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.

Attributes	Values
rdfs:label	Sergant A (en)
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)
dcterms:subject	1920s aircraft piston engines
Wikipage page ID	53168837 (xsd:integer)
Wikipage revision ID	1102333722 (xsd:integer)
Link from a Wikipage to another Wikipage	Petrol Peyret Avionette Inline engine (aeronautics) Manganese Zenith Carburettor Company (British) UK Aluminium France Bristol Cherub Carley C.12 Farman Moustique Italy Crankcase Crankshaft 1920s aircraft piston engines Camshaft Carmier-Simplex 10 hp Breguet Colibri Magneto Rocker arm Silicon Piston engine Carburettor Pushrod dbr:Peyret-le_Prieur_Hydroplan dbr:SABCA-Jullien_SJ-1A dbr:Scintilla_(aeronautics) dbr:Poncelet_Castar dbr:Poncelet_Vivette dbr:Gambier-SABCA
Link from a Wikipage to an external page	http://claudel.dopp.free.fr/Les_planeurs/Descriptions_planeurs/Poncelet_Vivette/Poncelet-Vivette.htm
sameAs	Sergant A Sergant A
valvetrain	cylinder head valves operated by rocker arms driven via pushrods from a camshaft in aluminium crankcase (en)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Reflist dbt:Short_description dbt:Aircontent dbt:Infobox_Aircraft_Engine dbt:Pistonspecs
national origin	France
designer	Sergant (en)
manufacturer	Sergant (en)
power	at 3,200 rpm crankshaft speed (en)
ref	Les Ailes, August 1923; Flight, February 1924 (en)
type	4 (xsd:integer)
weight	including carburettor and magneto (en)
has 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)
components other	Crankshaft: 3-bearing, silicon-manganese steel forging (en)
coolingsystem	air, directed from a forward scoop around cylinders and vertical fins (en)
fuelsystem	Zenith carburettor, single Scintilla magneto (en)
fueltype	Petrol
oilsystem	18000.0 (second)
power/weight	0.260000 (xsd:double)
reduction gear	Choice of three reduction gear ratios: 14/35, 15/34 and 16/33 (en)
prov:wasDerivedFrom	wikipedia-en:Sergant_A?oldid=1102333722&ns=0
page length (characters) of wiki page	4801 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:Sergant_A
is Link from a Wikipage to another Wikipage of	List of aircraft engines Peyret-Le Prieur seaplane Peyret Avionette Bréguet Colibri Carley C.12 Farman Moustique Carmier-Simplex 10 hp
is eng1 name of	Peyret-Le Prieur seaplane Peyret Avionette Carmier-Simplex 10 hp
is foaf:primaryTopic of	wikipedia-en:Sergant_A

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