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gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:air_support
|
2,000 lb/min
|
|
gptkbp:application
|
gptkb:business_jet
|
|
gptkbp:average_temperature
|
1,600 ° F
|
|
gptkbp:bypass_ratio
|
8.5:1
|
|
gptkbp:certification
|
CAEP/6
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compression_ratio
|
24:1
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:configuration
|
twin-spool
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_purpose
|
high efficiency
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
1.1 m
36 in
|
|
gptkbp:elevation
|
51,000 ft
|
|
gptkbp:emissions_standard
|
low NOx
|
|
gptkbp:engine
|
bleed air start
|
|
gptkbp:engine_configuration
|
high bypass ratio
pylon-mounted
|
|
gptkbp:engine_power
|
high reliability
18,500 lbf
|
|
gptkbp:fan_blades_material
|
composite
|
|
gptkbp:first_flight
|
gptkb:2016
|
|
gptkbp:fuel_capacity
|
1,800 lb
36 in
69.5 in
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW800-79 engine
|
|
gptkbp:is_tested_for
|
gptkb:Pratt_&_Whitney's_West_Palm_Beach
|
|
gptkbp:length
|
3.5 m
69.5 in
|
|
gptkbp:maintenance
|
5,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:maximum_continuous_thrust
|
17,000 lbf
|
|
gptkbp:noise_level
|
gptkb:Stage_4
Stage 4 compliant
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:propulsion
|
cascade
18,500 lbf
|
|
gptkbp:service_entry
|
gptkb:2018
|
|
gptkbp:turbine_blades_material
|
single crystal superalloy
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
high-bypass turbofan
twin-spool
|
|
gptkbp:used_in
|
gptkb:Bombardier_Global_7500
|
|
gptkbp:warranty
|
5 years
|
|
gptkbp:weight
|
1,200 kg
1,800 lb
|