About: Lockheed CL-475

Property	Value
dbo:abstract	سي إل-475 (CL-475) طائرة مروحية بمقعد واحد طورتها شركة لوكهيد لاستكشاف امكانيات تكنولوجيا المحركات الدوارة الجامدة. تستخدم محرك أساسي بثلاث مراوح دوارة ومحرك خلفي مثبت على الذيل دوار. بني نموذج واحد منها فقط. (ar) The Lockheed CL-475 is a two-seat, single-engine light helicopter developed by Lockheed to explore rigid rotor technology. The CL-475 has a three-bladed main rotor and a two-bladed tail rotor. Only one was built. (en) Lockheed CL-475 (pendaftaran N6940C) adalah helikopter ringan eksperimental dua-kursi, bermesin tunggal, yang dikembangkan oleh Lockheed untuk mengeksplorasi teknologi rotor rigid (kaku). CL-475 memiliki rotor utama berbilah tiga dan rotor ekor berbilah dua. Hanya satu dibangun. (in)
dbo:manufacturer	dbr:Lockheed_Corporation
dbo:numberBuilt	1 (xsd:nonNegativeInteger)
dbo:thumbnail	wiki-commons:Special:FilePath/Lockheed_CL-475.jpg?width=300
dbo:wikiPageID	23581855 (xsd:integer)
dbo:wikiPageLength	7653 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID	994144509 (xsd:integer)
dbo:wikiPageWikiLink	dbr:Rosamond_Lake dbr:Juan_de_la_Cierva dbr:List_of_rotorcraft dbr:Edwards_Air_Force_Base dbr:Mojave_Desert dbr:United_States_Army_Aviation_Museum dbr:Lockheed_Corporation dbr:Lockheed_XH-51 dbr:Lycoming_O-360 dbc:Single-engined_piston_helicopters dbc:1950s_United_States_helicopters dbr:AH-56_Cheyenne dbc:Rigid_rotor_helicopters dbr:Irv_Culver dbc:Aircraft_first_flown_in_1959 dbc:1950s_United_States_experimental_aircraft dbc:Lockheed_aircraft dbr:National_Air_and_Space_Museum
dbp:ceilingFt	2000 (xsd:integer)
dbp:ceilingM	610 (xsd:integer)
dbp:civilRegistration	N6940C (en)
dbp:crew	2 (xsd:integer)
dbp:designer	Irven Culver (en)
dbp:emptyWeightKg	737 (xsd:integer)
dbp:emptyWeightLb	1625 (xsd:integer)
dbp:eng1Hp	140 (xsd:integer)
dbp:eng1Kw	104 (xsd:integer)
dbp:eng1Name	Lycoming VO-360-A1A four-cylinder air-cooled piston engine (en)
dbp:eng1Number	1 (xsd:integer)
dbp:fate	In storage at United States Army Aviation Museum (en)
dbp:firstFlight	1959-11-02 (xsd:date)
dbp:grossWeightKg	907 (xsd:integer)
dbp:grossWeightLb	2000 (xsd:integer)
dbp:heightFt	9 (xsd:integer)
dbp:heightIn	3 (xsd:integer)
dbp:heightM	2.820000 (xsd:double)
dbp:lists	* List of rotorcraft (en)
dbp:manufacturer	dbr:Lockheed_Corporation
dbp:maxSpeedKmh	145 (xsd:integer)
dbp:maxSpeedMph	90 (xsd:integer)
dbp:nationalOrigin	United States (en)
dbp:numberBuilt	1 (xsd:integer)
dbp:primeUnits?_	imp (en)
dbp:rangeKm	120 (xsd:integer)
dbp:rangeMiles	75 (xsd:integer)
dbp:related	* Lockheed XH-51 (en)
dbp:rotDiaFt	32 (xsd:integer)
dbp:rotDiaIn	0 (xsd:integer)
dbp:rotDiaM	9.750000 (xsd:double)
dbp:rotNumber	1 (xsd:integer)
dbp:status	Retired (en)
dbp:type	Experimental helicopter (en)
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dcterms:subject	dbc:Single-engined_piston_helicopters dbc:1950s_United_States_helicopters dbc:Rigid_rotor_helicopters dbc:Aircraft_first_flown_in_1959 dbc:1950s_United_States_experimental_aircraft dbc:Lockheed_aircraft
gold:hypernym	dbr:Helicopter
rdf:type	owl:Thing schema:Product dbo:MeanOfTransportation wikidata:Q11436 yago:WikicatSingle-enginedPistonHelicopters yago:Aircraft102686568 yago:Artifact100021939 yago:Conveyance103100490 yago:Craft103125870 yago:Heavier-than-airCraft103510583 yago:Helicopter103512147 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 dbo:Aircraft yago:Vehicle104524313 yago:Whole100003553 yago:WikicatRigidRotorHelicopters umbel-rc:Model_airplane
rdfs:comment	سي إل-475 (CL-475) طائرة مروحية بمقعد واحد طورتها شركة لوكهيد لاستكشاف امكانيات تكنولوجيا المحركات الدوارة الجامدة. تستخدم محرك أساسي بثلاث مراوح دوارة ومحرك خلفي مثبت على الذيل دوار. بني نموذج واحد منها فقط. (ar) The Lockheed CL-475 is a two-seat, single-engine light helicopter developed by Lockheed to explore rigid rotor technology. The CL-475 has a three-bladed main rotor and a two-bladed tail rotor. Only one was built. (en) Lockheed CL-475 (pendaftaran N6940C) adalah helikopter ringan eksperimental dua-kursi, bermesin tunggal, yang dikembangkan oleh Lockheed untuk mengeksplorasi teknologi rotor rigid (kaku). CL-475 memiliki rotor utama berbilah tiga dan rotor ekor berbilah dua. Hanya satu dibangun. (in)
rdfs:label	لوكهيد سي إل-475 (ar) Lockheed CL-475 (in) Lockheed CL-475 (en)
owl:sameAs	freebase:Lockheed CL-475 yago-res:Lockheed CL-475 wikidata:Lockheed CL-475 dbpedia-ar:Lockheed CL-475 dbpedia-fa:Lockheed CL-475 dbpedia-id:Lockheed CL-475 https://global.dbpedia.org/id/4qnB5
prov:wasDerivedFrom	wikipedia-en:Lockheed_CL-475?oldid=994144509&ns=0
foaf:depiction	wiki-commons:Special:FilePath/Lockheed_CL-475.jpg
foaf:isPrimaryTopicOf	wikipedia-en:Lockheed_CL-475
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