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gptkbp:instance_of
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gptkb:turbofan_engine
|
|
gptkbp:air_support
|
high airflow capacity
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
high temperature capability
|
|
gptkbp:cancellation_reason
|
yes
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
lean burn combustor
|
|
gptkbp:competitors
|
gptkb:Rolls-Royce_Trent_1000
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
advanced cooling technology
advanced cooling system
|
|
gptkbp:customer_base
|
major airlines worldwide
|
|
gptkbp:design_advantage
|
reduced drag
|
|
gptkbp:design_feature
|
blended winglets
|
|
gptkbp:designed_for
|
gptkb:Boeing_787_Dreamliner
|
|
gptkbp:development
|
part of GEnx family
|
|
gptkbp:diameter
|
8:1
2.68 m
|
|
gptkbp:emissions_standard
|
lower NOx emissions
|
|
gptkbp:engine
|
widely available
innovative design features
comprehensive support services
quick start capability
GEnx series
|
|
gptkbp:engine_configuration
|
pylon mounted
twin spool
|
|
gptkbp:engine_power
|
high reliability
optimized performance
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
gptkb:2007
|
|
gptkbp:fuel_capacity
|
3.5 m
lightweight design
2.68 m
|
|
gptkbp:fuel_economy
|
15% better than previous models
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric GEnx-2 B67
|
|
gptkbp:investment
|
high pressure ratio
|
|
gptkbp:is_tested_for
|
extensive testing program
|
|
gptkbp:maintenance
|
longer intervals than predecessors
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:operational_range
|
high bypass ratio
|
|
gptkbp:performance
|
high performance engine
|
|
gptkbp:propulsion
|
67,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:Boeing_787
gptkb:Boeing_747-8
|
|
gptkbp:service_entry
|
gptkb:2011
|
|
gptkbp:technology
|
advanced composite fan blades
|
|
gptkbp:weight
|
approximately 4,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Lockheed_C-5_M_Super_Galaxy
|
|
gptkbp:bfsLayer
|
6
|