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Statements

Subject Item
dbr:Continental_O-200
rdf:type
yago:Object100002684 yago:Instrumentality103575240 yago:Motor103789946 yago:WikicatContinentalAircraftEngines yago:Whole100003553 yago:Device103183080 yago:WikicatBoxerEngines yago:Machine103699975 yago:Artifact100021939 yago:Engine103287733 yago:PhysicalEntity100001930 yago:AircraftEngine102687423
rdfs:label
Continental O-200 Continental O-200 Continental O-200 Continental O-200 Continental O-200
rdfs:comment
Les Continental C90 et O-200 forment une famille de moteurs d'avion quatre cylindres à plat refroidis par air et à entraînement direct ; d'une cylindrée de 3,29 ℓ (environ 200 pouces cubes d'où le nom du moteur), le moteur génère entre 67 et 75 kW (90 à 100 chevaux environ). Construit par Continental Motors, ces moteurs sont communs parmi les aéronefs d'aviation légère conçus aux États-Unis, notamment les premiers Piper PA-18 Super Cub, le Champion 7EC ou le Cessna 150. Continental C90 und O-200 sind eine Familie von luftgekühlten Vierzylinderboxermotoren für Kleinflugzeuge mit 3,29 Litern Hubraum und einer Leistung zwischen 90 PS (66 kW) und 100 PS (74 kW). Die Motoren wurden von Continental Motors gebaut und finden Anwendung in vielen US-amerikanischen Flugzeugmodellen wie der Piper PA-18 Super Cub, der , der Alon Aircoupe und der Cessna 150. Il Continental O-200 (designazione aziendale Continental C90) e i suoi derivati formano una famiglia di motori aeronautici a cilindri contrapposti 4 cilindri raffreddati ad aria, prodotto dagli anni quaranta dall'azienda statunitense . La sigla O-200 identifica il modello in base alla sua architettura a cilindri contrapposti (Opposed) ed alla cilindrata espressa in pollici cubi, circa 200 in³. Deriva dal precedente O-190, mantenendo gli stessi cilindri, ma con la corsa aumentata di 1/4 di pollice. The Continental C90 and O-200 are a family of air-cooled, horizontally opposed, four-cylinder, direct-drive aircraft engines of 201 in³ (3.29 L) displacement, producing between 90 and 100 horsepower (67 and 75 kW). Built by Continental Motors these engines are used in many light aircraft designs of the United States, including the early Piper PA-18 Super Cub, the Champion 7EC, the Alon Aircoupe, and the Cessna 150. O Continental C90 e o O-200 são uma família de motores de aeronaves de quatro cilindros, refrigerados a ar, horizontalmente opostos e de transmissão direta de 201 in³ (3,29 L) de cilindrada, produzindo entre 90 e 100 cavalos de potência (67 e 75 kW). Construídos pela Continental Motors, esses motores são usados em muitos projetos de aeronaves leves dos Estados Unidos, incluindo o Piper PA-18 Super Cub, o , o e o Cessna 150.
