|
gptkbp:instanceOf
|
gptkb:piston_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:bypassRatio
|
10:1
|
|
gptkbp:certification
|
August 2007
|
|
gptkbp:competitor
|
gptkb:General_Electric_GEnx
gptkb:Pratt_&_Whitney_PW1000G
|
|
gptkbp:configuration
|
three-shaft
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:enteredService
|
2011
|
|
gptkbp:family
|
gptkb:Rolls-Royce_Trent
|
|
gptkbp:firstOperator
|
gptkb:All_Nippon_Airways
|
|
gptkbp:firstRun
|
2006
|
|
gptkbp:fuelType
|
aviation kerosene
|
|
gptkbp:intendedAircraft
|
gptkb:aircraft
|
|
gptkbp:length
|
4.4 m
|
|
gptkbp:mainRotorDiameter
|
112 in (2.85 m)
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Holdings
|
|
gptkbp:notableFeature
|
advanced materials
reduced emissions
improved fuel efficiency
|
|
gptkbp:numberOfIssues
|
blade corrosion
durability problems
groundings of Boeing 787s
|
|
gptkbp:numberOfStages
|
6 (high-pressure)
8 (high-pressure)
|
|
gptkbp:predecessor
|
gptkb:Rolls-Royce_Trent_900
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Trent_XWB
|
|
gptkbp:thrust
|
53,000 to 78,000 lbf
|
|
gptkbp:weight
|
6,120 kg
|
|
gptkbp:bfsParent
|
gptkb:Boeing_787-9
gptkb:Boeing_787-8
gptkb:Boeing_787-10
gptkb:Rolls-Royce_Trent_800
gptkb:GEnx_engine
|
|
gptkbp:bfsLayer
|
6
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Trent 1000
|