|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional aircraft
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:bypass_ratio
|
5:1
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:configuration
|
twin-spool
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:transport_aircraft
gptkb:General_Electric
gptkb:CT7_family
CT7
advanced aerodynamics
performance upgrades
commercial aviation
mass production
reliable performance
regional aviation
CT7 series
ongoing development.
|
|
gptkbp:engine_configuration
|
twin-shaft
twin-spool turbofan
high bypass ratio turbofan
2,000 lbf
|
|
gptkbp:engine_power
|
high fuel efficiency
proven reliability
|
|
gptkbp:engine_type
|
turbofan
high bypass turbofan
CT7-2 E1
CT7-2 A1, CT7-2 B1
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:fuel_capacity
|
1,000 mm
400 kg
1,800 mm
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE CT7-2 E1
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
3,500 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:notable_users
|
gptkb:Bombardier_Q400
|
|
gptkbp:operational_range
|
1,500 nautical miles
|
|
gptkbp:power_output
|
1,500 k W
|
|
gptkbp:propulsion
|
2,000 lbf
|
|
gptkbp:service_ceiling
|
25,000 feet
|
|
gptkbp:status
|
in production
|
|
gptkbp:turbine_type
|
high bypass ratio
|
|
gptkbp:weight
|
400 kg
|
|
gptkbp:bfsParent
|
gptkb:AW189_M
gptkb:AW189_M_Helicopter
|
|
gptkbp:bfsLayer
|
6
|