|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
gptkb:Airbus_A300_family
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:certifications
|
gptkb:FAA
CAEP/6
|
|
gptkbp:climate
|
up to 1,600 °F
|
|
gptkbp:compressionRatio
|
5.5:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:customerService
|
gptkb:United_Airlines
|
|
gptkbp:diameter
|
68 inches
|
|
gptkbp:engine
|
68 inches
12.5 ft
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
gptkb:CF6-80C2B1F4
gptkb:CF6-80C2B1F3
gptkb:CF6-80C2B1F6
gptkb:CF6-80C2B1F5
gptkb:CF6-80C2B1F8
axial compressor
high-pressure and low-pressure turbines
CF6-80C2B1F2
CF6-80C2B1F7
CF6-80C2B1F9
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuelType
|
Jet A
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80C2B1F18
|
|
gptkbp:inspiration
|
high reliability
|
|
gptkbp:is_used_in
|
gptkb:Airbus_A310
gptkb:Airbus_A300
McDonnell Douglas MD-11
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:market
|
significant in wide-body aircraft
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:notable_feature
|
high bypass ratio
|
|
gptkbp:number_of_stages
|
3
|
|
gptkbp:operational_status
|
commercial airlines
|
|
gptkbp:operationalRange
|
long-haul flights
|
|
gptkbp:performances
|
up to 30,000 hours
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:propulsion
|
18,500 to 34,000 lbf
cascade
|
|
gptkbp:related_to
|
gptkb:CF6_family_of_engines
|
|
gptkbp:serviceType
|
1982
|
|
gptkbp:successor
|
CF6-80C2B1F2
|
|
gptkbp:technology
|
advanced materials
|
|
gptkbp:training
|
GE90 program
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:weight
|
3,000 lb
|