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gptkbp:instance_of
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gptkb:turbofan_engine
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|
gptkbp:application
|
helicopter propulsion
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|
gptkbp:average_temperature
|
up to 1,000 ° F
|
|
gptkbp:components
|
gptkb:turbofan_engine
gptkb:oil_and_gas_industry
gptkb:Noldor
gptkb:Control
gptkb:Blaster
gptkb:gasoline
gptkb:mounts
gptkb:exhaust_system
thermocouples
temperature sensors
pressure sensors
fuel injectors
oil filters
air intake
combustion chamber
mounting brackets
fuel filters
accessory gearbox
compressor blades
turbine blades
starter motor
fuel control unit
ignition leads
accessory drive
vibration isolators
cooling fins
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|
gptkbp:compression_ratio
|
8:1
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|
gptkbp:control_system
|
hydromechanical fuel control
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|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:turbofan_engine
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:emissions_standard
|
meets FAA regulations
|
|
gptkbp:engine_configuration
|
single spool
|
|
gptkbp:exhaust_system
|
axial
|
|
gptkbp:first_introduced
|
1960s
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|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
gptkbp:history
|
derived from T53-L-703
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-741
|
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gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:launch_platform
|
electric starter
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:notable_users
|
gptkb:Sikorsky_CH-54_Tarhe
gptkb:Boeing_CH-47_Chinook
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:operational_range
|
up to 1,000 miles
|
|
gptkbp:power_output
|
1,500 shp
|
|
gptkbp:propulsion
|
1,500 lbf
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:type
|
turbo shaft engine
|
|
gptkbp:used_in
|
gptkb:helicopter
|
|
gptkbp:variant
|
T53-L-703
|
|
gptkbp:weight
|
approximately 400 lb
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_T53-L-703
gptkb:Lycoming_T53-L-91
|
|
gptkbp:bfsLayer
|
8
|