Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
military tiltrotor aircraft
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:combustorType |
annular combustor
|
| gptkbp:compressionRatio |
14-stage axial compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
0.6 m
|
| gptkbp:family |
gptkb:Rolls-Royce_AE_family
|
| gptkbp:firstFlight |
1990s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasConcept |
gptkb:Rolls-Royce_AE_3007_core
|
| gptkbp:hasTower |
2-stage high-pressure, 2-stage power turbine
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce AE 1107C
|
| gptkbp:length |
1.8 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:marketedAs |
gptkb:Confederate_States_of_America
|
| gptkbp:powerOutput |
6,150 shp
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:Bell_Boeing_V-22_Osprey
gptkb:Bell_V-280_Valor |
| gptkbp:weight |
635 kg
|
| gptkbp:bfsParent |
gptkb:AE_1107C
|
| gptkbp:bfsLayer |
6
|