Rolls-Royce AE 1107 C-Liberty
GPTKB entity
Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
military and civilian rotorcraft
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compression_ratio |
16:1
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:development |
gptkb:Rolls-Royce_AE_1107_A-Liberty
|
| gptkbp:diameter |
600 mm
|
| gptkbp:engine |
2
|
| gptkbp:engine_configuration |
twin-spool
|
| gptkbp:exhaust_system |
mixed flow
|
| gptkbp:first_flight |
gptkb:2007
|
| gptkbp:fuel_economy |
0.5 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce AE 1107 C-Liberty
|
| gptkbp:length |
1,200 mm
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:max_speed |
250 knots
|
| gptkbp:power_output |
6,150 shp
|
| gptkbp:service_entry |
gptkb:2007
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Bell_Boeing_V-22_Osprey
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:CV-22_Osprey
gptkb:V-22_Osprey |
| gptkbp:bfsLayer |
4
|