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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° F
up to 1,600 ° F
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
electronic control system
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|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
military helicopter propulsion
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
single exhaust
|
|
gptkbp:engine
|
gptkb:Lycoming_T53-L-13
gptkb:Lycoming_T53-L-703
modular design
Brayton cycle
flexible mount
starter motor
2,000 hours
|
|
gptkbp:engine_type
|
free turbine
centrifugal compressor
T53-L-13
T53-L-701
T53-L-703
T53-L-703 A
multi-spool engine
T53-L-703 B
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
dual fuel system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-85
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
extensively tested
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:max_speed
|
42,000
|
|
gptkbp:notable_users
|
gptkb:aircraft
gptkb:military_unit
gptkb:battle
|
|
gptkbp:power_output
|
1,400 shp
|
|
gptkbp:propulsion
|
4.67:1
4.67 hp/lb
|
|
gptkbp:service_history
|
used in various military applications
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:weight
|
approximately 300 lb
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_T53-L-13
|
|
gptkbp:bfsLayer
|
6
|