|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional jets
|
|
gptkbp:average_temperature
|
up to 1,600 ° F
|
|
gptkbp:bypass_ratio
|
9:1
|
|
gptkbp:cancellation_reason
|
up to 75% compared to previous engines
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:competitors
|
gptkb:CF34-10_E
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:configuration
|
twin-spool
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:customer_support
|
gptkb:Bombardier
|
|
gptkbp:design_purpose
|
improve fuel efficiency
|
|
gptkbp:development
|
part of the Geared Turbofan family
|
|
gptkbp:diameter
|
81 inches
|
|
gptkbp:emissions_standard
|
meets CAEP/6 standards
|
|
gptkbp:engine
|
Pure Power
|
|
gptkbp:engine_configuration
|
high bypass ratio
|
|
gptkbp:first_flight
|
gptkb:2013
|
|
gptkbp:fuel_capacity
|
approximately 10.5 ft
approximately 2.1 ft
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
planetary gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW1200 G-8
|
|
gptkbp:maintenance
|
up to 10,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:market_segment
|
commercial aviation
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:propulsion
|
up to 23,300 lbf
|
|
gptkbp:service_entry
|
gptkb:2016
|
|
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
|