|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_T53-L-13
|
|
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
|
2,500 hours
|
|
gptkbp:developer
|
developed in the 1950s
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:drivetrain
|
integrated reduction gearbox
|
|
gptkbp:emissions_standard
|
low emissions
axial exhaust
|
|
gptkbp:engine
|
gptkb:Lycoming_T53-L-704
gptkb:Lycoming_T53-L-705
gptkb:Lycoming_T53-L-706
gptkb:Lycoming_T53-L-707
gptkb:Lycoming_T53-L-708
gptkb:Lycoming_T53-L-709
gptkb:Lycoming_T53-L-710
gptkb:Lycoming_T53-L-701
modular design
Brayton cycle
starter-generator system
Lycoming T53-L-702
|
|
gptkbp:engine_type
|
gptkb:engine
three
two
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
high efficiency
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical fuel control
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-69
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:investment
|
up to 30 psi
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:max_speed
|
42,000 rpm
|
|
gptkbp:modifications
|
various military modifications
|
|
gptkbp:noise_level
|
low noise
low vibration
|
|
gptkbp:operational_range
|
wide operating range
|
|
gptkbp:power_output
|
1,400 shp
|
|
gptkbp:powers
|
3.5 hp/lb
|
|
gptkbp:predecessor
|
gptkb:Lycoming_T53-L-1
|
|
gptkbp:propulsion
|
3.5:1
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:successor
|
gptkb:Lycoming_T53-L-703
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:weight
|
approximately 400 lb
|