|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:air_support
|
2,000 lb/sec
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
1,600 ° F
|
|
gptkbp:bypass_ratio
|
8:1
|
|
gptkbp:certification
|
gptkb:Stage_4
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
fan, 3-stage low-pressure, 10-stage high-pressure
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_support
|
gptkb:United_Airlines
|
|
gptkbp:design
|
20,000 hours
|
|
gptkbp:diameter
|
2.9 m
3.0 ft
|
|
gptkbp:engine
|
gptkb:CF6_family
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_type
|
gptkb:CF6-80_E1_F1
gptkb:CF6-80_E1_D1
gptkb:CF6-80_E1
gptkb:CF6-80_E1_A1
high-bypass turbofan
dual-rotor
CF6-80 E1 B1
CF6-80 E1 E1
CF6-80 E1 H1
CF6-80 E1 K1
CF6-80 E1 L1
CF6-80 E1 M1
CF6-80 E1 N1
CF6-80 E1 P1
CF6-80 E1 Q1
CF6-80 E1 R1
CF6-80 E1 S1
CF6-80 E1 T1
CF6-80 E1 U1
CF6-80 E1 V1
CF6-80 E1 W1
CF6-80 E1 X1
CF6-80 E1 Y1
CF6-80 E1 Z1
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_capacity
|
0.9 m
3.5 m
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:history
|
derived from CF6-50
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80 E1 D6
|
|
gptkbp:length
|
11.5 ft
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:notable_users
|
gptkb:Boeing_707
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_MD-11
|
|
gptkbp:propulsion
|
15:1
60,000 lbf
|
|
gptkbp:service_ceiling
|
42,000 ft
|
|
gptkbp:turbine_type
|
2-stage high-pressure, 2-stage low-pressure
|
|
gptkbp:water_requirement
|
1,200 lb/hr
|
|
gptkbp:weight
|
4,000 lb
|
|
gptkbp:bfsParent
|
gptkb:CF6-80_E1_D
|
|
gptkbp:bfsLayer
|
7
|