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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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gptkb:transport_aircraft
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gptkbp:armament
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gptkb:4
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gptkbp:compression_ratio
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12:1
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gptkbp:configuration
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two-shaft
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:cooling_system
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gptkb:Interpol
air-cooled
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gptkbp:design
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robust and efficient
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gptkbp:development
|
1950s
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gptkbp:diameter
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1,100 mm
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gptkbp:emissions_standard
|
compliant with standards
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gptkbp:engine
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advanced aerodynamics
air-start
widely used in aviation history
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gptkbp:engine_configuration
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wing-mounted
various upgrades available
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gptkbp:engine_emissions_control
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environmentally friendly design
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gptkbp:engine_power
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high efficiency
proven track record
5,000 hours
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gptkbp:engine_type
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turboprop
high bypass turboprop engine
compatible with various aircraft types
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gptkbp:first_flight
|
gptkb:1955
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gptkbp:fuel_capacity
|
1,200 kg
1,800 mm
1,100 mm
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|
gptkbp:fuel_economy
|
optimized for performance
0.5 kg/k W·h
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gptkbp:fuel_type
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kerosene
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Ivchenko AI-20 M
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gptkbp:length
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1,800 mm
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gptkbp:maintenance
|
easy access
1,000 hours
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gptkbp:manufacturer
|
Ivchenko
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gptkbp:noise_level
|
low
designed for low noise
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gptkbp:notable_users
|
gptkb:Soviet_Air_Force
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gptkbp:operational_range
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1,500 km
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gptkbp:power_output
|
2,900 k W
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gptkbp:powers
|
2.4 k W/kg
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gptkbp:produces
|
over 10,000
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gptkbp:production_years
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1955-1980
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gptkbp:propeller
|
variable-pitch
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gptkbp:propulsion
|
4,000 lbf
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gptkbp:reliability
|
high
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gptkbp:service_ceiling
|
8,000 m
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gptkbp:successor
|
AI-22
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gptkbp:thrust-to-weight_ratio
|
3.33
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gptkbp:used_in
|
gptkb:Antonov_An-12
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gptkbp:variant
|
AI-20 D
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gptkbp:weight
|
1,200 kg
3,000 kg
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gptkbp:bfsParent
|
gptkb:Antonov_An-32
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gptkbp:bfsLayer
|
6
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