|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Flight
|
|
gptkbp:cancellation_reason
|
yes
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
high bypass ratio
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:development
|
gptkb:GTF_engine_family
|
|
gptkbp:diameter
|
81 inches
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:fuel_economy
|
improved over previous models
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW1200 G-4
|
|
gptkbp:maintenance
|
longer than conventional engines
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:market_launch
|
gptkb:2016
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:operational_use
|
commercial aviation
|
|
gptkbp:original_run
|
gptkb:2013
|
|
gptkbp:propulsion
|
up to 23,300 lbf
|
|
gptkbp:target_aircraft
|
regional and narrow-body jets
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
geared turbofan engine
|
|
gptkbp:used_in
|
gptkb:Bombardier_CSeries
|
|
gptkbp:weight
|
approximately 3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_PW1200_G
|
|
gptkbp:bfsLayer
|
6
|