Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:Airbus_A330
|
| gptkbp:bypassRatio |
5.3:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:compressionRatio |
30.4:1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:family |
gptkb:General_Electric_CF6
|
| gptkbp:firstFlight |
1992
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasConcept |
high-bypass turbofan
|
| gptkbp:intendedAircraft |
gptkb:Airbus_A330_family
|
| gptkbp:length |
4.37 m
|
| gptkbp:mainRotorDiameter |
2.44 m
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:numberOfStages |
14
4 |
| gptkbp:relatedTo |
gptkb:General_Electric_CF6-80C2
|
| gptkbp:status |
in production
|
| gptkbp:thrust |
68,000 lbf to 72,000 lbf
|
| gptkbp:usedOn |
gptkb:aircraft
|
| gptkbp:weight |
4,300 kg
|
| gptkbp:bfsParent |
gptkb:Airbus_A330_family
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric CF6-80E1
|