|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_T53-L-703
gptkb:Lycoming_T53-L-91
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° F
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:controls
|
hydromechanical fuel control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
approximately 14 in
up to 20,000 rpm
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
single exhaust outlet
|
|
gptkbp:engine
|
modular design
Brayton cycle
electric starter
free turbine
flexible mount
single stage
1,400 shp
T53 family
|
|
gptkbp:engine_type
|
turbo shaft engine
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:first_introduced
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
300 lb
0.5 lb/hp/hr
40 in
14 in
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
dual fuel pumps
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-734
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:notable_users
|
gptkb:military_unit
|
|
gptkbp:power_output
|
1,400 shp
|
|
gptkbp:propulsion
|
1,400 lbf
4.67 shp/lb
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:status
|
in production
|
|
gptkbp:type
|
turbo shaft engine
|
|
gptkbp:used_in
|
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:weight
|
approximately 300 lb
|