foaf:depiction
n11:Continental_O-200-A_C150H_left_3-quarter_eye-level.jpg n11:Continental_O-200-A_C150H_left_side_above.jpg n11:ContinentalIOL200.jpg n11:Continental_O-200-A_C150H_left_3-quarter_above.jpg n11:Continental_O-200D.jpg n11:Cessna150MC-GYFT.jpg n11:Continental-O-200AF.jpg
dcterms:subject
dbc:Boxer_engines dbc:1940s_aircraft_piston_engines dbc:Continental_aircraft_engines
dbo:wikiPageID
1013385
dbo:wikiPageRevisionID
1083222068
dbo:wikiPageWikiLink
dbc:Continental_aircraft_engines dbr:Robin_DR.200 n5:ContinentalIOL200.jpg dbr:Cessna_140 n5:Continental-O-200AF.jpg dbr:Cessna_162_Skycatcher dbr:Sharp_Nemesis dbr:Ignition_magneto dbr:List_of_Louis_Blériot_medal_winners dbr:Williams_W-17_Stinger dbr:Piper_PA-18 n5:Continental_O-200D.jpg dbr:Falconar_Minihawk dbr:Reciprocating_engine dbr:Supplemental_Type_Certificate dbr:Ignition_system dbr:Malmö_MFI-9 n5:Cessna150MC-GYFT.jpg dbr:AMD_Zodiac dbr:Victa_Airtourer_100 dbr:Miller-Bohannon_JM-2_Pushy_Galore dbr:Aircraft_engine dbr:Fisher_Celebrity dbr:Luscombe_8 dbr:Bölkow_Bo_208 dbr:Miller_JM-2 dbr:Fleet_Model_80_Canuck dbr:Bölkow_BO_208 dbr:Piston dbr:QAC_Quickie_Q2 dbr:Four-stroke_cycle dbr:Coupé-Aviation_JC-01 dbr:Poppet_valve dbr:Zenith_STOL_CH_750 dbr:Fuel_injection dbr:Zodiac_601_HD dbr:VSR_SR-1_Snoshoo dbr:Piper_PA-11 dbr:Reims_Aviation dbr:Spark_plug dbr:Air-fuel_ratio dbr:Piper_PA-18_Super_Cub dbr:Engine_cooling dbr:Cessna_150 dbr:Continental_O-300 dbr:Continental_A65 dbr:Pottier_P.60_Minacro dbr:Bede_BD-12 dbr:Anglin_J6_Karatoo dbr:Variable-pitch_propeller_(aeronautics) dbr:Civil_Aviation_Department_MG-1 dbr:Barbaro_RB-50 dbr:Druine_Condor dbr:ERCO_Ercoupe dbr:Aeronca_Champ dbr:Bearhawk_LSA dbr:Piper_J-3 dbr:Cylinder_(engine) dbr:Bushcaddy_R-120 dbr:Rotax_912 dbr:Vashon_Ranger_R7 dbr:World_Aircraft_Spirit dbr:Falconar_F11_Sporty dbr:Aeronca_L-16 dbr:Light-sport_aircraft dbr:Tractor_configuration dbr:Avgas dbc:Boxer_engines dbr:Aeronca_Champion dbr:Flaeming_Air_FA_04_Peregrine dbr:Mignet_Pou-du-Ciel dbr:Taylorcraft_F-19_Sportsman dbr:Beagle_Pup dbr:American_Homebuilts_John_Doe dbr:Jodel_D11 dbr:Exhaust_system dbr:Wet_sump dbr:General_aviation dbc:1940s_aircraft_piston_engines dbr:ARV_Griffin dbr:Time_between_overhaul dbr:Cassutt_Special dbr:Continental_A-65 dbr:Fisher_Dakota_Hawk dbr:Interstate_Cadet dbr:Flat-4 dbr:Morane-Saulnier_MS-880 dbr:Rolls-Royce_Limited dbr:Franklin_O-200 dbr:Lycoming_O-235 dbr:Socata_Rallye dbr:List_of_aircraft_engines dbr:Warner_Sportster dbr:CubCrafters_Carbon_Cub_EX dbr:Pusher_configuration dbr:Dry_weight dbr:Rutan_VariEze dbr:Rutan_Voyager dbr:Ryson_ST-100_Cloudster dbr:CubCrafters_CC11-100_Sport_Cub_S2 dbr:Carburetor dbr:RLU-1_Breezy dbr:VTOL_Aircraft_Phillicopter dbr:Continental_O-190 dbr:Continental_O-240 dbr:Rokospol_Via dbr:Teledyne_Continental_Motors dbr:Nexaer_LS1 dbr:Thorp_T-211 dbr:Updraft_carburetor dbr:Jodel_DR1050_Excellence dbr:Intake
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freebase:m.03z6c7 dbpedia-fr:Continental_O-200 dbpedia-de:Continental_O-200 wikidata:Q3688932 dbpedia-pt:Continental_O-200 n22:3PszL dbpedia-it:Continental_O-200 yago-res:Continental_O-200
dbp:similarEngines
* Franklin O-200 * Lycoming O-235 * Rotax 912
dbp:specpower
0.5
dbp:stroke
3.88
dbp:valvetrain
Hydraulic lifters, two pushrod-actuated valves—one intake, one exhaust—per cylinder
dbp:wikiPageUsesTemplate
