http://dbpedia.org/ontology/abstract
|
The Energy Efficient Engine was a program … The Energy Efficient Engine was a program funded by NASA in the 1970s to develop technologies suitable for energy efficient turbofans. Its goal was to improve thrust specific fuel consumption by 12% compared to a GE CF6-50C. Both General Electric and Pratt & Whitney produced turbofans for the program. The GE core featured a 23:1 high-pressure (HP) ratio ten-stage HP compressor, later used in the GE90 and GEnx. P&W also used a ten-stage HP compressor in their core, but it developed 14:1 pressure ratio.ore, but it developed 14:1 pressure ratio.
|
http://dbpedia.org/ontology/wikiPageID
|
28344162
|
http://dbpedia.org/ontology/wikiPageLength
|
1663
|
http://dbpedia.org/ontology/wikiPageRevisionID
|
975451435
|
http://dbpedia.org/ontology/wikiPageWikiLink
|
http://dbpedia.org/resource/General_Electric_GEnx +
, http://dbpedia.org/resource/GE_CF6 +
, http://dbpedia.org/resource/Turbofan +
, http://dbpedia.org/resource/General_Electric_GE90 +
, http://dbpedia.org/resource/NASA +
, http://dbpedia.org/resource/Pratt_&_Whitney +
, http://dbpedia.org/resource/General_Electric +
, http://dbpedia.org/resource/Category:Turbofan_engines +
, http://dbpedia.org/resource/Thrust_specific_fuel_consumption +
, http://dbpedia.org/resource/Efficient_energy_use +
|
http://dbpedia.org/property/wikiPageUsesTemplate
|
http://dbpedia.org/resource/Template:Aviation-stub +
, http://dbpedia.org/resource/Template:Reflist +
|
http://purl.org/dc/terms/subject
|
http://dbpedia.org/resource/Category:Turbofan_engines +
|
http://purl.org/linguistics/gold/hypernym
|
http://dbpedia.org/resource/Program +
|
http://www.w3.org/ns/prov#wasDerivedFrom
|
http://en.wikipedia.org/wiki/Energy_Efficient_Engine?oldid=975451435&ns=0 +
|
http://xmlns.com/foaf/0.1/isPrimaryTopicOf
|
http://en.wikipedia.org/wiki/Energy_Efficient_Engine +
|
owl:sameAs |
http://dbpedia.org/resource/Energy_Efficient_Engine +
, http://yago-knowledge.org/resource/Energy_Efficient_Engine +
, http://www.wikidata.org/entity/Q5376925 +
, http://rdf.freebase.com/ns/m.0cp1ft2 +
, https://global.dbpedia.org/id/4jjJb +
|
rdf:type |
http://dbpedia.org/class/yago/Instrumentality103575240 +
, http://dbpedia.org/class/yago/PhysicalEntity100001930 +
, http://dbpedia.org/class/yago/Whole100003553 +
, http://dbpedia.org/ontology/Work +
, http://dbpedia.org/class/yago/Motor103789946 +
, http://dbpedia.org/class/yago/WikicatTurbofanEngines +
, http://dbpedia.org/class/yago/Device103183080 +
, http://dbpedia.org/class/yago/Reaction-propulsionEngine104057435 +
, http://dbpedia.org/class/yago/Artifact100021939 +
, http://dbpedia.org/class/yago/Machine103699975 +
, http://dbpedia.org/class/yago/Engine103287733 +
, http://dbpedia.org/class/yago/Fanjet103321103 +
, http://dbpedia.org/class/yago/JetEngine103596285 +
, http://dbpedia.org/class/yago/Object100002684 +
|
rdfs:comment |
The Energy Efficient Engine was a program … The Energy Efficient Engine was a program funded by NASA in the 1970s to develop technologies suitable for energy efficient turbofans. Its goal was to improve thrust specific fuel consumption by 12% compared to a GE CF6-50C. Both General Electric and Pratt & Whitney produced turbofans for the program. The GE core featured a 23:1 high-pressure (HP) ratio ten-stage HP compressor, later used in the GE90 and GEnx. P&W also used a ten-stage HP compressor in their core, but it developed 14:1 pressure ratio.ore, but it developed 14:1 pressure ratio.
|
rdfs:label |
Energy Efficient Engine
|