T58 Engine

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 4
gptkbp:bfsParent gptkb:General_Electric's_aviation_division
gptkbp:application gptkb:helicopter
gptkbp:average_temperature 1,600 ° F
up to 1,000 ° F
gptkbp:controls gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
gptkbp:design 2,000 hours
gptkbp:diameter approximately 14 in
gptkbp:drivetrain reduction gearbox
gptkbp:emissions_standard meets FAA regulations
gptkbp:engine high performance
twin-spool
T58 family
gptkbp:engine_type axial compressor
single-stage turbine
gptkbp:environmental_impact low emissions
gptkbp:features modular design
gptkbp:first_flight gptkb:1956
gptkbp:first_introduced gptkb:1955
gptkbp:fuel_capacity high efficiency
0.5 lb/hp/hr
gptkbp:fuel_type gptkb:Jet_A
dual fuel system
hydromechanical fuel control
gptkbp:historical_event developed in the 1950s
gptkbp:historical_significance pioneering turbo-shaft technology
https://www.w3.org/2000/01/rdf-schema#label T58 Engine
gptkbp:ignition_system spark ignition
gptkbp:is_tested_for extensive testing conducted
gptkbp:length approximately 48 in
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:General_Electric
gptkbp:market widely used in military applications
gptkbp:market_segment gptkb:aircraft
gptkbp:material titanium and nickel alloys
gptkbp:noise_level low noise operation
gptkbp:notable_feature reliability
gptkbp:number_of_stages 14 stages
gptkbp:operational_area multi-role capability
civilian helicopters
gptkbp:operational_range high altitude
gptkbp:power_output 1,000 to 1,500 shp
gptkbp:propulsion 3.5:1
1,400 lbf
gptkbp:regulatory_compliance FAA certified
gptkbp:service_ceiling 20,000 ft
gptkbp:successor gptkb:T700_Engine
gptkbp:type gptkb:engine
gptkbp:used_in gptkb:Boeing_CH-47_Chinook
gptkb:Bell_UH-1_Iroquois
gptkbp:weight approximately 400 lb