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Statements

Subject Item
dbr:Siemens-Halske_Sh_22
rdf:type
yago:WikicatRadialEngines yago:Motor103789946 yago:Machine103699975 yago:Object100002684 yago:Internal-combustionEngine103579982 yago:RadialEngine104040373 yago:Engine103287733 yago:PhysicalEntity100001930 dbo:Software yago:WikicatSiemens-HalskeAircraftEngines yago:Instrumentality103575240 yago:AircraftEngine102687423 yago:HeatEngine103507963 yago:Artifact100021939 yago:Whole100003553 yago:Device103183080
rdfs:label
Siemens-Halske Sh 22 Siemens-Halske Sh 22 Siemens-Halske Sh 22 Siemens & Halske Sh 22
rdfs:comment
El Siemens-Halske Sh 22 (també conegut com a SAM 22) va ser un motor radial de nou cilindres fabricat per Siemens & Halske a Alemanya a la dècada de 1930. Després de la reorganització del seu fabricant i del canvi en la nomenclatura militar, el motor va passar a anomenar-se Bramo 322. Siemens & Halske Sh 22 — немецкий поршневой звездообразный 9-цилиндровый авиадвигатель воздушного охлаждения, разработанный в 1928 году. Il Siemens-Halske Sh 22, citato anche come SAM 22 o semplicemente Siemens Sh 22, era un motore aeronautico radiale a 9 cilindri raffreddato ad aria prodotto dall'azienda tedesca Siemens-Schuckertwerke negli anni trenta. In una sua versione intermedia, la Sh 22B (o SAM 22B), prodotta nei primi anni trenta era caratterizzata dall'adozione di un compressore centrifugo a singolo stadio e di un riduttore epicicloidale interposto al mozzo dell'elica. La potenza erogata di questa versione, grazie ai miglioramenti introdotti dalla Bramo, risultava di 660 PS (485 kW). The Siemens-Halske Sh 22 (also known as SAM 22) was a nine-cylinder aircraft radial engine manufactured by Siemens & Halske in Germany in the 1930s. Following the reorganization of its manufacturer and change in military nomenclature, the engine became known as the Bramo 322.
dcterms:subject
dbc:Siemens-Halske_aircraft_engines dbc:1930s_aircraft_piston_engines dbc:Aircraft_air-cooled_radial_piston_engines
dbo:wikiPageID
19118890
dbo:wikiPageRevisionID
1065060582
dbo:wikiPageWikiLink
dbr:Radial_engine dbr:Junkers_Ju_86 dbr:Gasoline dbr:Bristol_Jupiter_IV dbr:Carburetor dbr:Heinkel_He_46 dbr:Fieseler_Fi_98 dbr:Bramo_323 dbr:Dornier_Do_19 dbr:Germany dbr:Overhead_valve dbr:Epicyclic_gearing dbr:Junkers_W_34 dbr:Siemens_&_Halske dbc:Siemens-Halske_aircraft_engines dbr:Centrifugal_type_supercharger dbr:Farman_Aviation_Works dbr:Henschel_Hs_122 dbr:Reich_Air_Ministry dbr:87_octane dbc:1930s_aircraft_piston_engines dbc:Aircraft_air-cooled_radial_piston_engines
owl:sameAs
dbpedia-ca:Siemens-Halske_Sh_22 n10:Siemens-Halske_Sh_22 wikidata:Q749922 freebase:m.04jf775 dbpedia-it:Siemens-Halske_Sh_22 n21:4uXdV dbpedia-ru:Siemens_&_Halske_Sh_22 yago-res:Siemens-Halske_Sh_22
dbp:specfuelcon
at max continuous
dbp:supercharger
Single-speed centrifugal type supercharger running at 6.25:1
dbp:valvetrain
Two overhead valves per cylinder driven by pushrods and rockers
dbp:wikiPageUsesTemplate
dbt:Infobox_Aircraft_Engine dbt:Reflist dbt:Cvt dbt:Pistonspecs dbt:Siemens-Halske_aeroengines
dbp:nationalOrigin
dbr:Germany
dbp:manufacturer
dbr:Siemens_&_Halske
dbp:power
:* at 2,150 rpm at sea level :* at 2,080 rpm at sea level :* at 2,000 rpm at sea level
dbp:ref
Aviacionnye motory voennykh vozdushnykh sil inostrannykh gosudarstv, Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944
dbp:type
dbr:Radial_engine 9
dbp:weight
dry, unequipped :::: wet, equipped
dbo:abstract
