|
gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:application
|
military transport aircraft
passenger aircraft
cargo_aircraft
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:countryOfOrigin
|
gptkb:Soviet_Union
|
|
gptkbp:design
|
low noise operation
high power-to-weight ratio
high efficiency
modular construction
low vibration
robust construction
reduction gearbox
low maintenance requirements
reversible pitch propeller
high thrust output
integrated fuel system
|
|
gptkbp:designedBy
|
gptkb:Ivchenko_Design_Bureau
|
|
gptkbp:diameter
|
1,200 mm
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_3
|
|
gptkbp:engine
|
air-cooled
electric starter
wing-mounted
|
|
gptkbp:engineConfiguration
|
twin-engine
|
|
gptkbp:engineType
|
turboprop
axial
single-stage
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:fuelCapacity
|
0.5 kg/hp/hr
|
|
gptkbp:fuelType
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ivchenko AI-20
|
|
gptkbp:length
|
2,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:maxSpeed
|
600 km/h
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:notableUsers
|
gptkb:Egyptian_Air_Force
gptkb:Soviet_Air_Force
gptkb:Indian_Air_Force
gptkb:Cuban_Air_Force
Aeroflot
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:performances
|
5,000 hours
|
|
gptkbp:powerOutput
|
4,000 hp
|
|
gptkbp:productionYears
|
1955-1980
|
|
gptkbp:propulsion
|
2.5
3,000 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
10,000 m
|
|
gptkbp:setting
|
two-shaft
|
|
gptkbp:successor
|
AI-25
|
|
gptkbp:totalGoals
|
over 10,000
|
|
gptkbp:usedIn
|
gptkb:Tupolev_Tu-95
gptkb:Antonov_An-12
|
|
gptkbp:weight
|
1,200 kg
|