About:Sergant A

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The Sergant A was a French 4-cylinder, air-cooled, upright inline piston engine with a maximum output of 7.5 kW (10 hp), designed to meet the needs of the very small and light single seat sports aircraft of the early 1920s. It was used by at least ten different types.

Property	Value
dbo:abstract	The Sergant A was a French 4-cylinder, air-cooled, upright inline piston engine with a maximum output of 7.5 kW (10 hp), designed to meet the needs of the very small and light single seat sports aircraft of the early 1920s. It was used by at least ten different types. (en)
dbo:wikiPageExternalLink	http://claudel.dopp.free.fr/Les_planeurs/Descriptions_planeurs/Poncelet_Vivette/Poncelet-Vivette.htm
dbo:wikiPageID	53168837 (xsd:integer)
dbo:wikiPageLength	4801 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID	1102333722 (xsd:integer)
dbo:wikiPageWikiLink	dbr:Petrol dbr:Peyret_Avionette dbr:Inline_engine_(aeronautics) dbr:Manganese dbr:Zenith_Carburettor_Company_(British) dbr:UK dbr:Aluminium dbr:France dbr:Bristol_Cherub dbr:Carley_C.12 dbr:Farman_Moustique dbr:Italy dbr:Crankcase dbr:Crankshaft dbc:1920s_aircraft_piston_engines dbr:Camshaft dbr:Carmier-Simplex_10_hp dbr:Breguet_Colibri dbr:Magneto dbr:Rocker_arm dbr:Silicon dbr:Piston_engine dbr:Carburettor dbr:Pushrod dbr:Peyret-le_Prieur_Hydroplan dbr:SABCA-Jullien_SJ-1A dbr:Scintilla_(aeronautics) dbr:Poncelet_Castar dbr:Poncelet_Vivette dbr:Gambier-SABCA
dbp:componentsOther	Crankshaft: 3-bearing, silicon-manganese steel forging (en)
dbp:coolingsystem	air, directed from a forward scoop around cylinders and vertical fins (en)
dbp:designer	Sergant (en)
dbp:fuelsystem	Zenith carburettor, single Scintilla magneto (en)
dbp:fueltype	dbr:Petrol
dbp:manufacturer	Sergant (en)
dbp:nationalOrigin	dbr:France
dbp:oilsystem	18000.0
dbp:power	at 3,200 rpm crankshaft speed (en)
dbp:power/weight	0.260000 (xsd:double)
dbp:reductionGear	Choice of three reduction gear ratios: 14/35, 15/34 and 16/33 (en)
dbp:ref	Les Ailes, August 1923; Flight, February 1924 (en)
dbp:type	4 (xsd:integer)
dbp:valvetrain	cylinder head valves operated by rocker arms driven via pushrods from a camshaft in aluminium crankcase (en)
dbp:weight	including carburettor and magneto (en)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Reflist dbt:Short_description dbt:Aircontent dbt:Infobox_Aircraft_Engine dbt:Pistonspecs
dcterms:subject	dbc:1920s_aircraft_piston_engines
rdfs:comment	The Sergant A was a French 4-cylinder, air-cooled, upright inline piston engine with a maximum output of 7.5 kW (10 hp), designed to meet the needs of the very small and light single seat sports aircraft of the early 1920s. It was used by at least ten different types. (en)
rdfs:label	Sergant A (en)
owl:sameAs	wikidata:Sergant A https://global.dbpedia.org/id/2qGqL
prov:wasDerivedFrom	wikipedia-en:Sergant_A?oldid=1102333722&ns=0
foaf:isPrimaryTopicOf	wikipedia-en:Sergant_A
isdbo:wikiPageWikiLink of	dbr:List_of_aircraft_engines dbr:Peyret-Le_Prieur_seaplane dbr:Peyret_Avionette dbr:Bréguet_Colibri dbr:Carley_C.12 dbr:Farman_Moustique dbr:Carmier-Simplex_10_hp
isdbp:eng1Name of	dbr:Peyret-Le_Prieur_seaplane dbr:Peyret_Avionette dbr:Carmier-Simplex_10_hp
isfoaf:primaryTopic of	wikipedia-en:Sergant_A

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About:Sergant A