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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:aircraft_operated
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gptkb:Boeing_CH-47_Chinook
gptkb:Bell_AH-1_Cobra
gptkb:Sikorsky_UH-60_Black_Hawk
gptkb:Mc_Donnell_Douglas_AH-64_Apache
Bell 204/205
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|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1,000 ° F
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
5,000 hours
|
|
gptkbp:developer
|
developed in the 1950s
|
|
gptkbp:diameter
|
approximately 14 in
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
low emissions
single exhaust
|
|
gptkbp:engine
|
gptkb:Lycoming_T53-L-13
gptkb:Lycoming_T53-L-703
Brayton cycle
flexible mount
|
|
gptkbp:engine_type
|
two-stage turbine
single-stage centrifugal compressor
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
dual fuel pumps
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-71
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:investment
|
up to 30 psi
|
|
gptkbp:launch_site
|
electric starter
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:market_segment
|
gptkb:aircraft
|
|
gptkbp:noise_level
|
low vibration
85 d B
|
|
gptkbp:notable_features
|
modular design
|
|
gptkbp:power_output
|
1,400 shp
|
|
gptkbp:predecessor
|
gptkb:Lycoming_T53-L-13
|
|
gptkbp:propulsion
|
1,400 lbf
4.67 shp/lb
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:Lycoming_T53-L-703
|
|
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
|
|
gptkbp:bfsLayer
|
6
|