gptkbp:instance_of
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gptkb:engine
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gptkbp:application
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gptkb:helicopter
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gptkbp:availability
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widely supported
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gptkbp:average_temperature
|
up to 1,000 ° F
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gptkbp:certification
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FAA certified
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gptkbp:compression_ratio
|
8:1
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gptkbp:controls
|
hydromechanical fuel control
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gptkbp:cooling_system
|
air-cooled
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gptkbp:diameter
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approximately 14 in
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gptkbp:drivetrain
|
reduction gearbox
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gptkbp:emissions_standard
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meets military standards
axial exhaust
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gptkbp:engine
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gptkb:engine
Brayton cycle
electric starter
up to 5,000 hours
T53-L-703
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gptkbp:engine_type
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free turbine
centrifugal compressor
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gptkbp:features
|
modular design
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gptkbp:first_flight
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gptkb:1960
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gptkbp:fuel_capacity
|
varies by application
high fuel efficiency
0.5 lb/hp/hr
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gptkbp:fuel_type
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gptkb:Jet_A
annular combustor
dual fuel system
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gptkbp:historical_event
|
developed in the late 1950s
|
https://www.w3.org/2000/01/rdf-schema#label
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Lycoming T53-L-47
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gptkbp:ignition_system
|
spark ignition
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gptkbp:is_tested_for
|
digital engine monitoring system
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gptkbp:legacy
|
used in many military helicopters
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gptkbp:length
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approximately 40 in
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gptkbp:maintenance
|
500 hours
low maintenance requirements
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gptkbp:manufacturer
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gptkb:Lycoming_Engines
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gptkbp:market_segment
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gptkb:aircraft
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gptkbp:max_speed
|
2,000 rpm
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gptkbp:noise_level
|
low noise level
low vibration level
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gptkbp:number_of_stages
|
2
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gptkbp:operational_area
|
moderate operational cost
helicopter propulsion
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gptkbp:operational_history
|
used in various military applications
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gptkbp:operational_range
|
long operational range
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gptkbp:power_output
|
1,400 shp
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gptkbp:propulsion
|
4.67
0.71 lb/shp
4.67 hp/lb
|
gptkbp:reliability
|
high reliability
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gptkbp:safety_features
|
multiple safety features
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gptkbp:service_ceiling
|
20,000 ft
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gptkbp:sport
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high endurance
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gptkbp:type
|
turbo shaft engine
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gptkbp:used_in
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gptkb:Bell_UH-1_Iroquois
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gptkbp:variant
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T53-L-13
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gptkbp:weight
|
approximately 300 lb
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gptkbp:bfsParent
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gptkb:Lycoming_T53-L-13
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gptkbp:bfsLayer
|
6
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