|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
wide-body aircraft
|
|
gptkbp:armament
|
composite
|
|
gptkbp:bypass_ratio
|
8.5:1
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:configuration
|
dual-spool
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:diameter
|
2.7 m
|
|
gptkbp:emissions_standard
|
reduced
|
|
gptkbp:engine
|
gptkb:PW4000
low emissions
advanced aerodynamics
fuel efficiency
modular design
advanced materials
high reliability
high bypass ratio
easy maintenance
air start
low noise design
robust performance
digital engine control
|
|
gptkbp:engine_configuration
|
pylon-mounted
|
|
gptkbp:engine_type
|
high-bypass turbofan
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
2.7 m
3.5 m
4,500 kg
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:has_historical_building
|
JT9 D
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW4000-113 B
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
long
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_engines
|
over 1,000
|
|
gptkbp:operational_period
|
commercial aviation
|
|
gptkbp:operational_use
|
commercial airline operations
|
|
gptkbp:propulsion
|
113,000 lbf
|
|
gptkbp:regulatory_compliance
|
ICAO Chapter 4
|
|
gptkbp:service_entry
|
gptkb:1995
|
|
gptkbp:thrust_rating
|
113,000 lbf
|
|
gptkbp:turbine_type
|
high-pressure turbine
low-pressure turbine
|
|
gptkbp:uses
|
gptkb:Boeing_707
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_MD-11
|
|
gptkbp:weight
|
4,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_PW4000
|
|
gptkbp:bfsLayer
|
5
|