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gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
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gptkb:Lycoming_T53-L-13
|
|
gptkbp:accessories
|
various accessories available
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° F
|
|
gptkbp:certification
|
FAA certified
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|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
hydromechanical fuel control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:drivetrain
|
integrated reduction gearbox
|
|
gptkbp:emissions_standard
|
low emissions
single exhaust outlet
|
|
gptkbp:engine
|
Brayton cycle
T53-L-701
flexible engine mount
|
|
gptkbp:engine_type
|
two-stage turbine
turbo-shaft
|
|
gptkbp:features
|
modular design
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
0.5 lb/hp/hr
dry sump oil system
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular combustor
dual fuel pumps
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-1
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:investment
|
up to 30 psi
|
|
gptkbp:launch_site
|
air start
|
|
gptkbp:legacy
|
widely used in helicopters
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:market
|
military and civilian markets
|
|
gptkbp:max_speed
|
30,000 rpm
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:power_output
|
1,100 shp
|
|
gptkbp:produced_by
|
over 10,000 units
|
|
gptkbp:production_years
|
1955-1980s
|
|
gptkbp:propulsion
|
1,100 lbf
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:services
|
gptkb:1956
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:successor
|
T53-L-703
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:variant
|
T53-L-13
|
|
gptkbp:water_source
|
integrated fuel filter
|
|
gptkbp:weight
|
lightweight design
approximately 300 lb
|