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gptkbp:instance_of
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gptkb:engine
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gptkbp:application
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gptkb:helicopter
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gptkbp:compression_ratio
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8:1
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gptkbp:controls
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digital control system
hydromechanical fuel control
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gptkbp:cooling_system
|
air-cooled
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gptkbp:diameter
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approximately 14 in
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gptkbp:emissions_standard
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EPA Tier 4
straight exhaust
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gptkbp:engine
|
gptkb:Lycoming_T53-L-13
gptkb:Lycoming_T53-L-703
developed in the 1950s
3,000 hours
mounting frame
horizontal shaft
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gptkbp:engine_type
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gptkb:engine
aluminum alloy
three
two
axial compressor
free power turbine
nickel-based superalloy
T53-L-13, T53-L-703
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|
gptkbp:first_flight
|
gptkb:1960
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|
gptkbp:fuel_capacity
|
0.5 lb/hp/hr
dry sump
40 in x 14 in
|
|
gptkbp:fuel_type
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gptkb:Jet_A
gptkb:railway_station
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-57
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|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
bench testing
Lycoming test facility
|
|
gptkbp:launch_site
|
electric starter
|
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gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:max_speed
|
42,000 rpm
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:operational_range
|
-40 to 60 ° C
|
|
gptkbp:power_output
|
1,400 shp
|
|
gptkbp:propulsion
|
4.67
4.67 shp/lb
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:status
|
in production
|
|
gptkbp:torque
|
splash lubrication
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Bell_UH-1_Iroquois
|
|
gptkbp:weight
|
300 lb
approximately 300 lb
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_T53-L-13
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gptkbp:bfsLayer
|
6
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