Walter Regulus (original) (raw)

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dbo:abstract والتر ريجولس هو محرك طائرة شعاعي تشيكوسلوفاكي مكون من 5 أسطوانات، ويُبرد بالهواء. صُنع المحرك لتشغيل الطائرات الخفيفة، وعمل لأول مرة في عام 1934، وأنتج قدرة 250 حصاناً (186 كيلو وات). (ar) Walter Regulus, Walter Regulus II a Walter Regulus III (II-R) byly československé pětiválcové zážehové vzduchem chlazené hvězdicové motory. Walter Regulus byl vyvinut počátkem 30. let 20. století a byl vyráběn Akciovou společností Walter, továrnou na automobily a letecké motory v Praze-Jinonicích. Dočkal se dalších modernizací na verzi Regulus II (1934) a Regulus III (1935). Walter Regulus je vystaven v expozici Leteckého muzea ve Kbelích. Walter Regulus (1930), zadní pohled (cs) Der Walter Regulus ist ein tschechoslowakischer Flugmotor des in Prag ansässigen Herstellers Walter Motors a.s. aus dem Jahr 1931. (de) The Walter Regulus was a Czechoslovakian five-cylinder, air-cooled radial engine for powering light aircraft that first ran in 1934. The engine produced 186 kW (250 hp). (en)
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dbo:wikiPageLength 3766 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID 1065047952 (xsd:integer)
dbo:wikiPageWikiLink dbr:List_of_aircraft_engines dbr:Benzine dbr:Horsepower dbr:Radial_engine dbr:Prague_Aviation_Museum,_Kbely dbr:Armstrong_Siddeley_Mongoose dbr:Benzole dbr:Walter_Aircraft_Engines dbr:Aircraft dbr:Aircraft_engine dbr:Czechoslovakia dbc:Aircraft_air-cooled_radial_piston_engines dbc:1930s_aircraft_piston_engines dbc:Walter_aircraft_engines dbr:Kinner_R-5
dbp:compression 5.700000 (xsd:double)
dbp:coolingsystem Air-cooled (en)
dbp:firstRun 1934 (xsd:integer)
dbp:fuelsystem One Zenith double 50DCJ carburettor (en)
dbp:fueltype 3050.0 (dbd:second)
dbp:lists *List of aircraft engines (en)
dbp:manufacturer dbr:Walter_Aircraft_Engines
dbp:nationalOrigin dbr:Czechoslovakia
dbp:oilsystem dry sump, pressure system (en)
dbp:power Normal: at 1,800 rpm; Maximum (en)
dbp:ref Jane's all the World's Aircraft 1931 (en)
dbp:similarEngines *Armstrong Siddeley Mongoose *Kinner R-5 (en)
dbp:type 5 (xsd:integer) dbr:Radial_engine dbr:Aircraft_engine
dbp:valvetrain One intake and one exhaust valve per cylinder operated by pushrods and rockers (en)
dbp:wikiPageUsesTemplate dbt:Commons_category dbt:Cvt dbt:Reflist dbt:Short_description dbt:Aircontent dbt:Infobox_Aircraft_Engine dbt:Pistonspecs dbt:Walter_aeroengines
dct:subject dbc:Aircraft_air-cooled_radial_piston_engines dbc:1930s_aircraft_piston_engines dbc:Walter_aircraft_engines
gold:hypernym dbr:Engine
rdf:type dbo:Software yago:WikicatWalterAircraftEngines 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:comment والتر ريجولس هو محرك طائرة شعاعي تشيكوسلوفاكي مكون من 5 أسطوانات، ويُبرد بالهواء. صُنع المحرك لتشغيل الطائرات الخفيفة، وعمل لأول مرة في عام 1934، وأنتج قدرة 250 حصاناً (186 كيلو وات). (ar) Walter Regulus, Walter Regulus II a Walter Regulus III (II-R) byly československé pětiválcové zážehové vzduchem chlazené hvězdicové motory. Walter Regulus byl vyvinut počátkem 30. let 20. století a byl vyráběn Akciovou společností Walter, továrnou na automobily a letecké motory v Praze-Jinonicích. Dočkal se dalších modernizací na verzi Regulus II (1934) a Regulus III (1935). Walter Regulus je vystaven v expozici Leteckého muzea ve Kbelích. Walter Regulus (1930), zadní pohled (cs) Der Walter Regulus ist ein tschechoslowakischer Flugmotor des in Prag ansässigen Herstellers Walter Motors a.s. aus dem Jahr 1931. (de) The Walter Regulus was a Czechoslovakian five-cylinder, air-cooled radial engine for powering light aircraft that first ran in 1934. The engine produced 186 kW (250 hp). (en)
rdfs:label والتر ريجولس (ar) Walter Regulus (cs) Walter Regulus (de) Walter Regulus (en)
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