|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:air_support
|
1,000 lb/s
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:bypass_ratio
|
5.5:1
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
fan, 3 axial
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
high bypass ratio
|
|
gptkbp:diameter
|
3.0 ft
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:CF6
gptkb:CF6_series
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_type
|
gptkb:CF6-50_C1
gptkb:CF6-50
high bypass turbofan
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
3.81 m
1,360 kg
0.91 m
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-50 C1
|
|
gptkbp:introduced
|
gptkb:1970
|
|
gptkbp:length
|
12.5 ft
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 0.85
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:notable_users
|
gptkb:Boeing_707
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_DC-10
|
|
gptkbp:operational_range
|
long-haul flights
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:power_source
|
twin-engine configuration
|
|
gptkbp:produces
|
over 1,000
|
|
gptkbp:propulsion
|
50,000 lbf
16.67:1
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
CF6-80 C2
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:water_requirement
|
2,000 lb/h
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:CF6-50_C
|
|
gptkbp:bfsLayer
|
7
|