Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
AE 1107C-Liberty
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:category |
piston engine
|
| gptkbp:compressionRatio |
axial/centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.6 m
|
| gptkbp:firstRun |
1988
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce T406 engine
|
| gptkbp:length |
2.1 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
gptkb:Allison_Engine_Company |
| gptkbp:numberOfStages |
2
14 |
| gptkbp:powerOutput |
6,150 shp
|
| gptkbp:status |
in production
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Bell_Boeing_V-22_Osprey
|
| gptkbp:weight |
1,030 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_T406_core
|
| gptkbp:bfsLayer |
8
|