dbt:Convert dbt:Columns-list dbt:Aircontent dbt:Commons_category dbt:Frac dbt:Pistonspecs dbt:Infobox_Aircraft_Engine dbt:Reflist dbt:US_military_piston_aeroengines dbt:Teledyne_Continental_aeroengines dbt:Multiple_image
dbo:thumbnail
n11:Continental_O-200-A_C150H_left_3-quarter_above.jpg?width=300
dbp:nationalOrigin
United States
dbp:align
right
dbp:caption
Two views of an O-200-A in a Cessna 150H
dbp:direction
vertical
dbp:height
23.18
dbp:image
Continental O-200-A C150H left side above.JPG Continental O-200-A C150H left 3-quarter eye-level.JPG
dbp:length
28.53
dbp:manufacturer
dbr:Teledyne_Continental_Motors
dbp:power
100.0
dbp:related
* Continental A-65 * Continental O-300
dbp:type
dbr:Piston dbr:Aircraft_engine Four-cylinder air-cooled horizontally opposed piston engine
dbp:weight
170.18
dbp:width
31.56 220
dbo:abstract
Les Continental C90 et O-200 forment une famille de moteurs d'avion quatre cylindres à plat refroidis par air et à entraînement direct ; d'une cylindrée de 3,29 ℓ (environ 200 pouces cubes d'où le nom du moteur), le moteur génère entre 67 et 75 kW (90 à 100 chevaux environ). Construit par Continental Motors, ces moteurs sont communs parmi les aéronefs d'aviation légère conçus aux États-Unis, notamment les premiers Piper PA-18 Super Cub, le Champion 7EC ou le Cessna 150. Bien que le O-200 ait succédé au C90 et que les avions conçus autour du O-200 aient vu leur production arriver à son terme dans les années 1980, la publication, en 2004, par l'Administration fédérale de l'Aviation des États-Unis d’une nouvelle réglementation posant la définition d'une catégorie appelée light sport aircraft a suscité un regain d'intérêt pour le O-200. Le standard light-sport aircraft définit un petit aéronef mono ou biplace pour lequel un O-200 est parfaitement en adéquation. O Continental C90 e o O-200 são uma família de motores de aeronaves de quatro cilindros, refrigerados a ar, horizontalmente opostos e de transmissão direta de 201 in³ (3,29 L) de cilindrada, produzindo entre 90 e 100 cavalos de potência (67 e 75 kW). Construídos pela Continental Motors, esses motores são usados em muitos projetos de aeronaves leves dos Estados Unidos, incluindo o Piper PA-18 Super Cub, o , o e o Cessna 150. Embora o C90 tenha sido substituído pelo O-200, e muitos dos projetos que utilizam o O-200 tenham saído de produção em 1980, com a publicação de 2004 dos regulamentos de aeronaves leves da "Federal Aviation Administration" (FAA) dos Estados Unidos, veio um ressurgimento da demanda pelo O-200. O padrão para aeronaves esportivas leves é para aeronaves pequenas e simples de um ou dois lugares, para as quais o O-200 é adequado. Il Continental O-200 (designazione aziendale Continental C90) e i suoi derivati formano una famiglia di motori aeronautici a cilindri contrapposti 4 cilindri raffreddati ad aria, prodotto dagli anni quaranta dall'azienda statunitense . La sigla O-200 identifica il modello in base alla sua architettura a cilindri contrapposti (Opposed) ed alla cilindrata espressa in pollici cubi, circa 200 in³. Deriva dal precedente O-190, mantenendo gli stessi cilindri, ma con la corsa aumentata di 1/4 di pollice. Il motore è costruito con un carter in lega leggera, sul quale sono flangiati singolarmente i cilindri, con canne in acciaio e testate in alluminio filettate direttamente sulle canne. L'alimentazione è a singolo carburatore (eccetto alcune versioni del C-90 