаждения. Разработан в конце 1912 года компанией Гном, серийный выпуск с 1913 года. (ru)
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dbo:wikiPageRevisionID 1022450630 (xsd:integer)
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dbp:coolingsystem Air-cooled (en)
dbp:firstRun c.1909 (en)
dbp:fuelsystem one static Bloctube carburettor feeding the crankcase (en)
dbp:fueltype 40 (xsd:integer)
dbp:lists *List of aircraft engines (en)
dbp:majorApplications dbr:Vickers_F.B.5 dbr:Avro_500
dbp:manufacturer dbr:Société_des_Moteurs_Gnome
dbp:oilsystem Total loss pressure fed (en)
dbp:power 75 (xsd:integer)
dbp:ref Lumsden. (en)
dbp:similarEngines *Bentley BR1 *Clerget *Le Rhône 9C (en)
dbp:specfuelcon 362 (xsd:integer)
dbp:type 9 (xsd:integer) dbr:Aircraft_engine dbr:Rotary_engine
dbp:unitCost 22000 (xsd:integer)
dbp:valvetrain Automatic centre-piston inlet valve, one overhead exhaust valve per cylinder. (en)
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dct:subject dbc:1900s_aircraft_piston_engines dbc:Gnome-Rhône_aircraft_engines dbc:Rotary_aircraft_piston_engines dbc:Air-cooled_aircraft_piston_engines
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rdfs:comment The Gnome 9 Delta was a French designed, nine-cylinder, air-cooled rotary aero engine that was produced under license in Britain. Powering several World War I era aircraft types it produced 100 hp (75 kW) from its capacity of 16 litres (980 cu in). (en) Гном 9 Delta (также известен как Gnome type 9A, Gnome 100 л. с. или Гном-100) — французский 9-цилиндровый авиационный поршневой ротативный двигатель воздушного охлаждения. Разработан в конце 1912 года компанией Гном, серийный выпуск с 1913 года. (ru)
rdfs:label Gnome Delta (en) Гном Delta (ru)
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