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gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional jets
|
|
gptkbp:armament
|
wide-chord fan blades
|
|
gptkbp:bypass_ratio
|
5.5:1
|
|
gptkbp:certification
|
gptkb:EASA
gptkb:FAA
CAEP/6
FAA certified
|
|
gptkbp:combustor_type
|
annular
annular combustor
|
|
gptkbp:competitors
|
gptkb:RB211
gptkb:CF34
|
|
gptkbp:compressor_type
|
gptkb:10
gptkb:6
aluminum alloy
|
|
gptkbp:configuration
|
twin-spool
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_support
|
global
|
|
gptkbp:design
|
high
|
|
gptkbp:design_purpose
|
low emissions
high efficiency
low noise
|
|
gptkbp:development
|
gptkb:Partnerships
|
|
gptkbp:diameter
|
1.8 m
2.5 m
1.9 m
|
|
gptkbp:elevation
|
40,000 ft
|
|
gptkbp:emissions_standard
|
CAEP/6 compliant
|
|
gptkbp:engine
|
gptkb:PW6000
Brayton cycle
air start
|
|
gptkbp:engine_configuration
|
twin-spool
pylon-mounted
twin-engine configuration
|
|
gptkbp:engine_design_life
|
20,000 hours
|
|
gptkbp:engine_maintenance_cost
|
low maintenance cost
|
|
gptkbp:engine_power
|
high reliability
60,000 lbf
high efficiency
high fuel efficiency
|
|
gptkbp:engine_type
|
PW6000-3
|
|
gptkbp:engine_upgrade_path
|
yes
|
|
gptkbp:engine_vibration_level
|
low vibration level
|
|
gptkbp:engine_weight_to_thrust_ratio
|
50:1
|
|
gptkbp:environmental_impact
|
reduced
|
|
gptkbp:first_flight
|
gptkb:1998
|
|
gptkbp:fuel_capacity
|
2.5 m
3.5 m
50 liters
|
|
gptkbp:fuel_economy
|
high
0.5 lb/hp/hr
low fuel consumption
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW6000-1 engine
|
|
gptkbp:innovation
|
advanced materials
aerodynamic design
digital engine control
|
|
gptkbp:is_tested_for
|
extensive
Pratt & Whitney test facility
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
6,000 hours
5,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:market_position
|
high
|
|
gptkbp:market_segment
|
commercial aviation
|
|
gptkbp:maximum_operating_temperature
|
1,600 ° F
|
|
gptkbp:noise_level
|
Stage 3
Stage 4 compliant
advanced noise reduction technology
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_cost
|
low
|
|
gptkbp:operational_range
|
long-haul
|
|
gptkbp:partnerships
|
research institutions
aircraft manufacturers
|
|
gptkbp:performance
|
efficient
|
|
gptkbp:project
|
next-gen engines
|
|
gptkbp:propulsion
|
yes
60,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:2000
|
|
gptkbp:sustainability
|
focus on green technology
|
|
gptkbp:turbine_type
|
2
single-crystal superalloy
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:upgrades
|
available
|
|
gptkbp:used_in
|
gptkb:Airbus
|
|
gptkbp:warranty
|
5 years
|
|
gptkbp:weight
|
3,000 kg
|