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gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
4
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|
gptkbp:bfsParent
|
gptkb:General_Electric's_aviation_division
|
|
gptkbp:aircraft_operated
|
F-22 Raptor, F-35 Lightning II
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
1,600 ° F
|
|
gptkbp:awarded_by
|
gptkb:1986
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:developer
|
$1 billion
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:emissions_standard
|
variable geometry
Nox standard compliant
|
|
gptkbp:engine
|
gptkb:advanced_technology
gptkb:East_Hartford,_Connecticut
gptkb:F119_family
2
high reliability
6,000 hours
twin-spool
superior performance
global support network
air start
low operational cost
ongoing R& D efforts
F120 Engine
effective lifecycle management
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:first_introduced
|
gptkb:1991
|
|
gptkbp:fuel_capacity
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-8
annular combustor
electronic fuel control
|
|
gptkbp:has_programs
|
gptkb:Advanced_Tactical_Fighter_(ATF)_program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119 Engine
|
|
gptkbp:is_designed_for
|
gptkb:F-22_Raptor
|
|
gptkbp:is_tested_for
|
Pratt & Whitney test facility
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_area
|
gptkb:2005
|
|
gptkbp:operational_range
|
2,000 miles
|
|
gptkbp:performance
|
continuous improvement program
|
|
gptkbp:propulsion
|
gptkb:battle
4.67
70,000 lbf
35,000 lbf
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:upgrades
|
F119-PW-100 upgrade
|
|
gptkbp:warranty
|
5 years
|
|
gptkbp:weight
|
1,500 lb
|