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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:application
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gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° F
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:controls
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gptkb:full_authority_digital_engine_control_(FADEC)
electronic control system
|
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gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:emissions_standard
|
single exhaust outlet
|
|
gptkbp:engine
|
high reliability
twin-spool
commercial helicopters
axial-flow compressor
flexible mount system
starter-generator system
T53-L-701
T53-L-703
|
|
gptkbp:engine_type
|
free turbine
turbo-shaft
T53-L-13
T53-L-701
T53-L-703
T53-L-37
|
|
gptkbp:features
|
modular design
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
0.5 lb/hp/hr
dry sump
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
fuel pump and control unit
|
|
gptkbp:historical_event
|
developed for military use
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-37
|
|
gptkbp:ignition_system
|
dual ignition system
|
|
gptkbp:is_tested_for
|
extensive ground testing
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:max_speed
|
42,000 rpm
|
|
gptkbp:operational_range
|
varies by application
|
|
gptkbp:power_output
|
1,400 shp
|
|
gptkbp:propulsion
|
1,400 lbf
4.67 hp/lb
|
|
gptkbp:status
|
in production
|
|
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
|