Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
8.5:1
|
| gptkbp:certification |
gptkb:EASA
gptkb:FAA |
| gptkbp:family |
gptkb:GEnx
|
| gptkbp:firstFlight |
2009
|
| gptkbp:fuelType |
improved over previous models
|
| gptkbp:hasConcept |
dual-spool
|
| https://www.w3.org/2000/01/rdf-schema#label |
GEnx-2B
|
| gptkbp:intendedUse |
long-haul commercial aircraft
|
| gptkbp:length |
184 inches
|
| gptkbp:mainRotorDiameter |
104 inches
|
| gptkbp:manufacturer |
gptkb:GE_Aviation
|
| gptkbp:successor |
gptkb:CF6-80C2
|
| gptkbp:technology |
composite fan blades
titanium aluminide blades lean-burn combustor |
| gptkbp:thrust |
66,500 lbf
|
| gptkbp:usedInAircraft |
gptkb:Boeing_747-8
|
| gptkbp:weight |
13,552 lb
|
| gptkbp:bfsParent |
gptkb:GEnx-1B
|
| gptkbp:bfsLayer |
7
|