T53-L-13 engine

GPTKB entity

Statements (61)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:helicopter
gptkbp:average_temperature up to 1,000 ° F
gptkbp:certification FAA certified
gptkbp:components gptkb:spark_plug
gptkb:exhaust_system
oil cooler
mounting brackets
reduction gearbox
compressor blades
turbine blades
fuel filter
fuel control unit
gptkbp:compression_ratio 8:1
gptkbp:compressor_type five
axial compressor
gptkbp:configuration free turbine
gptkbp:control_system digital control system
hydromechanical fuel control
gptkbp:cooling_system air-cooled
oil-based coolant
gptkbp:development developed in the 1950s
gptkbp:diameter approximately 14 in
gptkbp:displacement 1,200 in³
gptkbp:emissions_standard meets FAA regulations
gptkbp:engine Brayton cycle
gptkbp:engine_configuration flexible mount system
gptkbp:facilities General Electric test facility
gptkbp:first_flight gptkb:1955
gptkbp:fuel_economy 0.5 lb/hp/hr
good fuel efficiency
gptkbp:fuel_type gptkb:gasoline
gptkb:Jet_A
gptkbp:gearbox reduction gearbox
https://www.w3.org/2000/01/rdf-schema#label T53-L-13 engine
gptkbp:ignition_system spark ignition
gptkbp:investment up to 30 psi
gptkbp:launch_date approximately 30 seconds
gptkbp:legacy used in various helicopter models
gptkbp:length approximately 40 in
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:General_Electric
gptkbp:market military and civilian markets
gptkbp:modifications various upgrades available
gptkbp:noise_level moderate noise level
gptkbp:operating_life up to 5,000 hours
gptkbp:operational_range up to 30,000 ft
gptkbp:power_output 1,100 shp
gptkbp:propulsion 3.67:1
1,100 lb
gptkbp:reliability high reliability
gptkbp:service_history widely used in Vietnam War
gptkbp:successor T53-L-703
gptkbp:turbine_type two
free power turbine
nickel-based superalloy
gptkbp:type turbo-shaft
gptkbp:used_in gptkb:Bell_UH-1_Iroquois
gptkbp:weight approximately 300 lb
gptkbp:bfsParent gptkb:UH-1_Iroquois
gptkbp:bfsLayer 5