|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:bypass_ratio
|
8:1
|
|
gptkbp:certification
|
gptkb:FAA
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
fan, 3
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:designated_thrust_rating
|
80,000 lbf
|
|
gptkbp:diameter
|
3.0 ft
2.9 ft
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:CF6
|
|
gptkbp:engine_configuration
|
twin-spool
pylon-mounted
|
|
gptkbp:engine_type
|
gptkb:CF6-80_E1_F1
gptkb:CF6-80_E1_D1
gptkb:CF6-80_E1_D4
gptkb:CF6-80_E1_D5
gptkb:CF6-80_E1_D6
gptkb:CF6-80_E1_D7
gptkb:CF6-80_E1_D9
gptkb:CF6-80_E1
gptkb:CF6-80_E1_A1
high-bypass turbofan
CF6-80 C2
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80 E1 D8
|
|
gptkbp:length
|
11.5 ft
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
gptkb:Stage_4
|
|
gptkbp:notable_users
|
gptkb:Airbus
gptkb:Boeing
gptkb:Mc_Donnell_Douglas_MD-11
|
|
gptkbp:propulsion
|
cascade
68,000 lbf
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:weight
|
4,000 lb
|
|
gptkbp:bfsParent
|
gptkb:CF6-80_E1_D
|
|
gptkbp:bfsLayer
|
7
|