|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Flight
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:bypass_ratio
|
8:1
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:components
|
gptkb:turbofan_engine
gptkb:fans
gptkb:Noldor
gptkb:Control
gptkb:safety_equipment
gptkb:gasoline
gptkb:mounts
gptkb:exhaust_system
accessory gearbox
|
|
gptkbp:compressor_type
|
gptkb:10
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
30,000 hours
|
|
gptkbp:design_feature
|
advanced materials
|
|
gptkbp:design_purpose
|
fuel efficiency
|
|
gptkbp:diameter
|
81 in
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:PW1500_G
Brayton cycle
|
|
gptkbp:fuel_economy
|
15% over previous models
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
gptkbp:has_programs
|
gptkb:Geared_Turbofan_program
|
|
gptkbp:height
|
40 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW1200 G-2
|
|
gptkbp:legal_principle
|
jet propulsion
|
|
gptkbp:length
|
118 in
|
|
gptkbp:maintenance
|
longer intervals
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:market_segment
|
commercial aviation
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
high bypass ratio
|
|
gptkbp:original_run
|
gptkb:2013
|
|
gptkbp:propulsion
|
18,000 lbf
|
|
gptkbp:rating
|
high thrust-to-weight ratio
|
|
gptkbp:service_entry
|
gptkb:2016
|
|
gptkbp:target_aircraft
|
regional airliners
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
geared turbofan engine
|
|
gptkbp:used_in
|
gptkb:Bombardier_CSeries
|
|
gptkbp:weight
|
1,500 lb
|
|
gptkbp:width
|
40 in
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_PW1200_G
|
|
gptkbp:bfsLayer
|
6
|