Rolls-Royce RB211 (production model)
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
4.3–5.1:1
|
| gptkbp:configuration |
three-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:firstFlight |
1969
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce RB211 (production model)
|
| gptkbp:introduced |
1972
|
| gptkbp:length |
3.9 m
|
| gptkbp:mainRotorDiameter |
86–97 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableFeature |
first production three-spool turbofan
|
| gptkbp:primaryUse |
commercial airliners
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Rolls-Royce_Trent
|
| gptkbp:thrust |
37,400–60,600 lbf
|
| gptkbp:usedIn |
gptkb:Boeing_757
gptkb:Boeing_767 gptkb:aircraft gptkb:Lockheed_L-1011_TriStar gptkb:Tu-204 |
| gptkbp:weight |
4,400–5,200 lb
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_RB211_(proposed,_not_built)
|
| gptkbp:bfsLayer |
6
|