Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
8.8:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:emissionStandard |
CAEP/6
|
| gptkbp:family |
gptkb:GEnx
|
| gptkbp:firstFlight |
2009
|
| gptkbp:fuel_efficiency |
improved over CF6
|
| https://www.w3.org/2000/01/rdf-schema#label |
GEnx-2B67 turbofan
|
| gptkbp:mainRotorDiameter |
104.7 inches
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:relatedTo |
gptkb:GEnx-1B
|
| gptkbp:technology |
composite fan blades
titanium aluminide blades twin-annular pre-swirl combustor |
| gptkbp:thrust |
66,500 lbf
|
| gptkbp:type |
high-bypass
|
| gptkbp:usedInAircraft |
gptkb:Boeing_747-8
|
| gptkbp:bfsParent |
gptkb:747-8
gptkb:Boeing_747-8 |
| gptkbp:bfsLayer |
5
|