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gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional jets
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:competitors
|
gptkb:CF34
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:configuration
|
dual-spool
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_base
|
gptkb:Bombardier
|
|
gptkbp:customer_support
|
global support network
|
|
gptkbp:design
|
modular design
30,000 cycles
|
|
gptkbp:development
|
GTF (Geared Turbofan) technology
|
|
gptkbp:diameter
|
81 inches
|
|
gptkbp:elevation
|
up to 40,000 ft
|
|
gptkbp:emissions_standard
|
low NOx
|
|
gptkbp:engine
|
air-start
GTF family
|
|
gptkbp:engine_configuration
|
twin-engine
high bypass ratio
pylon-mounted
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:environmental_impact
|
reduced emissions
|
|
gptkbp:first_flight
|
gptkb:2013
|
|
gptkbp:fuel_economy
|
high efficiency
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW1200 G
|
|
gptkbp:innovation
|
geared architecture
|
|
gptkbp:is_tested_for
|
extensive testing conducted
|
|
gptkbp:length
|
9.5 ft
|
|
gptkbp:maintenance
|
5,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:operational_cost
|
low operational cost
|
|
gptkbp:operational_range
|
regional aircraft
|
|
gptkbp:performance
|
high performance
|
|
gptkbp:power_setting
|
max thrust
|
|
gptkbp:propulsion
|
10.3
18,500 lbf
|
|
gptkbp:related_aircraft
|
CSeries family
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_entry
|
gptkb:2016
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:used_in
|
gptkb:Bombardier_CSeries
|
|
gptkbp:water_requirement
|
1,200 lb/hr
|
|
gptkbp:weight
|
1,800 lb
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_GTF
|
|
gptkbp:bfsLayer
|
6
|