Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:Boeing_747-8
|
| gptkbp:bypassRatio |
8.5:1
|
| gptkbp:certification |
2010
|
| gptkbp:emissionStandard |
reduced NOx
|
| gptkbp:family |
gptkb:GEnx
|
| gptkbp:firstFlight |
2009
|
| gptkbp:fuelType |
improved over CF6
|
| gptkbp:hasConcept |
high-bypass
|
| gptkbp:length |
184 inches
|
| gptkbp:mainRotorDiameter |
104 inches
|
| gptkbp:maintenanceInterval |
extended
|
| gptkbp:manufacturer |
gptkb:GE_Aviation
|
| gptkbp:successor |
gptkb:CF6
|
| gptkbp:technology |
composite fan blades
titanium aluminide blades twin-annular pre-swirl combustor |
| gptkbp:thrust |
66,500 lbf
|
| gptkbp:volume |
reduced
|
| gptkbp:weight |
13,552 lb
|
| gptkbp:bfsParent |
gptkb:Boeing_747-8I
gptkb:B748 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
GEnx-2B67
|