|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
high temperature
|
|
gptkbp:bypass_ratio
|
5.5:1
|
|
gptkbp:certification
|
gptkb:FAA
NOx compliance
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_features
|
advanced materials
modular construction
high bypass ratio
|
|
gptkbp:diameter
|
68 in
112 in
|
|
gptkbp:engine
|
gptkb:CF6
gptkb:CF6-80
|
|
gptkbp:engine_configuration
|
pylon-mounted
|
|
gptkbp:engine_type
|
gptkb:CF6-80_E1_F1
gptkb:CF6-80_E1_D10
gptkb:CF6-80_E1_D4
gptkb:CF6-80_E1_D5
gptkb:CF6-80_E1_D6
gptkb:CF6-80_E1_D8
gptkb:CF6-80_E1_D9
gptkb:CF6-80_E1
turbofan
CF6-80 C2
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
electronic fuel control
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80 E1 D7
|
|
gptkbp:length
|
150 in
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:maximum_continuous_thrust
|
65,000 lbf
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:notable_users
|
gptkb:Boeing_707
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_MD-11
|
|
gptkbp:operational_history
|
in service since 1982
|
|
gptkbp:propulsion
|
cascade
70,000 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
|