|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
1,000 ° F
|
|
gptkbp:combustor_type
|
annular combustion chamber
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:control_system
|
hydromechanical control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:jet_engine
|
|
gptkbp:development
|
1950s
|
|
gptkbp:diameter
|
14 in
|
|
gptkbp:emissions_standard
|
Stage 3
|
|
gptkbp:engine
|
gptkb:General_Electric_T700
gptkb:General_Electric_T64
gptkb:General_Electric_T58-GE-10
gptkb:General_Electric_T58-GE-400
gptkb:General_Electric_T58-GE-8
|
|
gptkbp:engine_configuration
|
single spool
|
|
gptkbp:exhaust_system
|
axial exhaust
|
|
gptkbp:first_flight
|
gptkb:1958
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric T58
|
|
gptkbp:length
|
42 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:notable_users
|
gptkb:Royal_Air_Force
gptkb:Royal_Canadian_Air_Force
gptkb:US_Army
gptkb:US_Navy
|
|
gptkbp:operational_use
|
1960s
|
|
gptkbp:power_output
|
1,000 shp
|
|
gptkbp:propulsion
|
1,400 lbf
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:successor
|
gptkb:General_Electric_T700
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Boeing_CH-47_Chinook
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:weight
|
300 lb
|
|
gptkbp:bfsParent
|
gptkb:CH-124_Sea_King
|
|
gptkbp:bfsLayer
|
6
|