|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional aircraft
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:bypass_ratio
|
4.5:1
|
|
gptkbp:certification
|
gptkb:Federal_Aviation_Administration_(FAA)
gptkb:European_Union_Aviation_Safety_Agency_(EASA)
CAEP/6
|
|
gptkbp:competitors
|
gptkb:Rolls-Royce's_AE_3007
gptkb:GE_Aviation's_CF34
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:configuration
|
twin-spool
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
Air-cooled
|
|
gptkbp:customer_support
|
gptkb:Flight
Lessors
Aircraft manufacturers
|
|
gptkbp:design_feature
|
Advanced aerodynamics
High bypass ratio
Composite fan blades
Low noise technology
|
|
gptkbp:design_purpose
|
High efficiency
|
|
gptkbp:diameter
|
68 in
30 in
|
|
gptkbp:engine
|
gptkb:Geared_Turbofan
|
|
gptkbp:environmental_impact
|
Reduced emissions
|
|
gptkbp:first_flight
|
gptkb:2014
|
|
gptkbp:fuel_capacity
|
Dry sump
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
Improved over previous models
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
Electronic fuel control
|
|
gptkbp:gearbox
|
Reduction gearbox
|
|
gptkbp:has_programs
|
gptkb:Pure_Power_PW1000_G
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW1900 G engine
|
|
gptkbp:ignition_system
|
Dual spark plug
|
|
gptkbp:legal_principle
|
Brayton cycle
|
|
gptkbp:length
|
60 in
|
|
gptkbp:maintenance
|
5,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:market_segment
|
Regional aviation
|
|
gptkbp:noise_level
|
gptkb:Stage_4
|
|
gptkbp:propulsion
|
4,700 lbf
3.9:1
|
|
gptkbp:related_aircraft
|
gptkb:Embraer_E-Jet_E2
gptkb:Mitsubishi_Space_Jet
gptkb:Bombardier_CRJ_Series
|
|
gptkbp:service_entry
|
gptkb:2016
|
|
gptkbp:services_provided
|
Maintenance, repair, and overhaul (MRO)
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Geared_Turbofan_family
|
|
gptkbp:bfsLayer
|
7
|