|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:compressor_type
|
gptkb:5
axial compressor
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:General_Electric
20,000 hours
|
|
gptkbp:diameter
|
3.0 ft
2.5 ft
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
modular design
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_type
|
gptkb:CF6-50_A
gptkb:CF6-50_B
gptkb:CF6-50_C
gptkb:CF6-50_E
gptkb:CF6-50_R
gptkb:CF6-50_S
dual-rotor
|
|
gptkbp:fan_art
|
wide-chord fan blades
|
|
gptkbp:fan_material
|
composite materials
|
|
gptkbp:first_flight
|
gptkb:1971
|
|
gptkbp:fuel_capacity
|
lightweight
|
|
gptkbp:fuel_economy
|
high efficiency
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric CF6-50
|
|
gptkbp:is_tested_for
|
extensive ground testing
|
|
gptkbp:legal_principle
|
gptkb:jet_engine
|
|
gptkbp:length
|
11.5 ft
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:market_segment
|
wide-body aircraft
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:propulsion
|
50,000 lbf
12.5:1
|
|
gptkbp:related_aircraft
|
gptkb:Boeing_707
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_DC-10
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:1972
|
|
gptkbp:successor
|
gptkb:General_Electric_CF6-80
|
|
gptkbp:turbine_type
|
2
high-pressure turbine
nickel alloy
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:weight
|
4,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Mc_Donnell_Douglas_DC-10-30
|
|
gptkbp:bfsLayer
|
5
|