Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Airbus_A350-900
|
| gptkbp:bypassRatio |
9.3:1
|
| gptkbp:certification |
gptkb:EASA
|
| gptkbp:configuration |
three-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:family |
gptkb:Rolls-Royce_Trent
|
| gptkbp:firstRun |
2010
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Trent XWB-84
|
| gptkbp:introduced |
2015
|
| gptkbp:length |
4.84 m
|
| gptkbp:mainRotorDiameter |
118 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_plc
|
| gptkbp:marketEntry |
gptkb:Qatar_Airways
|
| gptkbp:notableFeature |
most efficient large aero engine (as of 2020)
|
| gptkbp:numberOfStages |
1 (HP), 1 (IP), 6 (LP)
8 (IP), 6 (HP) |
| gptkbp:relatedTo |
gptkb:Rolls-Royce_Trent_XWB-97
|
| gptkbp:thrust |
84,000 lbf
|
| gptkbp:usedOn |
gptkb:Airbus_A350_XWB
|
| gptkbp:weight |
7,420 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Trent_XWB-97
|
| gptkbp:bfsLayer |
6
|