|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:air_support
|
1,000 lb/sec
|
|
gptkbp:application
|
gptkb:Boeing_707
gptkb:Airbus
|
|
gptkbp:armament
|
composite
|
|
gptkbp:average_temperature
|
up to 1,600 ° F
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_air_source
|
fan air
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
high bypass ratio
|
|
gptkbp:diameter
|
94 inches
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:PW4000-100_R
gptkb:PW4000-112
gptkb:PW4000-94
global support network
PW4000 series
approximately 20,000 hours
|
|
gptkbp:engine_configuration
|
high performance
twin-engine
pylon-mounted
|
|
gptkbp:engine_power
|
high reliability
|
|
gptkbp:engine_upgrade_options
|
performance improvement packages
|
|
gptkbp:first_flight
|
gptkb:1986
|
|
gptkbp:fuel_capacity
|
approximately 2.5 ft
approximately 12.5 ft
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW4000-100 engine
|
|
gptkbp:is_tested_for
|
Pratt & Whitney facilities
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:market_segment
|
wide-body aircraft
|
|
gptkbp:maximum_continuous_thrust
|
30,000 lbf
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:notable_feature
|
modular design
|
|
gptkbp:operational_range
|
up to 40,000 ft
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:propulsion
|
cascade
18,500 to 33,000 lbf
33,000 lbf
|
|
gptkbp:service_entry
|
gptkb:1990
|
|
gptkbp:turbine_type
|
2
single crystal superalloy
|
|
gptkbp:type
|
dual spool
dual-spool
|
|
gptkbp:warranty
|
standard warranty terms
|
|
gptkbp:weight
|
approximately 8,000 lb
|