predisposte per l'iniezione), la distribuzione ad aste e bilancieri con albero a camme nel basamento, punterie idrauliche e due valvole per cilindro (OHV). L'accensione è a doppio magnete, con due candele per cilindro. La trasmissione del moto tra albero motore, albero a camme e accessori (magneti, alternatore, motorino di avviamento ecc.) avviene totalmente mediante ingranaggi contenuti nella scatola accessori integrale nella parte posteriore del motore. Nella parte frontale è presente la predisposizione per la pompa a vuoto (per alimentazione degli strumenti giroscopici) e la pompa meccanica della benzina, azionati rispettivamente da un ingranaggio conico ed un eccentrico presenti sull'albero a camme. La serie O-200 copre la fascia tra i 90 e i 100 hp (67-75 kW). Il C-90 esprime la sua massima potenza di 95 cavalli al decollo ad un regime di 2625 RPM, e la potenza continuativa di 90 cavalli a 2475 RPM, mentre l'O-200 esprime la sua potenza massima continuativa di 100 cavalli ad un regime di 2750 RPM. Il motore nasce per la benzina avio 80/87 ottani, ma può funzionare senza problemi anche con l'Avgas 100 LL, e può essere certificato per la benzina da autotrazione. Il tempo di funzionamento tra le revisioni è 1800 ore. Continental C90 und O-200 sind eine Familie von luftgekühlten Vierzylinderboxermotoren für Kleinflugzeuge mit 3,29 Litern Hubraum und einer Leistung zwischen 90 PS (66 kW) und 100 PS (74 kW). Die Motoren wurden von Continental Motors gebaut und finden Anwendung in vielen US-amerikanischen Flugzeugmodellen wie der Piper PA-18 Super Cub, der , der Alon Aircoupe und der Cessna 150. Obwohl der C90 durch den O-200 verdrängt wurde und viele der Flugzeuge, in denen der O-200 eingesetzt wurde, seit 1980 nicht mehr produziert werden, entstand mit Einführung der Light-Sport-Aircraft-Klasse durch die US-amerikanische Federal Aviation Administration eine neue Nachfrage nach dem O-200, der für diese Flugzeugklasse gut geeignet ist. The Continental C90 and O-200 are a family of air-cooled, horizontally opposed, four-cylinder, direct-drive aircraft engines of 201 in³ (3.29 L) displacement, producing between 90 and 100 horsepower (67 and 75 kW). Built by Continental Motors these engines are used in many light aircraft designs of the United States, including the early Piper PA-18 Super Cub, the Champion 7EC, the Alon Aircoupe, and the Cessna 150. Though the C90 was superseded by the O-200, and many of the designs utilizing the O-200 had gone out of production by 1980, with the 2004 publication of the United States Federal Aviation Administration light-sport aircraft regulations came a resurgence in demand for the O-200. The light-sport aircraft standard is for small, simple single- and two-seat aircraft for which the O-200 is well-suited.
dbp:bore
4.06
dbp:compression
7
dbp:coolingsystem
Air-cooled
dbp:developedFrom
dbr:Continental_O-190
dbp:displacement
201.0
dbp:firstRun
1947
dbp:fuelsystem
Updraft carburetor with manual mixture control
dbp:fueltype
80
dbp:lists
* List of aircraft engines
dbp:majorApplications
ERCO Ercoupe dbr:Cessna_140 Cessna 162 Skycatcher Cessna 150 RLU-1 Breezy
dbp:oilsystem
6
n25:weight
0.5600000000000001
dbp:produced
-1980.0 2004
gold:hypernym
dbr:Family
prov:wasDerivedFrom
wikipedia-en:Continental_O-200?oldid=1083222068&ns=0
dbo:wikiPageLength
18320
foaf:isPrimaryTopicOf
wikipedia-en:Continental_O-200