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