|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
wide-body aircraft
|
|
gptkbp:armament
|
composite
|
|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:bypass_ratio
|
8.5:1
|
|
gptkbp:cancellation_reason
|
yes
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
2.5 m
2.7 m
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:advanced_technology
commercial aviation
innovative technology
global support network
large engine
|
|
gptkbp:engine_configuration
|
modern design
twin-engine
high bypass ratio
pylon-mounted
|
|
gptkbp:engine_emissions
|
low emissions
|
|
gptkbp:engine_modification
|
modification options available
|
|
gptkbp:engine_power
|
high performance
high reliability
high efficiency
30,000 hours
|
|
gptkbp:engine_replacement
|
replacement options available
|
|
gptkbp:engine_type
|
turbofan
high bypass turbofan
compatible with various aircraft
|
|
gptkbp:engine_upgrade
|
upgrade options available
|
|
gptkbp:first_flight
|
gptkb:1990
|
|
gptkbp:fuel_capacity
|
2.7 m
3.5 m
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW4000-113 H
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
low maintenance
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 0.85
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_users
|
gptkb:Boeing_707
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_MD-11
|
|
gptkbp:number_of_engines
|
over 1,000
|
|
gptkbp:propulsion
|
no
113,000 lbf
|
|
gptkbp:service_entry
|
gptkb:1990
|
|
gptkbp:turbine_type
|
high bypass turbofan
|
|
gptkbp:weight
|
4,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_PW4000
|
|
gptkbp:bfsLayer
|
5
|