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gptkbp:instance_of
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gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Flight
|
|
gptkbp:average_temperature
|
high pressure turbine
|
|
gptkbp:bypass_ratio
|
9:1
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|
gptkbp:cancellation_reason
|
geared architecture
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:competitors
|
gptkb:Rolls-Royce_Trent_1000
|
|
gptkbp:components
|
gptkb:spark_plug
gptkb:oil_and_gas_industry
gptkb:Noldor
gptkb:sports_equipment
gptkb:gasoline
gptkb:sensors
gptkb:exhaust_system
mounting bracket
engine control unit
piping
bearing
air intake
air seal
casing
shaft
accessory gearbox
thrust reverser
high pressure turbine
low pressure turbine
engine nacelle
control valves
vibration monitoring system
fuel nozzle
fan blade
high bypass ratio fan
accessory drive
engine mount
bypass duct
compressor blade
high pressure compressor
low pressure compressor
turbine blade
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
advanced cooling techniques
|
|
gptkbp:design_feature
|
advanced materials
|
|
gptkbp:diameter
|
81 inches
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:has_programs
|
GTF program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW1200 G-3
|
|
gptkbp:legal_principle
|
gptkb:jet_engine
|
|
gptkbp:maintenance
|
longer than previous models
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:market_segment
|
commercial aviation
|
|
gptkbp:original_run
|
gptkb:2013
|
|
gptkbp:propulsion
|
up to 23,300 lbf
|
|
gptkbp:related_aircraft
|
CSeries family
|
|
gptkbp:type
|
geared turbofan engine
|
|
gptkbp:used_in
|
gptkb:Bombardier_CSeries
|
|
gptkbp:weight
|
approximately 1,500 lb
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_PW1200_G
|
|
gptkbp:bfsLayer
|
6
|