Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:certifications |
gptkb:EASA
gptkb:FAA |
| gptkbp:controls |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:design |
three-shaft engine
|
| gptkbp:diameter |
2.9 m
2.7 m |
| gptkbp:engineType |
2
6 |
| gptkbp:firstFlight |
1995
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Trent 800A
|
| gptkbp:is_used_in |
gptkb:Boeing_777
|
| gptkbp:length |
3.4 m
|
| gptkbp:maintenance |
6,000 hours
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableUsers |
gptkb:Cathay_Pacific
gptkb:United_Airlines gptkb:British_Airways gptkb:Air_India gptkb:Korean_Air |
| gptkbp:operationalRange |
-54 to 50 °C
|
| gptkbp:propulsion |
up to 110,000 lbf
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:weight |
4,000 kg
|