|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:competitors
|
gptkb:Rolls-Royce_RB211
gptkb:Pratt_&_Whitney_PW4000
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_base
|
global airlines
|
|
gptkbp:design
|
advanced aerodynamics
|
|
gptkbp:development
|
5 years
|
|
gptkbp:diameter
|
2.5 m
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
modular design
|
|
gptkbp:environmental_impact
|
low
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_economy
|
good
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-50 C6
|
|
gptkbp:involved_technology
|
24/7
|
|
gptkbp:legacy
|
widely used engine
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:market_position
|
high
|
|
gptkbp:market_share
|
gptkb:significant
|
|
gptkbp:modifications
|
upgrades available
|
|
gptkbp:network
|
worldwide
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:project
|
ongoing research
|
|
gptkbp:propulsion
|
50,000 lbf
16.67
|
|
gptkbp:rating
|
excellent
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:1971
|
|
gptkbp:training_programs
|
available
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:uses
|
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_DC-10
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:CF6-50_C
|
|
gptkbp:bfsLayer
|
7
|