|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° F
1,000 ° F
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:controls
|
hydromechanical fuel control
hydromechanical control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
single exhaust
|
|
gptkbp:engine
|
military and civilian applications
twin-spool
two stages
flexible mount
1,400 shp
starter-generator system
|
|
gptkbp:engine_type
|
gptkb:engine
reduction gearbox
two turbine stages
single exhaust system
three axial compressor stages
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
300 lb
0.5 lb/hp/hr
40 in
14 in
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular combustion chamber
Jet A or Jet B
gear-type fuel pump
gear-type pump
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-83
|
|
gptkbp:ignition_system
|
dual ignition system
|
|
gptkbp:launched
|
starter-generator
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:number_of_stages
|
three stages
|
|
gptkbp:operational_range
|
up to 30,000 ft
|
|
gptkbp:power_output
|
1,400 shp
|
|
gptkbp:propulsion
|
4.67
4.67 hp/lb
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:torque
|
3,000 lb-ft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:variant
|
T53-L-703
|
|
gptkbp:weight
|
approximately 300 lb
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_T53-L-13
|
|
gptkbp:bfsLayer
|
6
|