|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_AE_1107_C-Liberty
|
|
gptkbp:application
|
military and civilian aircraft
|
|
gptkbp:average_temperature
|
1,600 ° C
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
liquid-cooled
|
|
gptkbp:diameter
|
600 mm
|
|
gptkbp:engine
|
twin-spool
pylon-mounted
air-start
twin-spool engine
|
|
gptkbp:engine_type
|
gptkb:engine
turbo-shaft
|
|
gptkbp:first_flight
|
gptkb:2007
|
|
gptkbp:fuel_capacity
|
high
1,200 kg
1,200 mm
600 mm
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce AE 1107 A-Liberty
|
|
gptkbp:length
|
1,200 mm
|
|
gptkbp:maintenance
|
2,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_feature
|
gptkb:dual-channel_FADEC
|
|
gptkbp:operational_range
|
1,000 nautical miles
|
|
gptkbp:power_output
|
twin-engine configuration
6,150 shp
|
|
gptkbp:propulsion
|
5.1:1
5.1 hp/kg
|
|
gptkbp:service_ceiling
|
25,000 feet
|
|
gptkbp:status
|
in production
|
|
gptkbp:supports
|
100 kg/s
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Bell_Boeing_V-22_Osprey
|
|
gptkbp:weight
|
1,200 kg
|