About: SNECMA 14R

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An Entity of Type : yago:WikicatRadialEngines, within Data Space : dbpedia.org associated with source document(s)
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The SNECMA 14R was a 14-cylinder two-row air-cooled radial engine developed in France just prior to the start of World War II from the Gnome-Rhône 14N. The 14N radial engine was itself an improved version of the popular pre-war Gnome-Rhône 14K Mistral Major series; designed and manufactured by Gnome et Rhône, a major French aircraft engine manufacturer whose origins pre-date the First World War.

Attributes	Values
rdf:type	yago:AircraftEngine102687423 yago:Artifact100021939 yago:Device103183080 yago:Engine103287733 yago:HeatEngine103507963 yago:Instrumentality103575240 yago:Internal-combustionEngine103579982 yago:Machine103699975 yago:Motor103789946 yago:Object100002684 yago:PhysicalEntity100001930 yago:RadialEngine104040373 yago:Whole100003553 yago:WikicatRadialEngines
rdfs:label	SNECMA 14R (en)
rdfs:comment	The SNECMA 14R was a 14-cylinder two-row air-cooled radial engine developed in France just prior to the start of World War II from the Gnome-Rhône 14N. The 14N radial engine was itself an improved version of the popular pre-war Gnome-Rhône 14K Mistral Major series; designed and manufactured by Gnome et Rhône, a major French aircraft engine manufacturer whose origins pre-date the First World War. (en)
foaf:depiction
dcterms:subject	Gnome-Rhône aircraft engines Aircraft air-cooled radial piston engines 1930s aircraft piston engines Snecma aircraft engines
Wikipage page ID	33237355 (xsd:integer)
Wikipage revision ID	1111487863 (xsd:integer)
Link from a Wikipage to another Wikipage	List of aircraft engines Radial engine Gnome-Rhône 14K SNECMA Gnome-Rhône 14N Gnome-Rhône aircraft engines Aircraft engine First World War France Gnome et Rhône Aircraft air-cooled radial piston engines 1930s aircraft piston engines Snecma aircraft engines Mercury (element) 92 Octane B.M.E.P. Breguet Br 500 Colmar Gnome-Rhône 100 octane
sameAs	SNECMA 14R SNECMA 14R SNECMA 14R SNECMA 14R SNECMA 14R
specfuelcon	0.292000 (xsd:double)
specpower	31.850000 (xsd:double)
supercharger	Gear-driven 2-speed supercharger at 6.5:1 and 9.0:1 ratios (en)
valvetrain	Single inlet and exhaust valves operated by rockers and pushrods (en)
dbp:wikiPageUsesTemplate	dbt:Commons_category dbt:Convert dbt:Reflist dbt:Aircontent dbt:Infobox_aircraft_engine dbt:Pistonspecs dbt:Gnome-Rhône_aeroengines dbt:Snecma_aeroengines
thumbnail	wiki-commons:Special:FilePath/Gnome_et_Rhône_14R_04-05_-_Musée_Safran_07.jpg?width=300
national origin	France
manufacturer	SNECMA Gnome-Rhône
power	Take-off: at 2,600 rpm at Hg boost with 100 octane fuel Military, low: at 2,600 rpm at Military, high: at 2,600 rpm at Normal, low: at 2,400 rpm at *Normal, high: at 2,400 rpm at (en)
type	14 (xsd:integer)
has abstract	The SNECMA 14R was a 14-cylinder two-row air-cooled radial engine developed in France just prior to the start of World War II from the Gnome-Rhône 14N. The 14N radial engine was itself an improved version of the popular pre-war Gnome-Rhône 14K Mistral Major series; designed and manufactured by Gnome et Rhône, a major French aircraft engine manufacturer whose origins pre-date the First World War. The improved 14R was initially known as the Gnome-Rhône 14P and then the Gnome-Rhône 14R. There were several improvements such as the introduction of a longer crankshaft and crankcase with a centre bearing, an increase in cylinder capacity, and a two-speed compressor. These changes allowed the engine to deliver 1,400hp at take-off and 1,300hp at 1,500m (1st gear) and 1200hp at 4000m (2nd gear). This came at the cost of a much increased total weight. It was expected that further development, such as the introduction of higher grade fuels, would lead to a power output of 1,660hp at low altitude. With the Fall of France, engine development was stopped under the occupation. After the war, development recommenced; however production of this engine after 1945 was transferred to the newly formed SNECMA and the engine was renamed the SNECMA 14R. (en)
components other	Starter: Air equipment electric inertia starter * Ignition: 2 x R.B. magnetos, 2 x short reach spark plugs per cylinder fed by a shielded ignition harness. (en)
compression	6.800000 (xsd:double)
coolingsystem	Air-cooled with baffles (en)
developed from	Gnome-Rhône 14N
fuelsystem	1 (xsd:integer)
fueltype	92 (xsd:integer)
general other	Frontal Area: (en)
lists	* List of aircraft engines (en)
major applications	Breguet Br 500 Colmar
oilcon	0.006700 (xsd:double)
oilsystem	Pressure fed at (en)
performance other	14 (xsd:integer)
power/weight	1.494000 (xsd:double)
reduction gear	Planetary / epicyclic bevel reduction gearing at 0.67:1 ratio (en)
prov:wasDerivedFrom	wikipedia-en:SNECMA_14R?oldid=1111487863&ns=0
page length (characters) of wiki page	6466 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:SNECMA_14R
is Link from a Wikipage to another Wikipage of	List of aircraft engines SNECMA 14R-24 SNCAC NC.211 Cormoran Lioré et Olivier LeO 45 SNCAC NC.1070 Gnome-Rhône 14R-04 Gnome-Rhône 14R-05 Gnome-Rhône 14R Gnome-Rhône 14R-26 Gnome-Rhône 14R-27 Gnome-Rhône 14R-28 Gnome-Rhône 14R-29 Gnome-Rhône 28T-1 Gnome et Rhône 14R Gnome et Rhône 14Rsd
is Wikipage redirect of	SNECMA 14R-24 Gnome-Rhône 14R-04

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