About: SNECMA Régnier 4L

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The SNECMA-Régnier 4L is a French four cylinder air-cooled inverted inline piston engine, introduced shortly after the end of World War II.

Attributes	Values
rdfs:label	SNECMA Régnier 4L (en)
rdfs:comment	The SNECMA-Régnier 4L is a French four cylinder air-cooled inverted inline piston engine, introduced shortly after the end of World War II. (en)
foaf:depiction
dcterms:subject	1940s aircraft piston engines Inverted aircraft piston engines Air-cooled aircraft piston engines Snecma aircraft engines
Wikipage page ID	45155469 (xsd:integer)
Wikipage revision ID	1101671844 (xsd:integer)
Link from a Wikipage to another Wikipage	List of aircraft engines Boisavia Anjou Boisavia Mercurey Cylinder (engine) Cylinder head De Havilland Gipsy Major De Havilland Gipsy Six Duralumin Inline engine (aeronautics) SNECMA Connecting rod Occupation of France 1940s aircraft piston engines Inverted aircraft piston engines Leduc RL.21 Air-cooled aircraft piston engines France Brochet MB.110 Nord 3202 Nord Norécrin Farman F.500 Crankcase Crankshaft Aubert Cigale LIBIS KB-6 Dry weight Snecma aircraft engines Guerchais-Roche T.35 World War II Nord NC.850 Nord Norélan Straight engine SNCASE SE-2300 Régnier Motor Company Piston engine Aluminium-bronze
sameAs	SNECMA Régnier 4L SNECMA Régnier 4L SNECMA Régnier 4L SNECMA Régnier 4L
valvetrain	1 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Columns-list dbt:Commons_category dbt:Convert dbt:Reflist dbt:Short_description dbt:Aircontent dbt:Infobox_Aircraft_Engine dbt:Pistonspecs dbt:Regnier_aeroengines
thumbnail	wiki-commons:Special:FilePath/Espace_Air_Passion_-_SNECMA-Régnier_4L08_-1.jpg?width=300
national origin	France
length	over starter (en)
manufacturer	SNECMA
power	Maximum continuous at 2,280 rpm; take-off at 2,340 rpm (en)
ref	Jane's All the World's Aircraft 1956-57. (en)
type	4 (xsd:integer) Four cylinder in-line inverted air-cooled piston engine (en)
weight	dry (en)
has abstract	The SNECMA-Régnier 4L is a French four cylinder air-cooled inverted inline piston engine, introduced shortly after the end of World War II. (en)
compression	6.200000 (xsd:double)
coolingsystem	Air; finned cylinder heads (en)
developed from	1936 (xsd:integer)
first run	c. 1945 (en)
fuelcon	per hour at maximum cruising power (en)
fuelsystem	Zenith 1DC carburettor on port side, fed by 2 Guyot K or O pumps.2 BG plugs/cylinder, BG dual magneto (en)
lists	*List of aircraft engines (en)
major applications	Nord NC.850
oilsystem	Pressure lubrication from engine driven pump; 2 scavenge pumps. (en)
prov:wasDerivedFrom	wikipedia-en:SNECMA_Régnier_4L?oldid=1101671844&ns=0
page length (characters) of wiki page	8144 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:SNECMA_Régnier_4L
is Link from a Wikipage to another Wikipage of	List of aircraft engines SNECMA-Regnier 4L SNECMA-Régnier 4LO SNECMA 4L SNECMA 4L-00 SNECMA 4L-02 SNECMA 4L-04 SNECMA 4L-06 SNECMA 4L-08 Safran Aircraft Engines Leduc RL.21 SNECMA Regnier 4L SNECMA Régnier 4L-02 Régnier Motor Company Régnier 4L Régnier 4LO Regnier 4L Regnier 4L-02 Regnier 4L-22

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