|
gptkbp:instanceOf
|
turboshaft engine
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:compressionRatio
|
16:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
gptkb:Rolls-Royce_Corporation
|
|
gptkbp:developer
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
20 in
|
|
gptkbp:emissionsStandard
|
mixed exhaust
compliant_with_ICAO
|
|
gptkbp:engine
|
60 inches
20 inches
V-22 Osprey
advanced technology
modular design
1,200 pounds
annular combustor
AE 1107C-1
military rotorcraft
|
|
gptkbp:engineConfiguration
|
twin-spool
twin-spool design
6,150_shaft_horsepower
|
|
gptkbp:engineType
|
gptkb:dual-channel_FADEC
air start
turbo-shaft
AE 1107C-1
|
|
gptkbp:exhaustSystem
|
mixed
|
|
gptkbp:firstFlight
|
2007
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:hasArea
|
ground testing
FAA_certified
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce AE 1107C
|
|
gptkbp:is_used_in
|
gptkb:Bell_Boeing_V-22_Osprey
|
|
gptkbp:length
|
60 in
|
|
gptkbp:maintenance
|
2,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise design
|
|
gptkbp:notable_feature
|
tilt-rotor capability
|
|
gptkbp:operational_status
|
gptkb:U.S._military
|
|
gptkbp:performances
|
high performance
high reliability
|
|
gptkbp:powerOutput
|
6,150 shp
|
|
gptkbp:propulsion
|
5.0:1
6,000 lbf
6,000 pounds-force
|
|
gptkbp:related_engine
|
gptkb:Rolls-Royce_AE_1107C-Liberty
gptkb:AE_family
Brayton_cycle
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:type
|
turbo-shaft engine
|
|
gptkbp:weight
|
1,200 lb
|