El Siemens-Halske Sh 22 (també conegut com a SAM 22) va ser un motor radial de nou cilindres fabricat per Siemens & Halske a Alemanya a la dècada de 1930. Després de la reorganització del seu fabricant i del canvi en la nomenclatura militar, el motor va passar a anomenar-se Bramo 322. Va ser el resultat d'una sèrie de modificacions al disseny original del Bristol Jupiter IV, que Siemens va llicenciar el 1929. Les primeres modificacions van ser per "germanitzar" les dimensions, produint el Sh 20 i el Sh 21. El disseny va ser aleshores modificat ampliant els pistons per produir el Sh 22 de 950 CV (708 kW) el 1930. A mitjans dels anys trenta, el RLM va racionalitzar la denominació del motor, i a Bramo se li va donar el bloc de números 300, el Sh 14 i el Sh 22 es van reanomenar Bramo 314 i 322 respectivament. Es va convertir en la base per al disseny del Bramo 323. Il Siemens-Halske Sh 22, citato anche come SAM 22 o semplicemente Siemens Sh 22, era un motore aeronautico radiale a 9 cilindri raffreddato ad aria prodotto dall'azienda tedesca Siemens-Schuckertwerke negli anni trenta. Sviluppo del britannico Bristol Jupiter, come gli altri motori della gamma l'azienda tedesca, che era controllata dalla Siemens-Halske AG, utilizzava il marchio dell'azienda madre. In seguito, a causa dello scorporo, nel 1936, della sezione motoristica e la fondazione della Brandenburgische Motorenwerke GmbH (Bramo), confluita a sua volta, nel 1939, nella BMW GmbH, continuò ad essere prodotto e sviluppato dalle due aziende con la denominazione RLM Bramo 322 ed in seguito BMW-Bramo 322. In una sua versione intermedia, la Sh 22B (o SAM 22B), prodotta nei primi anni trenta era caratterizzata dall'adozione di un compressore centrifugo a singolo stadio e di un riduttore epicicloidale interposto al mozzo dell'elica. La potenza erogata di questa versione, grazie ai miglioramenti introdotti dalla Bramo, risultava di 660 PS (485 kW). Siemens & Halske Sh 22 — немецкий поршневой звездообразный 9-цилиндровый авиадвигатель воздушного охлаждения, разработанный в 1928 году. The Siemens-Halske Sh 22 (also known as SAM 22) was a nine-cylinder aircraft radial engine manufactured by Siemens & Halske in Germany in the 1930s. Following the reorganization of its manufacturer and change in military nomenclature, the engine became known as the Bramo 322. It was a result of a series of modifications to the original Bristol Jupiter IV design, which Siemens licensed in 1929. The first modifications were to "Germanize" the dimensions, producing the Sh.20 and Sh.21. The design was then bored out to produce the 950 hp (708 kW) Sh.22 in 1930. Like the Jupiter, the Sh.22 featured a rather "old" looking arrangement with rather prominent valve pushrods on the front of the engine. In the mid-1930s the Reich Air Ministry (RLM) rationalized engine naming, and Bramo was given the 300-block of numbers, the Sh.14 and Sh.22 becoming the Bramo 314 and 322 respectively. The 322 never matured and remained unreliable. It became a base for the more successful Bramo 323.
dbp:compression
6.4
dbp:coolingsystem
Air-cooled
dbp:developedFrom
Siemens-Halske Sh.21
dbp:developedInto
dbr:Bramo_323
dbp:displacement
26.82
dbp:firstRun
1930
dbp:fuelsystem
dbr:Carburetor
dbp:fueltype
87
dbp:oilcon
at max continuous
dbp:oilsystem
pressure fed at
n19:weight
at cruise *B.M.E.P.:
dbp:reductionGear
Farman epicyclic gearing, 0.62:1
gold:hypernym
dbr:Engine
prov:wasDerivedFrom
wikipedia-en:Siemens-Halske_Sh_22?oldid=1065060582&ns=0
dbo:wikiPageLength
4424
foaf:isPrimaryTopicOf
wikipedia-en:Siemens-Halske_Sh_22