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Statements

Subject Item
dbr:Power_Jets_W.2
rdf:type
yago:Device103183080 yago:PhysicalEntity100001930 yago:Motor103789946 yago:Machine103699975 yago:AircraftEngine102687423 yago:Artifact100021939 yago:Instrumentality103575240 yago:Engine103287733 yago:Whole100003553 dbo:Software yago:Object100002684
rdfs:label
Power Jets W.2 Power Jets W.2 Power Jets W.2
rdfs:comment
Le Power Jets W.2 était un turboréacteur britannique, conçu par Frank Whittle et sa compagnie, la Power Jets (Research and Development) Ltd.. Comme le précédent Power Jets W.1, sa configuration « en trombone » comprenait un compresseur centrifuge unique à double entrée, des chambres de combustion de type reverse flow (à flux inversé) et une turbine axiale refroidie par circulation d'air. Power Jets W.2 byl britský proudový motor navržený Frankem Whittleyem a . Jako předchozí motor Power Jets W.1 měl podobnou konfiguraci jako protiproudé trubkové spalovací komory, oboustranný radiální kompresor a vzduchem chlazenou část s turbínou. The Power Jets W.2 was a British turbojet engine designed by Frank Whittle and Power Jets (Research and Development) Ltd. Like the earlier Power Jets W.1, the reverse-flow combustion configuration included a double-sided centrifugal compressor, 10 combustion chambers and an axial-flow turbine with air-cooled disc.
foaf:depiction
n11:Welland.jpg n11:Whittle_Jet_Engine_W2-700.jpg
dcterms:subject
dbc:Power_Jets dbc:1940s_turbojet_engines dbc:Centrifugal-flow_turbojet_engines
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24677697
dbo:wikiPageRevisionID
1102991074
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dbp:thrust
2485
n24:weight
2.6
dbp:turbine
Single stage axial flow
dbp:wikiPageUsesTemplate
dbt:Power_Jets_aeroengines dbt:Refend dbt:Reflist dbt:Refbegin dbt:Infobox_Aircraft_Engine dbt:Short_description dbt:Cite_book dbt:ISBN dbt:Commons_category dbt:Jetspecs dbt:Aircontent dbt:Convert dbt:Use_British_English dbt:Use_dmy_dates
dbo:thumbnail
n11:Whittle_Jet_Engine_W2-700.jpg?width=300
dbp:manufacturer
dbr:Rover_Company
dbp:ref
Jane's
dbp:related
* Power Jets W.1 * General Electric I-A * Rolls-Royce Welland
dbp:type
dbr:Turbojet Centrifugal flow turbojet
dbp:weight
950.0
dbo:abstract
Le Power Jets W.2 était un turboréacteur britannique, conçu par Frank Whittle et sa compagnie, la Power Jets (Research and Development) Ltd.. Comme le précédent Power Jets W.1, sa configuration « en trombone » comprenait un compresseur centrifuge unique à double entrée, des chambres de combustion de type reverse flow (à flux inversé) et une turbine axiale refroidie par circulation d'air. Power Jets W.2 byl britský proudový motor navržený Frankem Whittleyem a . Jako předchozí motor Power Jets W.1 měl podobnou konfiguraci jako protiproudé trubkové spalovací komory, oboustranný radiální kompresor a vzduchem chlazenou část s turbínou. The Power Jets W.2 was a British turbojet engine designed by Frank Whittle and Power Jets (Research and Development) Ltd. Like the earlier Power Jets W.1, the reverse-flow combustion configuration included a double-sided centrifugal compressor, 10 combustion chambers and an axial-flow turbine with air-cooled disc.
dbp:aircon
47
dbp:combustion
10
dbp:compression
4
dbp:compressor
Single-stage double-sided centrifugal flow
dbp:developedFrom
dbr:Power_Jets_W.1
dbp:developedInto
Rolls-Royce Derwent Rolls-Royce Welland dbr:General_Electric_I-A
dbp:firstRun
c.1941
dbp:fuelcon
2610
dbp:fueltype
Kerosene
dbp:lists
*List of aircraft engines
dbp:majorApplications
dbr:Gloster_Meteor n16:39
gold:hypernym
dbr:Engine
prov:wasDerivedFrom
wikipedia-en:Power_Jets_W.2?oldid=1102991074&ns=0
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15309
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wikipedia-en:Power_Jets_W.2