Ilyushin AI-14 R

URI: https://gptkb.org/entity/Ilyushin_AI-14_R
GPTKB entity
Statements (48)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 6
gptkbp:bfsParent gptkb:Ilyushin_Il-103
gptkbp:application gptkb:aircraft
gptkbp:bore 150 mm
gptkbp:certification certified for use
gptkbp:compression_ratio 6.5:1
gptkbp:cooling_system air-cooled
gptkbp:design Vladimir Ilyushin
gptkbp:displacement 14 liters
gptkbp:engine gptkb:14
high performance
high reliability
four-stroke
horizontally opposed
civil and military aviation
good fuel efficiency
radial layout
aircraft engine design
influential in aircraft design.
2800 rpm
360 hp at 2800 rpm
AI-14 family
gptkbp:engine_type piston engine
AI-14 V, AI-14 R-1
gptkbp:first_flight 1947
gptkbp:fuel_capacity 0.9 m
1.5 m
1.2 m
gptkbp:fuel_type gptkb:product
aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label Ilyushin AI-14 R
gptkbp:ignition_system spark ignition
gptkbp:is_tested_for extensively tested
gptkbp:maintenance low maintenance requirements
gptkbp:manufacturer gptkb:Ilyushin
gptkbp:notable_users gptkb:Soviet_Air_Force
gptkbp:power_output 360 hp
gptkbp:production_years 1947-1955
gptkbp:propulsion variable-pitch propeller
gptkbp:setting 14-cylinder
gptkbp:stroke 150 mm
gptkbp:successor AI-26 engine
gptkbp:torque 500 Nm
gptkbp:type gptkb:engine
gptkbp:used_in gptkb:Ilyushin_Il-14
gptkbp:valve_configuration pushrod
gptkbp:weight 200 kg