Statements (34)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:certifications |
gptkb:FAA
|
| gptkbp:climate |
1,500 °F
|
| gptkbp:compressionRatio |
5.5:1
|
| gptkbp:controls |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
68 in
60 in |
| gptkbp:emissionsStandard |
CAEP/6
|
| gptkbp:engine |
gptkb:CF6-80C2B6E1
2 68 in 4,000 lb 158 in |
| gptkbp:engineConfiguration |
twin-spool
|
| gptkbp:engineType |
2
3 high bypass turbofan B6E1 |
| gptkbp:firstFlight |
1982
|
| gptkbp:fuel_capacity |
0.5 lb/lbf/hr
|
| gptkbp:fuelType |
Jet A
annular |
| https://www.w3.org/2000/01/rdf-schema#label |
CF6-80C2B6E1
|
| gptkbp:length |
158 in
|
| gptkbp:maintenance |
6,000 hours
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notableUsers |
gptkb:Airbus_A330
gptkb:Boeing_767 |
| gptkbp:propulsion |
60,000 lbf
|
| gptkbp:related_engine |
gptkb:CF6-80C2
CF6 |
| gptkbp:weight |
4,000 lb
|