Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
9.0:1
|
| gptkbp:certification |
gptkb:ETOPS
|
| gptkbp:emissionStandard |
reduced NOx
|
| gptkbp:family |
gptkb:GEnx
|
| gptkbp:firstFlight |
2007
|
| gptkbp:fuelType |
improved over previous generation
|
| gptkbp:hasConcept |
dual-spool
|
| https://www.w3.org/2000/01/rdf-schema#label |
GEnx-1B
|
| gptkbp:mainRotorDiameter |
111 in
|
| gptkbp:manufacturer |
gptkb:GE_Aviation
|
| gptkbp:marketEntry |
2012
|
| gptkbp:primaryUser |
gptkb:Japan_Airlines
gptkb:Qatar_Airways gptkb:United_Airlines gptkb:All_Nippon_Airways gptkb:Ethiopian_Airlines |
| gptkbp:relatedTo |
gptkb:GEnx-2B
|
| gptkbp:successor |
gptkb:CF6
|
| gptkbp:technology |
composite fan blades
titanium aluminide blades twin-annular pre-swirl combustor |
| gptkbp:thrust |
53,000–75,000 lbf
|
| gptkbp:usedInAircraft |
gptkb:aircraft
|
| gptkbp:volume |
reduced
|
| gptkbp:bfsParent |
gptkb:Qatar_Airways_Boeing_787
gptkb:GEnx-2B67_turbofan |
| gptkbp:bfsLayer |
6
|