Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
10:1
|
| gptkbp:certification |
August 7, 2007
|
| gptkbp:configuration |
three-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:enteredService |
2011
|
| gptkbp:family |
gptkb:Rolls-Royce_Trent
|
| gptkbp:firstRun |
2006
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trent 1000
|
| gptkbp:mainRotorDiameter |
112 inches
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableOperation |
gptkb:British_Airways
gptkb:Norwegian_Air_Shuttle gptkb:All_Nippon_Airways gptkb:Air_New_Zealand |
| gptkbp:numberOfIssues |
blade corrosion
durability problems groundings due to technical issues |
| gptkbp:numberOfSpools |
three
|
| gptkbp:numberOfStages |
6 (high and intermediate pressure)
8 (high pressure) |
| gptkbp:predecessor |
gptkb:Trent_900
|
| gptkbp:successor |
gptkb:Trent_XWB
|
| gptkbp:thrust |
53,000 to 78,000 lbf
|
| gptkbp:usedInAircraft |
gptkb:aircraft
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Holdings
|
| gptkbp:bfsLayer |
5
|