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gptkbp:instance_of
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gptkb:turbofan_engine
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|
gptkbp:application
|
wide-body aircraft
|
|
gptkbp:armament
|
gptkb:textiles
|
|
gptkbp:average_temperature
|
up to 1,600 ° F
|
|
gptkbp:bypass_ratio
|
8:1
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|
gptkbp:certification
|
gptkb:Federal_Aviation_Administration_(FAA)
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:configuration
|
dual-spool
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:diameter
|
approximately 3.0 ft
approximately 8.5 ft
|
|
gptkbp:emissions_standard
|
NOx compliant
|
|
gptkbp:engine
|
gptkb:East_Hartford,_Connecticut
gptkb:PW4000_family
|
|
gptkbp:engine_configuration
|
high bypass turbofan
|
|
gptkbp:engine_type
|
gptkb:PW4000-100
gptkb:PW4000-112
gptkb:PW4000-94
gptkb:PW4000-114
gptkb:PW4000-115
PW4000-113
PW4000-126 D
PW4000-126 E
PW4000-126 F
PW4000-126 H
PW4000-126 K
PW4000-126 L
PW4000-126 M
PW4000-126 N
PW4000-126 P
PW4000-126 Q
PW4000-126 R
PW4000-126 S
PW4000-126 T
PW4000-126 U
PW4000-126 V
PW4000-126 W
PW4000-126 X
PW4000-126 Y
PW4000-126 Z
|
|
gptkbp:first_flight
|
gptkb:1990
|
|
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
|
PW4000-126
|
|
gptkbp:is_tested_for
|
Pratt & Whitney's test facility
|
|
gptkbp:length
|
approximately 11.5 ft
|
|
gptkbp:maintenance
|
approximately 6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:maximum_diameter
|
approximately 2.9 ft
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:notable_users
|
gptkb:Boeing_707
gptkb:Airbus
|
|
gptkbp:propulsion
|
up to 26,000 lbf
|
|
gptkbp:service_entry
|
gptkb:1992
|
|
gptkbp:turbine_type
|
2
single crystal superalloy
|
|
gptkbp:weight
|
approximately 4,000 lb
|
|
gptkbp:bfsParent
|
gptkb:PW4000-112
gptkb:PW4000-112_H
gptkb:PW4000_engine
|
|
gptkbp:bfsLayer
|
6
|