|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:armament
|
composite
|
|
gptkbp:certification
|
gptkb:FAA
|
|
gptkbp:compressor_type
|
gptkb:5
axial compressor
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
modular
|
|
gptkbp:development
|
gptkb:CF6_family
|
|
gptkbp:diameter
|
3.0 ft
60 in
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:CF6-6
gptkb:CF6-80_E1
gptkb:CF6-80_A
modular design
scheduled maintenance
performance upgrades available
replaceable components
|
|
gptkbp:engine_configuration
|
50,000 lbf
twin spool
|
|
gptkbp:engine_design_life
|
20,000 hours
|
|
gptkbp:engine_power
|
high efficiency
optimized for long-haul flights
|
|
gptkbp:engine_type
|
gptkb:CF6-50_A
gptkb:CF6-50_B
high bypass ratio
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
10,000 lb
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-50 C10
|
|
gptkbp:is_tested_for
|
static testing
flight testing
advanced diagnostics system
|
|
gptkbp:launch_platform
|
electric starter
|
|
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
low noise
|
|
gptkbp:notable_users
|
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_DC-10
|
|
gptkbp:operational_history
|
in service since 1970
|
|
gptkbp:propulsion
|
50,000 lbf
16.67
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
CF6-80 C2
|
|
gptkbp:turbine_type
|
gptkb:Super_GT
2
high-pressure turbine
|
|
gptkbp:warranty
|
5 years
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:CF6-50_C
|
|
gptkbp:bfsLayer
|
7
|