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gptkbp:instance_of
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gptkb:engine
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gptkbp:application
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gptkb:Boeing_CH-47_Chinook
gptkb:Bell_UH-1_Iroquois
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gptkbp:average_temperature
|
up to 1,000 ° F
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|
gptkbp:compression_ratio
|
12:1
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gptkbp:controls
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gptkb:full_authority_digital_engine_control_(FADEC)
hydromechanical control
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gptkbp:cooling_system
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air-cooled
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gptkbp:diameter
|
approximately 14 in
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gptkbp:drivetrain
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reduction gearbox
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gptkbp:emissions_standard
|
EPA Tier 4
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gptkbp:engine
|
modular design
twin-spool
1,500 shp
electric start
2,500 hours
flexible mount
|
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gptkbp:engine_type
|
gptkb:6
gptkb:engine
2
nickel-based superalloy
|
|
gptkbp:first_flight
|
gptkb:1960
|
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gptkbp:fuel_capacity
|
300 lb
5 gallons
200 gallons
0.5 lb/hp/hr
40 in
14 in
|
|
gptkbp:fuel_type
|
gptkb:railway_station
direct injection
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming T53-L-45
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:launched
|
starter-generator
|
|
gptkbp:length
|
approximately 40 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:max_speed
|
30,000 rpm
|
|
gptkbp:noise_level
|
85 d B
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|
gptkbp:operational_range
|
1,000 miles
|
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gptkbp:power_output
|
1,500 shp
|
|
gptkbp:propulsion
|
5:1
1,500 lbf
turbo-shaft propulsion
|
|
gptkbp:service_ceiling
|
20,000 ft
|
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gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:helicopter
|
|
gptkbp:weight
|
approximately 300 lb
|
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gptkbp:bfsParent
|
gptkb:Lycoming_T53-L-13
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gptkbp:bfsLayer
|
6
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