|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:bypassRatio
|
9.0:1
|
|
gptkbp:certification
|
gptkb:FAA
|
|
gptkbp:competitor
|
gptkb:Rolls-Royce_Trent_1000
|
|
gptkbp:emissionStandard
|
reduced NOx emissions
|
|
gptkbp:ETOPS
|
330 minutes
|
|
gptkbp:family
|
gptkb:GEnx
|
|
gptkbp:firstFlight
|
2007
|
|
gptkbp:fuelType
|
improved over previous models
|
|
gptkbp:hasConcept
|
dual-spool
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric GEnx-1B
|
|
gptkbp:mainRotorDiameter
|
111 inches
|
|
gptkbp:maintenanceInterval
|
improved over previous GE engines
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:marketEntry
|
2011
|
|
gptkbp:noiseReduction
|
composite fan blades
|
|
gptkbp:notableOperation
|
gptkb:Japan_Airlines
gptkb:Qatar_Airways
gptkb:United_Airlines
gptkb:All_Nippon_Airways
|
|
gptkbp:successor
|
gptkb:CF6_engine_family
|
|
gptkbp:technology
|
gptkb:TAPS_II_combustor
titanium aluminide blades
composite fan case
|
|
gptkbp:thrust
|
53,000–75,000 lbf
|
|
gptkbp:usedInAircraft
|
gptkb:aircraft
|
|
gptkbp:weight
|
approx. 13,552 lb
|
|
gptkbp:bfsParent
|
gptkb:Boeing_787-10
|
|
gptkbp:bfsLayer
|
5
|