Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Airbus_A350-1000
|
| gptkbp:bypassRatio |
10:1
|
| gptkbp:certification |
2015
|
| gptkbp:compressionRatio |
50:1
|
| gptkbp:configuration |
three-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:family |
gptkb:Rolls-Royce_Trent
|
| gptkbp:firstRun |
2014
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Trent XWB-97
|
| gptkbp:length |
4.37 m
|
| gptkbp:mainRotorDiameter |
118 inches
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Holdings
|
| gptkbp:notableFeature |
most powerful engine in Trent family
used exclusively on Airbus A350-1000 |
| gptkbp:numberOfStages |
8 (intermediate), 6 (high-pressure)
1 (high-pressure), 1 (intermediate), 6 (low-pressure) |
| gptkbp:relatedTo |
gptkb:Rolls-Royce_Trent_XWB-84
|
| gptkbp:thrust |
97,000 lbf
|
| gptkbp:weight |
7,420 kg
|
| gptkbp:bfsParent |
gptkb:Airbus_A350-1000
|
| gptkbp:bfsLayer |
5
|