Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Fokker_100
gptkb:Gulfstream_GIV gptkb:Dassault_Falcon_900 |
| gptkbp:compressionRatio |
2-stage fan, 12-stage HP compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:derivedFrom |
gptkb:Rolls-Royce_RB.183
|
| gptkbp:diameter |
1.04 m
|
| gptkbp:family |
gptkb:Rolls-Royce_RB.183_Tay
|
| gptkbp:firstRun |
1984
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:hasTower |
2-stage HP, 3-stage LP
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Tay
|
| gptkbp:length |
2.6 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_plc
|
| gptkbp:notableVariant |
gptkb:Tay_611-8
gptkb:Tay_620-15 |
| gptkbp:status |
in production
|
| gptkbp:thrust |
13,850–15,100 lbf
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:usedIn |
civil aviation
|
| gptkbp:weight |
1,350 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Spey
gptkb:Pratt_&_Whitney_J48 gptkb:Rolls-Royce_BR700_family gptkb:Rolls-Royce_aircraft_engines gptkb:Rolls-Royce_Tay_611-8 gptkb:Rolls-Royce_BR715 |
| gptkbp:bfsLayer |
7
|