|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Bombardier_CSeries
|
|
gptkbp:armament
|
composite
|
|
gptkbp:average_temperature
|
up to 1,600 ° F
|
|
gptkbp:bypass_ratio
|
8.5:1
|
|
gptkbp:cancellation_reason
|
geared architecture
up to 75% compared to previous engines
|
|
gptkbp:certification
|
multiple certifications obtained
FAA type certificate
|
|
gptkbp:combustor_type
|
annular
annular combustor
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
81 in
|
|
gptkbp:emissions_standard
|
CAEP/6
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:Geared_Turbofan_family
global support network
regional jets
future upgrades planned
ongoing development efforts
|
|
gptkbp:engine_configuration
|
modular design
|
|
gptkbp:engine_power
|
high reliability
high efficiency
optimized performance
|
|
gptkbp:engine_type
|
multiple variants available
|
|
gptkbp:first_flight
|
gptkb:2013
|
|
gptkbp:fuel_capacity
|
60 in
81 in
118 in
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
gptkbp:has_programs
|
gptkb:Geared_Turbofan_program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW1500 G engine
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:maintenance
|
20,000 hours
5,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low noise
low vibration
|
|
gptkbp:number_of_engines
|
2
over 1,000
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_range
|
up to 3,300 nautical miles
-40 to 50 ° C
|
|
gptkbp:propulsion
|
15,590 lbf
8.66:1
|
|
gptkbp:service_entry
|
gptkb:2016
|
|
gptkbp:turbine_type
|
2
single crystal superalloy
|
|
gptkbp:type
|
geared turbofan engine
geared turbofan
|
|
gptkbp:warranty
|
comprehensive warranty
|
|
gptkbp:weight
|
1,800 lb
3,500 lb
|
|
gptkbp:bfsParent
|
gptkb:PW1000_G_engine
|
|
gptkbp:bfsLayer
|
6
|