Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Airbus_A350-900
|
| gptkbp:bypassRatio |
9.6:1
|
| gptkbp:certification |
gptkb:EASA
|
| gptkbp:compressionRatio |
50:1
|
| 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 |
Trent XWB-84
|
| gptkbp:length |
4.83 m
|
| gptkbp:mainRotorDiameter |
118 inches
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableFeature |
most efficient large aero engine (as of 2020)
|
| gptkbp:numberOfAxles |
3
|
| gptkbp:status |
in production
|
| gptkbp:successor |
gptkb:Trent_XWB-97
|
| gptkbp:thrust |
84,000 lbf
|
| gptkbp:weight |
7,300 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Trent_XWB
|
| gptkbp:bfsLayer |
6
|