Lycoming T53-L-51

GPTKB entity

Statements (56)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:application gptkb:helicopter
gptkbp:average_temperature up to 1,000 ° F
gptkbp:compression_ratio 8:1
gptkbp:controls gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
gptkbp:design military helicopter propulsion
gptkbp:diameter approximately 14 in
gptkbp:drivetrain reduction gearbox
gptkbp:emissions_standard low emissions
single exhaust
gptkbp:engine gptkb:Lycoming_T53-L-13
gptkb:Lycoming_T53-L-703
Brayton cycle
flexible mount
single spool
up to 5,000 hours
gptkbp:first_flight gptkb:1960
gptkbp:fuel_capacity high fuel efficiency
0.5 lb/hp/hr
dry sump oil system
gptkbp:fuel_type gptkb:Jet_A
annular combustion chamber
dual fuel system
gptkbp:historical_event developed in the late 1950s
gptkbp:historical_significance significant in military aviation history
https://www.w3.org/2000/01/rdf-schema#label Lycoming T53-L-51
gptkbp:ignition_system dual ignition system
gptkbp:investment up to 30 psi
gptkbp:is_tested_for extensively tested
gptkbp:launched air start
gptkbp:length approximately 40 in
gptkbp:maintenance 500 hours
moderate maintenance cost
gptkbp:manufacturer gptkb:Lycoming_Engines
gptkbp:market widely available
gptkbp:market_segment gptkb:aircraft
gptkbp:material aluminum and titanium
gptkbp:max_speed 30,000 rpm
gptkbp:noise_level moderate noise level
gptkbp:operational_range varied operational range
gptkbp:power_output 1,400 shp
gptkbp:predecessor T53-L-13
gptkbp:propulsion 4.67:1
gptkbp:regulatory_compliance FAA certified
gptkbp:service_history used in various military operations
gptkbp:setting free turbine
gptkbp:successor T53-L-703
gptkbp:torque 1,200 lb-ft
gptkbp:type gptkb:engine
gptkbp:used_in gptkb:Bell_UH-1_Iroquois
gptkbp:variant T53-L-13
T53-L-703
gptkbp:weight approximately 300 lb
gptkbp:bfsParent gptkb:Lycoming_T53-L-13
gptkbp:bfsLayer 6